                      Code_Saturne
                      ************

 Version:   4.2
 Path:      /home/lgarelli/Code_Saturne/code_saturne-421/

 Result directory:
   /home/lgarelli/RUNS/Code_Saturne/Baffle/Baffle/RESU/20161121-0925


 ****************************************
  Compiling user subroutines and linking
 ****************************************


 ****************************
  Preparing calculation data
 ****************************

 Single processor Code_Saturne simulation.


 ***************************
  Preprocessing calculation
 ***************************


 **********************
  Starting calculation
 **********************

command: 
 ./cs_solver --param Thinh_wall2.xml --log 0

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

                                  (R)
                      Code_Saturne

                      Version 4.2.1


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

  revision 4.2.1
  build Fri 15 Jul 2016 11:52:17 PM ART
  MPI version 3.0 (MPICH 3.1)


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

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

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


Local case configuration:

  Date:                Mon 21 Nov 2016 09:25:12 AM ART
  System:              Linux 4.0.6-200.fc21.x86_64
  Machine:             localhost.localdomain
  Processor:           model name	: Intel(R) Core(TM) i7 CPU       Q 720  @ 1.60GHz
  Memory:              7903 MB
  User:                lgarelli (lgarelli)
  Directory:           /home/lgarelli/RUNS/Code_Saturne/Baffle/Baffle/RESU/20161121-0925
  OpenMP threads:      2
  Processors/node:     8
  I/O read method:     standard input and output, serial access
  I/O write method:    standard input and output, serial access

  External libraries for partitioning:
    METIS

 Reading metadata from file: "mesh_input"

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

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


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




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


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

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

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


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

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


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


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

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

       ICORIO =          0 (Coriolis source terms       )

  -- Continuous phase:

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

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

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

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


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

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


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


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

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


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

 --- Continuous phase:

   - Commons
       ITURB  =             20 (Turbulence model            )
       IWALLF =              4 (wall function               )
                               (0: disabled                 )
                               (1: one scale power law
                                   (forbidden for k-epsilon))
                               (2: one scale log law        )
                               (3: two scales log law       )
                               (4: scalable wall function   )
                               (5: two scales V. Driest     )
                               (6: two scales smooth/rough  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.10880E+02 (Limit Y+                    )
       IGRHOK =              0 (1: computed Grad(rho k)     )

   - k-epsilon           (ITURB = 20)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       ICLKEP =              0 (k-epsilon clipping model    )
       IKECOU =              0 (k-epsilon coupling mode     )
       IGRAKE =              0 (Account for gravity         )


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

 --- Constants

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

   - k-epsilon           (ITURB = 20)
       Ce1    =    0.14400E+01 (Cepsilon 1: production coef.)
       CE2    =    0.19200E+01 (Cepsilon 2: dissipat.  coef.)
       SIGMAK =    0.10000E+01 (Prandtl relative to k       )
       SIGMAE =    0.13000E+01 (Prandtl relative to epsilon )
       CMU    =    0.90000E-01 (Cmu constant                )


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


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

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


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


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

    STEADY ALGORITHM

 --- Global parameters

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


 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per variable relaxation coefficient

-----------------------------
 Variable          RELAXV
-----------------------------
 Velocity          0.7000E+00
 Pressure          0.3000E+00
 k                 0.7000E+00
 epsilon           0.7000E+00
----------------------------

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


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


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

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

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


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


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

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

       ARAK   =    0.10000E+01 (Arakawa factor              )

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


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


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

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

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

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

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


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


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


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


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

------------------------------------
 Variable              EPSILO IDIRCL
------------------------------------
 Velocity          0.1000E-07      1
 Pressure          0.1000E-07      1
 k                 0.1000E-07      1
 epsilon           0.1000E-07      1
------------------------------------

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


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


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

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


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

       INPDT0 =              0 (1: 0 time step calcuation   )
       NTMABS =             50 (Final time step required    )

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


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


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

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

 --- Post-processed variables


Velocity
Pressure
k
epsilon
TurbVisc
total_pressure
Yplus
         --           --

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

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

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

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

         2 Velocity                       0
         5 Pressure                       0
         6 k                              0
         7 epsilon                        0
        10 TurbVisc                    -999
        13 total_pressure              -999
         --           --                --

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


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


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

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


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


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

  -1: name: Result_subroutine3
      directory: postprocessing
      format: EnSight Gold
      options: binary
      time dependency: fixed mesh
      output: at calculation end


 Reading file:        mesh_input
 Finished reading:    mesh_input

  After addition of user-defined thin walls
     Number of cells:          20000
     Number of interior faces: 55850
     Number of boundary faces: 8300
     Number of vertices:       24321
 Number of cells:                                      20000

 ----------------------------------------------------------
 Number of cells + halo cells:                         20000


 ----------------------------------------------------------
 Number of interior faces:                             55850

 ----------------------------------------------------------
 Number of boundary faces:                             8300

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

 Histogram of the number of interior faces per cell:

    minimum value =                  3
    maximum value =                  6

      1 : [          3 ;          4 [ =         12
      2 : [          4 ;          5 [ =        884
      3 : [          5 ;          6 ] =      19104

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

 Renumbering mesh:

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

   renumbering for interior faces:
     cell adjacency pre-ordering:         lowest id first
     faces adjacent to ghost cells last:  no
     numbering:                           multipass

   renumbering for boundary faces:
     numbering:                           none

 Number of thread pools for interior faces :          2
 Number of threading groups for interior faces :      2
 Estimated thread imbalance for interior faces :      8.95255e-04

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

 Matrix bandwidth for volume mesh :          10099
 Matrix profile/lines for volume mesh :      149

 Mesh coordinates:               minimum    and maximum
                       X :  0.0000000e+00  5.0000000e-01
                       Y :  0.0000000e+00  5.0000000e-01
                       Z :  0.0000000e+00  1.0000000e+01
 Mesh
     Number of cells:          20000
     Number of interior faces: 55850
     Number of boundary faces: 8300
     Number of vertices:       24321

 Groups:
    "3"
       cells:                 20000
    "5"
       boundary faces:         8000
    "6"
       boundary faces:          100
    "7"
       boundary faces:          100
    "8"
       boundary faces:          100

 --- Information on the volumes
       Minimum control volume      =  1.2500000e-04
       Maximum control volume      =  1.2500000e-04
       Total volume for the domain =  2.5000000e+00

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

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

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

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

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

 Computing geometric quantities (0.0546 s)
                                                             
       ALMAX  =    0.13572E+01 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.

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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Pressure          0.0000E+00  0.0000E+00
  k                 0.6000E-03  0.6000E-03
  epsilon           0.9746E-06  0.9746E-06
 ---------------------------------



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

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



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



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


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




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


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


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1179E+01  0.1179E+01
  molecular_viscos  0.1830E-04  0.1830E-04
  turbulent_viscos  0.3918E-01  0.3918E-01
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         100
Smooth wall               5        8100
Rough wall                6           0
Symmetry                  4           0
Free outlet               3         100
Free inlet               13           0
Convective inlet         15           0
Free surface             14           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.25000E-01   0.25000E-01   0.10000E+02



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100         0.000000000E+00
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.00000E+00 0.00000E+00
   Friction velocity        uk    :  0.13416E-01 0.13416E-01
   Dimensionless distance   yplus :  0.21602E+02 0.21602E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39337E+00      44   0.37117E-01   0.10722E+05 0.10436E+03 
c  Velocity[X]                                      0.11769E+03 
c  Velocity[Y]                                      0.12307E+00 
c  Velocity[Z]                                      0.10604E+05 
c  Pressure     0.22802E+00     156   0.80485E-08   0.10000E+01 0.10666E+03 
c  k            0.27914E+01      47   0.23415E-05   0.19484E+02 0.96919E+02 
c  epsilon      0.50492E+00      49   0.50526E-05   0.79919E+00 0.96273E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.142          21.142     -1.5625e-10     -1.5625e-10
v  Velocity[Y]           -0.83231         0.83231     -1.0033e-10     -1.0033e-10
v  Velocity[Z]             1.3196          27.483          9.9841          9.9841
v  ǁVelocityǁ               2.106          30.853          10.047          10.047
v  Pressure                7.3405          3796.8            1904            1904
v  k                   0.00059999          5.3033        0.065138        0.065138
v  epsilon             9.8866e-07          1.0062         0.01402         0.01402
v  TurbVisc              0.039183        0.039183        0.039183        0.039183
v  total_pressure      1.0133e+05      1.0512e+05      1.0323e+05      1.0323e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          21.602          21.082          21.082


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294654998E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.77981E+00 0.22050E+02
   Friction velocity        uet   :  0.11897E+00 0.24651E+01
   Friction velocity        uk    :  0.13416E-01 0.11993E+01
   Dimensionless distance   yplus :  0.21602E+02 0.19310E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69496E+02      45   0.40156E-01   0.30733E+03 0.82813E+02 
c  Velocity[X]                                      0.11985E+03 
c  Velocity[Y]                                      0.15430E+01 
c  Velocity[Z]                                      0.18594E+03 
c  Pressure     0.23599E+00      92   0.87946E-08   0.10000E+01 0.13821E+04 
c  k            0.35991E+02      39   0.32178E-03   0.46703E+02 0.10568E+04 
c  epsilon      0.79847E+03      43   0.21187E-02   0.80989E+06 0.37863E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.377          18.072       -0.003832       -0.003832
v  Velocity[Y]            -1.6956          1.6765      1.2102e-10      1.2102e-10
v  Velocity[Z]           -0.71355          24.961          10.011          10.011
v  ǁVelocityǁ             0.46111          25.014          10.068          10.068
v  Pressure               -182.25           405.3          109.74          109.74
v  k                   0.00060469          4.3705        0.094935        0.094935
v  epsilon             1.1053e-06          398.44          1.5765          1.5765
v  TurbVisc            5.4189e-05          2.9652        0.040806        0.040806
v  total_pressure      1.0114e+05      1.0173e+05      1.0143e+05      1.0143e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0            1931          58.034          58.034


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655002E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.12635E+00 0.20122E+02
   Friction velocity        uet   :  0.84350E-02 0.13865E+01
   Friction velocity        uk    :  0.38462E-01 0.10798E+01
   Dimensionless distance   yplus :  0.61930E+02 0.17387E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15977E+03      40   0.30828E-01   0.54807E+03 0.18551E+03 
c  Velocity[X]                                      0.22879E+03 
c  Velocity[Y]                                      0.11808E+02 
c  Velocity[Z]                                      0.30747E+03 
c  Pressure     0.16850E+00      89   0.98061E-08   0.99341E+00 0.84162E+03 
c  k            0.13594E+03      51   0.31825E-02   0.17068E+05 0.11515E+05 
c  epsilon      0.54834E+02      44   0.18783E+00   0.18513E+06 0.30192E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5792           19.98       -0.002497       -0.002497
v  Velocity[Y]            -3.1243          3.1398     -5.7133e-06     -5.7133e-06
v  Velocity[Z]            -4.9062          25.637          10.013          10.013
v  ǁVelocityǁ             0.46122          26.086          10.083          10.083
v  Pressure               -398.08          673.95          233.37          233.37
v  k                   0.00063986          22.685         0.35375         0.35375
v  epsilon             2.7167e-06          155.71           1.232           1.232
v  TurbVisc            0.00014269          14.727        0.090347        0.090347
v  total_pressure      1.0093e+05        1.02e+05      1.0156e+05      1.0156e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          1738.7          125.16          125.16


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.47109E-02 0.22061E+02
   Friction velocity        uet   :  0.24896E-03 0.13099E+01
   Friction velocity        uk    :  0.62193E-01 0.24277E+01
   Dimensionless distance   yplus :  0.10014E+03 0.39089E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12061E+04      39   0.24588E-01   0.21984E+04 0.10996E+04 
c  Velocity[X]                                      0.11701E+04 
c  Velocity[Y]                                      0.74185E+02 
c  Velocity[Z]                                      0.95414E+03 
c  Pressure     0.15009E+00     106   0.78953E-08   0.11138E+01 0.13678E+05 
c  k            0.17374E+04      48   0.21370E-03   0.70027E+05 0.27019E+05 
c  epsilon      0.17111E+05      49   0.27806E-02   0.84992E+08 0.26063E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3162          16.533         -0.0017         -0.0017
v  Velocity[Y]            -5.3894          5.3946      9.3475e-07      9.3475e-07
v  Velocity[Z]            -7.6246          41.634          10.007          10.007
v  ǁVelocityǁ             0.82167          41.637          10.106          10.106
v  Pressure               -1911.1            6725          1295.1          1295.1
v  k                   0.00074229          40.335          0.7417          0.7417
v  epsilon             1.5963e-05          2025.2          6.6824          6.6824
v  TurbVisc            0.00018873          105.43         0.73214         0.73214
v  total_pressure           99414      1.0805e+05      1.0262e+05      1.0262e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3908.9          260.31          260.31


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294654998E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.23341E+00 0.34875E+02
   Friction velocity        uet   :  0.11834E-01 0.18931E+01
   Friction velocity        uk    :  0.84869E-01 0.34786E+01
   Dimensionless distance   yplus :  0.13665E+03 0.56010E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10305E+03      44   0.65798E-01   0.60538E+04 0.38011E+03 
c  Velocity[X]                                      0.36453E+04 
c  Velocity[Y]                                      0.68102E+03 
c  Velocity[Z]                                      0.17275E+04 
c  Pressure     0.12603E+01      79   0.98580E-08   0.16368E+01 0.75086E+03 
c  k            0.65569E+02      46   0.44061E-02   0.18916E+04 0.76776E+03 
c  epsilon      0.14826E+04      46   0.25823E-01   0.12135E+08 0.14638E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -59.819          40.832        -0.01476        -0.01476
v  Velocity[Y]            -24.952           24.92       -2.15e-05       -2.15e-05
v  Velocity[Z]            -24.436          40.569          9.9854          9.9854
v  ǁVelocityǁ             0.86557          60.157          10.288          10.288
v  Pressure               -770.68          2363.9          845.91          845.91
v  k                    0.0011404          45.597          1.0341          1.0341
v  epsilon             0.00011433          4097.3          14.261          14.261
v  TurbVisc            0.00030397          3.3002         0.14453         0.14453
v  total_pressure      1.0055e+05      1.0369e+05      1.0217e+05      1.0217e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0            5601          461.15          461.15


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294654990E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.35101E-01 0.51498E+02
   Friction velocity        uet   :  0.18760E-02 0.23596E+01
   Friction velocity        uk    :  0.10839E+00 0.36985E+01
   Dimensionless distance   yplus :  0.17453E+03 0.59551E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60135E+02      45   0.88869E-01   0.16654E+04 0.13148E+03 
c  Velocity[X]                                      0.10393E+04 
c  Velocity[Y]                                      0.96187E+02 
c  Velocity[Z]                                      0.52990E+03 
c  Pressure     0.73542E+00     127   0.86132E-08   0.25631E+01 0.96874E+03 
c  k            0.56597E+02      46   0.38785E-01   0.67270E+04 0.58943E+03 
c  epsilon      0.25774E+04      43   0.78856E-01   0.13933E+08 0.55650E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.218          23.109        -0.01269        -0.01269
v  Velocity[Y]            -13.048          13.056     -8.9847e-06     -8.9847e-06
v  Velocity[Z]             -13.53          40.485           9.992           9.992
v  ǁVelocityǁ              1.4218          40.488          10.283          10.283
v  Pressure               -740.82          1008.2          326.72          326.72
v  k                    0.0024889          83.916          1.5049          1.5049
v  epsilon             0.00059686          7004.7          29.317          29.317
v  TurbVisc            0.00048418          1.3275        0.079723        0.079723
v  total_pressure      1.0058e+05      1.0233e+05      1.0165e+05      1.0165e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          5955.1          640.91          640.91


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655004E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.18433E+00 0.34361E+02
   Friction velocity        uet   :  0.97570E-02 0.17154E+01
   Friction velocity        uk    :  0.13112E+00 0.48525E+01
   Dimensionless distance   yplus :  0.21112E+03 0.78131E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46120E+02      42   0.73895E-01   0.39677E+03 0.59537E+02 
c  Velocity[X]                                      0.17623E+03 
c  Velocity[Y]                                      0.25829E+02 
c  Velocity[Z]                                      0.19472E+03 
c  Pressure     0.49763E+00      98   0.75563E-08   0.26370E+01 0.38000E+03 
c  k            0.63749E+02      44   0.10285E-01   0.22688E+04 0.25942E+03 
c  epsilon      0.43612E+04      41   0.73335E-01   0.62441E+08 0.47888E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.729          19.932      -0.0076533      -0.0076533
v  Velocity[Y]            -8.1145          8.1412     -2.9974e-06     -2.9974e-06
v  Velocity[Z]            -12.456           39.11          9.9954          9.9954
v  ǁVelocityǁ             0.72719          39.115          10.277          10.277
v  Pressure               -574.98          568.34          181.66          181.66
v  k                    0.0048663          133.94          1.8333          1.8333
v  epsilon              0.0016505           23606          51.657          51.657
v  TurbVisc            0.00064511          0.8999        0.049048        0.049048
v  total_pressure      1.0075e+05      1.0189e+05      1.0151e+05      1.0151e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          7813.1           772.8           772.8


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294654998E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.38101E+00 0.33251E+02
   Friction velocity        uet   :  0.19038E-01 0.16421E+01
   Friction velocity        uk    :  0.15211E+00 0.63390E+01
   Dimensionless distance   yplus :  0.24492E+03 0.10207E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41121E+02      42   0.67978E-01   0.23456E+03 0.43574E+02 
c  Velocity[X]                                      0.81752E+02 
c  Velocity[Y]                                      0.12529E+02 
c  Velocity[Z]                                      0.14028E+03 
c  Pressure     0.35714E+00      70   0.96968E-08   0.23218E+01 0.75723E+02 
c  k            0.54019E+02      43   0.18348E-01   0.12860E+04 0.18118E+03 
c  epsilon      0.53890E+04      39   0.23629E-01   0.37309E+07 0.12164E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -9.0783           17.43      -0.0048292      -0.0048292
v  Velocity[Y]            -5.6913          5.7116       7.193e-06       7.193e-06
v  Velocity[Z]            -11.926          37.508          9.9981          9.9981
v  ǁVelocityǁ             0.99237          37.515          10.275          10.275
v  Pressure               -414.26           438.7          154.31          154.31
v  k                    0.0083069           98.67          1.9897          1.9897
v  epsilon              0.0034041           25346           58.93           58.93
v  TurbVisc            0.00099778          0.6886        0.037407        0.037407
v  total_pressure      1.0091e+05      1.0176e+05      1.0148e+05      1.0148e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0           10207          842.34          842.34


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.20812E+00 0.31560E+02
   Friction velocity        uet   :  0.95104E-02 0.15679E+01
   Friction velocity        uk    :  0.17137E+00 0.54407E+01
   Dimensionless distance   yplus :  0.27593E+03 0.87603E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39195E+02      42   0.61631E-01   0.16519E+03 0.35571E+02 
c  Velocity[X]                                      0.51276E+02 
c  Velocity[Y]                                      0.79878E+01 
c  Velocity[Z]                                      0.10593E+03 
c  Pressure     0.26678E+00      96   0.63997E-08   0.21773E+01 0.26591E+02 
c  k            0.46723E+02      42   0.34766E-01   0.11841E+04 0.16354E+03 
c  epsilon      0.38681E+04      38   0.16605E+00   0.10784E+08 0.20098E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9364          15.434      -0.0036308      -0.0036308
v  Velocity[Y]            -3.9878          4.0108      3.7882e-06      3.7882e-06
v  Velocity[Z]                -12          36.025          9.9992          9.9992
v  ǁVelocityǁ             0.78912          36.034          10.281          10.281
v  Pressure               -342.13          376.91          145.93          145.93
v  k                     0.012657          64.025          2.0687          2.0687
v  epsilon              0.0059223           13171          56.864          56.864
v  TurbVisc             0.0013011         0.55096         0.03141         0.03141
v  total_pressure      1.0098e+05       1.017e+05      1.0147e+05      1.0147e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          8760.3          871.15          871.15


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.24094E+00 0.30035E+02
   Friction velocity        uet   :  0.12100E-01 0.15032E+01
   Friction velocity        uk    :  0.18890E+00 0.42427E+01
   Dimensionless distance   yplus :  0.30415E+03 0.68313E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38297E+02      42   0.53845E-01   0.13254E+03 0.31275E+02 
c  Velocity[X]                                      0.38702E+02 
c  Velocity[Y]                                      0.58758E+01 
c  Velocity[Z]                                      0.87967E+02 
c  Pressure     0.21045E+00     110   0.92166E-08   0.20533E+01 0.14982E+02 
c  k            0.43025E+02      42   0.25933E-01   0.84685E+03 0.14113E+03 
c  epsilon      0.23771E+04      38   0.18197E+00   0.49315E+07 0.19910E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0367          14.729      -0.0031248      -0.0031248
v  Velocity[Y]            -3.3375          3.4181       1.124e-05       1.124e-05
v  Velocity[Z]            -11.941          34.625          9.9998          9.9998
v  ǁVelocityǁ             0.41459          34.634          10.293          10.293
v  Pressure               -317.87          353.07          146.37          146.37
v  k                     0.017887          45.043          2.1263          2.1263
v  epsilon              0.0092151          5626.6          54.447          54.447
v  TurbVisc             0.0015229         0.45528        0.027809        0.027809
v  total_pressure      1.0101e+05      1.0168e+05      1.0147e+05      1.0147e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          6831.3          880.17          880.17


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.10648E+00 0.28655E+02
   Friction velocity        uet   :  0.59713E-02 0.14447E+01
   Friction velocity        uk    :  0.20467E+00 0.36011E+01
   Dimensionless distance   yplus :  0.32955E+03 0.57982E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37962E+02      41   0.49069E-01   0.10537E+03 0.27400E+02 
c  Velocity[X]                                      0.27120E+02 
c  Velocity[Y]                                      0.44749E+01 
c  Velocity[Z]                                      0.73778E+02 
c  Pressure     0.17193E+00     105   0.79885E-08   0.18628E+01 0.17151E+02 
c  k            0.41221E+02      41   0.15078E-01   0.62295E+03 0.12157E+03 
c  epsilon      0.17065E+04      38   0.11354E+00   0.22186E+07 0.19072E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5871          15.151      -0.0030374      -0.0030374
v  Velocity[Y]            -3.0334          3.0457      1.3203e-05      1.3203e-05
v  Velocity[Z]            -11.966          33.269              10              10
v  ǁVelocityǁ              0.6107          33.276          10.309          10.309
v  Pressure               -302.94          350.83           149.8           149.8
v  k                     0.023756          37.204          2.1801          2.1801
v  epsilon               0.013243          3559.8           53.48           53.48
v  TurbVisc             0.0017557         0.38143        0.025441        0.025441
v  total_pressure      1.0102e+05      1.0168e+05      1.0147e+05      1.0147e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          5798.2          880.86          880.86


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.17795E+00 0.27357E+02
   Friction velocity        uet   :  0.10218E-01 0.13900E+01
   Friction velocity        uk    :  0.21879E+00 0.29847E+01
   Dimensionless distance   yplus :  0.35228E+03 0.48058E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         12, Physical time    0.12000E+02


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

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

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

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

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37905E+02      41   0.45201E-01   0.92452E+02 0.25233E+02 
c  Velocity[X]                                      0.22611E+02 
c  Velocity[Y]                                      0.39342E+01 
c  Velocity[Z]                                      0.65906E+02 
c  Pressure     0.13666E+00      91   0.71973E-08   0.16489E+01 0.15443E+02 
c  k            0.40286E+02      41   0.88225E-02   0.47773E+03 0.10492E+03 
c  epsilon      0.14224E+04      38   0.57810E-01   0.11850E+07 0.16404E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2379          15.588      -0.0031665      -0.0031665
v  Velocity[Y]            -3.6144          3.4861      1.4299e-05      1.4299e-05
v  Velocity[Z]            -12.221          32.018          10.001          10.001
v  ǁVelocityǁ             0.43273           32.03          10.328          10.328
v  Pressure               -301.03          363.42          152.69          152.69
v  k                     0.030211          38.127          2.2352          2.2352
v  epsilon               0.017915          2210.5          53.622          53.622
v  TurbVisc             0.0019945         0.32397        0.023801        0.023801
v  total_pressure      1.0102e+05      1.0169e+05      1.0148e+05      1.0148e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4805.8          878.84          878.84


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.17895E+00 0.26936E+02
   Friction velocity        uet   :  0.12162E-01 0.13404E+01
   Friction velocity        uk    :  0.23163E+00 0.26243E+01
   Dimensionless distance   yplus :  0.37296E+03 0.42256E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37998E+02      41   0.40026E-01   0.79234E+02 0.23001E+02 
c  Velocity[X]                                      0.16511E+02 
c  Velocity[Y]                                      0.33522E+01 
c  Velocity[Z]                                      0.59371E+02 
c  Pressure     0.10010E+00     112   0.74262E-08   0.12760E+01 0.15135E+02 
c  k            0.39751E+02      40   0.59184E-02   0.38669E+03 0.92332E+02 
c  epsilon      0.12877E+04      37   0.31401E-01   0.72661E+06 0.13635E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8883          15.948       -0.003311       -0.003311
v  Velocity[Y]            -3.9488          4.0122      1.6791e-05      1.6791e-05
v  Velocity[Z]            -12.348          31.347          10.001          10.001
v  ǁVelocityǁ             0.41167          31.366          10.348          10.348
v  Pressure               -300.72          382.03          155.29          155.29
v  k                     0.036801          39.992          2.2918          2.2918
v  epsilon               0.023127          1391.9          54.302          54.302
v  TurbVisc              0.001802         0.27854        0.022633        0.022633
v  total_pressure      1.0102e+05      1.0171e+05      1.0148e+05      1.0148e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4225.6          876.77          876.77


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.19611E+00 0.26772E+02
   Friction velocity        uet   :  0.15112E-01 0.13043E+01
   Friction velocity        uk    :  0.24345E+00 0.25883E+01
   Dimensionless distance   yplus :  0.39199E+03 0.41675E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38224E+02      41   0.38281E-01   0.68750E+02 0.21098E+02 
c  Velocity[X]                                      0.13348E+02 
c  Velocity[Y]                                      0.30386E+01 
c  Velocity[Z]                                      0.52363E+02 
c  Pressure     0.68490E-01     100   0.63835E-08   0.87359E+00 0.13462E+02 
c  k            0.39464E+02      40   0.45046E-02   0.32309E+03 0.82317E+02 
c  epsilon      0.12166E+04      37   0.19280E-01   0.48467E+06 0.11409E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.7342          16.115      -0.0033344      -0.0033344
v  Velocity[Y]            -4.2318          4.2813      1.1972e-05      1.1972e-05
v  Velocity[Z]            -12.527          31.074          10.002          10.002
v  ǁVelocityǁ             0.44378          31.085           10.37           10.37
v  Pressure               -301.19           395.2          156.51          156.51
v  k                     0.043624          41.629          2.3507          2.3507
v  epsilon               0.028774            1320          55.251          55.251
v  TurbVisc            0.00075111         0.23975        0.021794        0.021794
v  total_pressure      1.0102e+05      1.0172e+05      1.0148e+05      1.0148e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4167.5          875.35          875.35


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.22878E+00 0.26548E+02
   Friction velocity        uet   :  0.18935E-01 0.12929E+01
   Friction velocity        uk    :  0.25383E+00 0.25400E+01
   Dimensionless distance   yplus :  0.40870E+03 0.40898E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38520E+02      41   0.37836E-01   0.59936E+02 0.19402E+02 
c  Velocity[X]                                      0.10442E+02 
c  Velocity[Y]                                      0.25431E+01 
c  Velocity[Z]                                      0.46951E+02 
c  Pressure     0.52721E-01     117   0.74088E-08   0.68286E+00 0.12779E+02 
c  k            0.39358E+02      39   0.37687E-02   0.27512E+03 0.73937E+02 
c  epsilon      0.11722E+04      36   0.14368E-01   0.35914E+06 0.98777E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.5183          16.183      -0.0032564      -0.0032564
v  Velocity[Y]            -3.5637          3.5526      3.8392e-06      3.8392e-06
v  Velocity[Z]            -12.865          31.052          10.002          10.002
v  ǁVelocityǁ             0.33838          31.068          10.392          10.392
v  Pressure               -305.41          403.88           156.7           156.7
v  k                     0.050507          43.735          2.4126          2.4126
v  epsilon               0.034753          1256.6          56.339          56.339
v  TurbVisc             0.0003607         0.21222          0.0212          0.0212
v  total_pressure      1.0102e+05      1.0173e+05      1.0148e+05      1.0148e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4089.8          874.85          874.85


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.27996E+00 0.26534E+02
   Friction velocity        uet   :  0.14918E-01 0.12944E+01
   Friction velocity        uk    :  0.23911E+00 0.24893E+01
   Dimensionless distance   yplus :  0.38500E+03 0.40081E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38899E+02      41   0.37503E-01   0.53879E+02 0.18063E+02 
c  Velocity[X]                                      0.86240E+01 
c  Velocity[Y]                                      0.21875E+01 
c  Velocity[Z]                                      0.43067E+02 
c  Pressure     0.47321E-01     100   0.74976E-08   0.62112E+00 0.12714E+02 
c  k            0.39423E+02      39   0.32805E-02   0.23739E+03 0.66647E+02 
c  epsilon      0.11413E+04      36   0.11698E-01   0.28298E+06 0.87394E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2989          15.932      -0.0031509      -0.0031509
v  Velocity[Y]            -3.3586          3.3204      2.8443e-06      2.8443e-06
v  Velocity[Z]            -13.073          31.215          10.002          10.002
v  ǁVelocityǁ              0.4415          31.224          10.413          10.413
v  Pressure               -303.52          404.29          154.56          154.56
v  k                     0.057315          45.288           2.478           2.478
v  epsilon               0.040965            1196          57.538          57.538
v  TurbVisc            0.00025432         0.21245        0.020796        0.020796
v  total_pressure      1.0102e+05      1.0173e+05      1.0148e+05      1.0148e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4008.1          875.43          875.43


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.36973E+00 0.26567E+02
   Friction velocity        uet   :  0.19704E-01 0.13067E+01
   Friction velocity        uk    :  0.21312E+00 0.24358E+01
   Dimensionless distance   yplus :  0.34315E+03 0.39220E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39258E+02      41   0.34558E-01   0.48121E+02 0.16775E+02 
c  Velocity[X]                                      0.77936E+01 
c  Velocity[Y]                                      0.18109E+01 
c  Velocity[Z]                                      0.38516E+02 
c  Pressure     0.38070E-01     105   0.71952E-08   0.52424E+00 0.12553E+02 
c  k            0.39639E+02      39   0.29185E-02   0.20635E+03 0.60130E+02 
c  epsilon      0.11194E+04      36   0.10039E-01   0.23157E+06 0.78264E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.15          16.238      -0.0030551      -0.0030551
v  Velocity[Y]            -2.9411          2.9035      4.2186e-06      4.2186e-06
v  Velocity[Z]            -13.467          31.347          10.002          10.002
v  ǁVelocityǁ             0.31376          31.349          10.435          10.435
v  Pressure               -307.01          402.91          152.86          152.86
v  k                     0.063945          46.743          2.5471          2.5471
v  epsilon               0.047272          1133.8          58.838          58.838
v  TurbVisc            0.00026657         0.21413        0.020542        0.020542
v  total_pressure      1.0102e+05      1.0173e+05      1.0148e+05      1.0148e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0            3922          877.07          877.07


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.24585E+00 0.26688E+02
   Friction velocity        uet   :  0.13246E-01 0.13223E+01
   Friction velocity        uk    :  0.22792E+00 0.23818E+01
   Dimensionless distance   yplus :  0.36697E+03 0.38351E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39688E+02      41   0.33699E-01   0.43072E+02 0.15630E+02 
c  Velocity[X]                                      0.67781E+01 
c  Velocity[Y]                                      0.14755E+01 
c  Velocity[Z]                                      0.34818E+02 
c  Pressure     0.34723E-01     104   0.72914E-08   0.48792E+00 0.12488E+02 
c  k            0.40003E+02      39   0.26260E-02   0.18065E+03 0.54357E+02 
c  epsilon      0.11052E+04      36   0.87581E-02   0.19356E+06 0.70539E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9487          16.065       -0.002916       -0.002916
v  Velocity[Y]            -2.8855          2.8206      4.1665e-06      4.1665e-06
v  Velocity[Z]            -13.743          31.498          10.002          10.002
v  ǁVelocityǁ             0.35011          31.503          10.456          10.456
v  Pressure               -305.72          402.28             151             151
v  k                     0.070326          48.009            2.62            2.62
v  epsilon               0.053612          1165.8          60.245          60.245
v  TurbVisc            0.00043501         0.21563        0.020413        0.020413
v  total_pressure      1.0102e+05      1.0173e+05      1.0148e+05      1.0148e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3835.1           879.6           879.6


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.14202E+00 0.26773E+02
   Friction velocity        uet   :  0.98959E-02 0.13395E+01
   Friction velocity        uk    :  0.26720E+00 0.23368E+01
   Dimensionless distance   yplus :  0.43022E+03 0.37626E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40131E+02      41   0.32051E-01   0.38510E+02 0.14567E+02 
c  Velocity[X]                                      0.56989E+01 
c  Velocity[Y]                                      0.11555E+01 
c  Velocity[Z]                                      0.31655E+02 
c  Pressure     0.32581E-01     108   0.89839E-08   0.45448E+00 0.12339E+02 
c  k            0.40526E+02      38   0.23710E-02   0.15912E+03 0.49218E+02 
c  epsilon      0.10987E+04      35   0.76401E-02   0.16322E+06 0.63540E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7448          16.134      -0.0027832      -0.0027832
v  Velocity[Y]            -2.5235          2.4837      2.2226e-06      2.2226e-06
v  Velocity[Z]            -14.078          31.706          10.002          10.002
v  ǁVelocityǁ             0.31115          31.711          10.476          10.476
v  Pressure               -307.39          399.97          149.11          149.11
v  k                     0.076407          49.071          2.6974          2.6974
v  epsilon               0.059902          1214.3          61.784          61.784
v  TurbVisc            0.00094583         0.21743        0.020385        0.020385
v  total_pressure      1.0102e+05      1.0172e+05      1.0147e+05      1.0147e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3762.6          882.98          882.98


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.16019E+00 0.26877E+02
   Friction velocity        uet   :  0.10177E-01 0.13579E+01
   Friction velocity        uk    :  0.29201E+00 0.22964E+01
   Dimensionless distance   yplus :  0.47018E+03 0.36976E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40571E+02      41   0.31663E-01   0.34742E+02 0.13642E+02 
c  Velocity[X]                                      0.55406E+01 
c  Velocity[Y]                                      0.89862E+00 
c  Velocity[Z]                                      0.28303E+02 
c  Pressure     0.29570E-01     112   0.70001E-08   0.42130E+00 0.12465E+02 
c  k            0.41175E+02      38   0.21555E-02   0.14138E+03 0.44736E+02 
c  epsilon      0.10992E+04      35   0.66497E-02   0.13861E+06 0.57179E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6038          16.492      -0.0026768      -0.0026768
v  Velocity[Y]            -2.3693          2.2948     -4.4903e-06     -4.4903e-06
v  Velocity[Z]            -14.334          31.855          10.002          10.002
v  ǁVelocityǁ             0.24301          31.859          10.496          10.496
v  Pressure               -306.48          394.87          146.52          146.52
v  k                     0.082157          50.068          2.7785          2.7785
v  epsilon                0.06605          1243.3          63.454          63.454
v  TurbVisc             0.0018492         0.21949        0.020444        0.020444
v  total_pressure      1.0102e+05      1.0172e+05      1.0147e+05      1.0147e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3697.6          887.11          887.11


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.20342E+00 0.27041E+02
   Friction velocity        uet   :  0.10972E-01 0.13724E+01
   Friction velocity        uk    :  0.29748E+00 0.22687E+01
   Dimensionless distance   yplus :  0.47898E+03 0.36529E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41041E+02      40   0.30459E-01   0.31572E+02 0.12823E+02 
c  Velocity[X]                                      0.48056E+01 
c  Velocity[Y]                                      0.72320E+00 
c  Velocity[Z]                                      0.26043E+02 
c  Pressure     0.26205E-01     113   0.82416E-08   0.36414E+00 0.11891E+02 
c  k            0.41983E+02      38   0.19777E-02   0.12745E+03 0.41007E+02 
c  epsilon      0.11073E+04      35   0.58030E-02   0.11933E+06 0.51639E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.429            16.1      -0.0025565      -0.0025565
v  Velocity[Y]            -2.3959          2.4122     -2.8027e-06     -2.8027e-06
v  Velocity[Z]            -14.474          32.074          10.002          10.002
v  ǁVelocityǁ             0.23238          32.078          10.514          10.514
v  Pressure               -307.59          393.67          144.51          144.51
v  k                     0.087557          50.933           2.864           2.864
v  epsilon               0.071987          1276.8          65.281          65.281
v  TurbVisc             0.0029488         0.22112        0.020575        0.020575
v  total_pressure      1.0102e+05      1.0172e+05      1.0147e+05      1.0147e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3652.9          891.92          891.92


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11600E+00 0.27154E+02
   Friction velocity        uet   :  0.63681E-02 0.13854E+01
   Friction velocity        uk    :  0.30240E+00 0.22425E+01
   Dimensionless distance   yplus :  0.48690E+03 0.36107E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41484E+02      40   0.29373E-01   0.28773E+02 0.12143E+02 
c  Velocity[X]                                      0.43012E+01 
c  Velocity[Y]                                      0.57787E+00 
c  Velocity[Z]                                      0.23894E+02 
c  Pressure     0.23777E-01     112   0.72204E-08   0.33031E+00 0.11592E+02 
c  k            0.42908E+02      38   0.18417E-02   0.11677E+03 0.37960E+02 
c  epsilon      0.11221E+04      35   0.51777E-02   0.10503E+06 0.47003E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2518           16.41      -0.0024799      -0.0024799
v  Velocity[Y]            -2.2053          2.2058      8.4256e-07      8.4256e-07
v  Velocity[Z]            -14.727          32.279          10.002          10.002
v  ǁVelocityǁ             0.15803          32.288          10.532          10.532
v  Pressure               -306.87          392.85          143.13          143.13
v  k                     0.092596          51.655          2.9533          2.9533
v  epsilon               0.077735          1296.2          67.265          67.265
v  TurbVisc             0.0031457         0.22349         0.02077         0.02077
v  total_pressure      1.0102e+05      1.0172e+05      1.0147e+05      1.0147e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3610.7          897.32          897.32


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.17747E+00 0.27286E+02
   Friction velocity        uet   :  0.97674E-02 0.13971E+01
   Friction velocity        uk    :  0.30683E+00 0.22295E+01
   Dimensionless distance   yplus :  0.49403E+03 0.35898E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41912E+02      40   0.31740E-01   0.26642E+02 0.11571E+02 
c  Velocity[X]                                      0.44352E+01 
c  Velocity[Y]                                      0.47726E+00 
c  Velocity[Z]                                      0.21730E+02 
c  Pressure     0.25391E-01     101   0.72229E-08   0.35283E+00 0.11779E+02 
c  k            0.43979E+02      38   0.17417E-02   0.10933E+03 0.35656E+02 
c  epsilon      0.11440E+04      34   0.47813E-02   0.95542E+05 0.43462E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1117          16.579      -0.0024089      -0.0024089
v  Velocity[Y]            -2.1948          2.1445     -1.8736e-07     -1.8736e-07
v  Velocity[Z]            -14.876          32.325          10.002          10.002
v  ǁVelocityǁ             0.22991          32.331          10.549          10.549
v  Pressure               -307.28          387.03          140.25          140.25
v  k                     0.097256          52.489          3.0464          3.0464
v  epsilon               0.083278          1322.2          69.412          69.412
v  TurbVisc             0.0031781         0.22541        0.021017        0.021017
v  total_pressure      1.0102e+05      1.0171e+05      1.0147e+05      1.0147e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3589.8          903.24          903.24


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.19001E+00 0.27423E+02
   Friction velocity        uet   :  0.10180E-01 0.14042E+01
   Friction velocity        uk    :  0.31081E+00 0.22284E+01
   Dimensionless distance   yplus :  0.50045E+03 0.35880E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         24, Physical time    0.24000E+02


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

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

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

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

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42332E+02      40   0.27269E-01   0.25417E+02 0.11222E+02 
c  Velocity[X]                                      0.42810E+01 
c  Velocity[Y]                                      0.39616E+00 
c  Velocity[Z]                                      0.20739E+02 
c  Pressure     0.24402E-01     100   0.56336E-08   0.33839E+00 0.11331E+02 
c  k            0.45154E+02      37   0.16709E-02   0.10419E+03 0.33888E+02 
c  epsilon      0.11718E+04      34   0.45978E-02   0.90002E+05 0.40889E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9911          16.089      -0.0023231      -0.0023231
v  Velocity[Y]            -2.5168          2.4357      1.5826e-06      1.5826e-06
v  Velocity[Z]            -15.025          32.497          10.001          10.001
v  ǁVelocityǁ             0.15378          32.501          10.565          10.565
v  Pressure               -306.13          384.24          137.64          137.64
v  k                      0.10144          53.099          3.1424          3.1424
v  epsilon               0.088691          1334.8          71.693          71.693
v  TurbVisc             0.0032019         0.22745        0.021311        0.021311
v  total_pressure      1.0102e+05      1.0171e+05      1.0146e+05      1.0146e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0            3588          909.52          909.52


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.61871E-01 0.27536E+02
   Friction velocity        uet   :  0.34405E-02 0.14115E+01
   Friction velocity        uk    :  0.31437E+00 0.22569E+01
   Dimensionless distance   yplus :  0.50617E+03 0.36339E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42729E+02      40   0.26585E-01   0.22832E+02 0.10578E+02 
c  Velocity[X]                                      0.35665E+01 
c  Velocity[Y]                                      0.31592E+00 
c  Velocity[Z]                                      0.18949E+02 
c  Pressure     0.21478E-01      97   0.96255E-08   0.28819E+00 0.10687E+02 
c  k            0.46434E+02      37   0.16113E-02   0.10066E+03 0.32538E+02 
c  epsilon      0.12047E+04      34   0.45165E-02   0.87106E+05 0.39067E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8368          16.338      -0.0022573      -0.0022573
v  Velocity[Y]            -2.7344          2.6997     -4.5597e-06     -4.5597e-06
v  Velocity[Z]            -15.154          32.577          10.002          10.002
v  ǁVelocityǁ             0.17231          32.581          10.579          10.579
v  Pressure               -305.22          383.89          136.48          136.48
v  k                      0.10526          53.886          3.2413          3.2413
v  epsilon               0.094059          1357.5          74.102          74.102
v  TurbVisc             0.0032156         0.22989        0.021643        0.021643
v  total_pressure      1.0102e+05      1.0171e+05      1.0146e+05      1.0146e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3633.9          916.11          916.11


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.12878E+00 0.27596E+02
   Friction velocity        uet   :  0.68651E-02 0.14157E+01
   Friction velocity        uk    :  0.31742E+00 0.23029E+01
   Dimensionless distance   yplus :  0.51108E+03 0.37080E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43097E+02      40   0.30317E-01   0.21484E+02 0.10167E+02 
c  Velocity[X]                                      0.38057E+01 
c  Velocity[Y]                                      0.28571E+00 
c  Velocity[Z]                                      0.17392E+02 
c  Pressure     0.23870E-01     109   0.87072E-08   0.31936E+00 0.10632E+02 
c  k            0.47794E+02      37   0.15629E-02   0.98255E+02 0.31451E+02 
c  epsilon      0.12419E+04      34   0.44850E-02   0.85909E+05 0.37716E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7156           16.57      -0.0021799      -0.0021799
v  Velocity[Y]            -2.8872          2.7917     -6.1216e-06     -6.1216e-06
v  Velocity[Z]            -15.192          32.684          10.002          10.002
v  ǁVelocityǁ             0.13641          32.687          10.593          10.593
v  Pressure               -303.61          378.96          134.02          134.02
v  k                      0.10878          54.647          3.3424          3.3424
v  epsilon               0.099597          1372.4          76.609          76.609
v  TurbVisc             0.0032079         0.23232         0.02201         0.02201
v  total_pressure      1.0102e+05       1.017e+05      1.0146e+05      1.0146e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0            3708          922.94          922.94


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.81891E-01 0.27670E+02
   Friction velocity        uet   :  0.43555E-02 0.14201E+01
   Friction velocity        uk    :  0.32017E+00 0.23484E+01
   Dimensionless distance   yplus :  0.51552E+03 0.37812E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43458E+02      40   0.27024E-01   0.20997E+02 0.10039E+02 
c  Velocity[X]                                      0.38399E+01 
c  Velocity[Y]                                      0.25403E+00 
c  Velocity[Z]                                      0.16903E+02 
c  Pressure     0.22927E-01     101   0.91453E-08   0.30579E+00 0.10199E+02 
c  k            0.49208E+02      37   0.15195E-02   0.96802E+02 0.30603E+02 
c  epsilon      0.12820E+04      34   0.44577E-02   0.85936E+05 0.36734E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6116          16.121      -0.0020684      -0.0020684
v  Velocity[Y]            -3.2491          3.1946     -3.9995e-06     -3.9995e-06
v  Velocity[Z]            -15.283          32.701          10.001          10.001
v  ǁVelocityǁ             0.12877          32.705          10.606          10.606
v  Pressure               -301.05          377.32             132             132
v  k                      0.11196          55.345          3.4453          3.4453
v  epsilon                 0.1055          1387.4          79.193          79.193
v  TurbVisc             0.0032013         0.23485        0.022405        0.022405
v  total_pressure      1.0102e+05       1.017e+05      1.0146e+05      1.0146e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3781.2          929.99          929.99


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.99556E-02 0.27670E+02
   Friction velocity        uet   :  0.56013E-03 0.14230E+01
   Friction velocity        uk    :  0.32268E+00 0.23851E+01
   Dimensionless distance   yplus :  0.51956E+03 0.38403E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43795E+02      40   0.25401E-01   0.19110E+02 0.95582E+01 
c  Velocity[X]                                      0.31930E+01 
c  Velocity[Y]                                      0.22903E+00 
c  Velocity[Z]                                      0.15688E+02 
c  Pressure     0.21226E-01     102   0.91921E-08   0.27009E+00 0.96241E+01 
c  k            0.50666E+02      37   0.14704E-02   0.95396E+02 0.29812E+02 
c  epsilon      0.13241E+04      34   0.43853E-02   0.85886E+05 0.35816E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4784          16.368      -0.0019448      -0.0019448
v  Velocity[Y]            -3.4594          3.4381     -3.0052e-06     -3.0052e-06
v  Velocity[Z]            -15.287          32.753          10.001          10.001
v  ǁVelocityǁ             0.17242          32.756          10.617          10.617
v  Pressure               -298.78          376.83          130.86          130.86
v  k                      0.11488          56.113          3.5499          3.5499
v  epsilon                0.11215            1406          81.838          81.838
v  TurbVisc             0.0031967         0.23748        0.022827        0.022827
v  total_pressure      1.0103e+05       1.017e+05      1.0146e+05      1.0146e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3840.3          937.31          937.31


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.54974E-01 0.27700E+02
   Friction velocity        uet   :  0.28482E-02 0.14242E+01
   Friction velocity        uk    :  0.32497E+00 0.24206E+01
   Dimensionless distance   yplus :  0.52325E+03 0.38975E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44117E+02      40   0.28451E-01   0.18167E+02 0.92408E+01 
c  Velocity[X]                                      0.34060E+01 
c  Velocity[Y]                                      0.20648E+00 
c  Velocity[Z]                                      0.14554E+02 
c  Pressure     0.22829E-01     100   0.79558E-08   0.28715E+00 0.94359E+01 
c  k            0.52129E+02      37   0.14246E-02   0.94355E+02 0.29109E+02 
c  epsilon      0.13668E+04      34   0.42842E-02   0.85810E+05 0.34952E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3697          16.514      -0.0017534      -0.0017534
v  Velocity[Y]            -3.6655          3.6424     -6.7807e-07     -6.7807e-07
v  Velocity[Z]            -15.264          32.721          10.001          10.001
v  ǁVelocityǁ             0.13207          32.723          10.628          10.628
v  Pressure               -294.94          373.32          129.09          129.09
v  k                      0.11782          56.953          3.6552          3.6552
v  epsilon                0.11971          1420.6          84.509          84.509
v  TurbVisc             0.0031944         0.24044        0.023271        0.023271
v  total_pressure      1.0103e+05       1.017e+05      1.0145e+05      1.0145e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3897.5          944.78          944.78


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.36093E-01 0.27648E+02
   Friction velocity        uet   :  0.18696E-02 0.14252E+01
   Friction velocity        uk    :  0.32709E+00 0.24487E+01
   Dimensionless distance   yplus :  0.52665E+03 0.39428E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44432E+02      39   0.25664E-01   0.17995E+02 0.92023E+01 
c  Velocity[X]                                      0.35182E+01 
c  Velocity[Y]                                      0.20206E+00 
c  Velocity[Z]                                      0.14275E+02 
c  Pressure     0.21243E-01     103   0.57568E-08   0.26554E+00 0.90554E+01 
c  k            0.53594E+02      37   0.13773E-02   0.93292E+02 0.28436E+02 
c  epsilon      0.14097E+04      34   0.41613E-02   0.85433E+05 0.34082E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2769          16.065      -0.0015057      -0.0015057
v  Velocity[Y]             -3.846          3.8572      2.8245e-06      2.8245e-06
v  Velocity[Z]            -15.245          32.725          10.001          10.001
v  ǁVelocityǁ              0.1807          32.727          10.638          10.638
v  Pressure               -291.96          372.49          127.59          127.59
v  k                       0.1209          57.713          3.7614          3.7614
v  epsilon                0.12834            1440            87.2            87.2
v  TurbVisc              0.003196         0.24362        0.023735        0.023735
v  total_pressure      1.0103e+05       1.017e+05      1.0145e+05      1.0145e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3942.8          952.43          952.43


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655000E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.19438E-01 0.27619E+02
   Friction velocity        uet   :  0.10136E-02 0.14243E+01
   Friction velocity        uk    :  0.32900E+00 0.24778E+01
   Dimensionless distance   yplus :  0.52973E+03 0.39896E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44727E+02      39   0.25391E-01   0.16569E+02 0.88235E+01 
c  Velocity[X]                                      0.30411E+01 
c  Velocity[Y]                                      0.17553E+00 
c  Velocity[Z]                                      0.13352E+02 
c  Pressure     0.19298E-01     102   0.88704E-08   0.23612E+00 0.86937E+01 
c  k            0.55027E+02      37   0.13303E-02   0.92253E+02 0.27800E+02 
c  epsilon      0.14514E+04      34   0.40186E-02   0.84701E+05 0.33205E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.1603          16.339      -0.0012349      -0.0012349
v  Velocity[Y]            -4.0695          4.0647     -5.7659e-06     -5.7659e-06
v  Velocity[Z]            -15.163          32.654          10.001          10.001
v  ǁVelocityǁ             0.23766          32.656          10.647          10.647
v  Pressure               -287.63          371.35          126.37          126.37
v  k                      0.12466          58.373          3.8678          3.8678
v  epsilon                0.13891          1471.4          89.887          89.887
v  TurbVisc             0.0031981         0.24751        0.024217        0.024217
v  total_pressure      1.0104e+05       1.017e+05      1.0145e+05      1.0145e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3989.6          960.27          960.27


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.33346E-01 0.27551E+02
   Friction velocity        uet   :  0.17398E-02 0.14262E+01
   Friction velocity        uk    :  0.33079E+00 0.25026E+01
   Dimensionless distance   yplus :  0.53261E+03 0.40295E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45005E+02      39   0.26593E-01   0.15742E+02 0.85535E+01 
c  Velocity[X]                                      0.29299E+01 
c  Velocity[Y]                                      0.18775E+00 
c  Velocity[Z]                                      0.12624E+02 
c  Pressure     0.21888E-01      93   0.73794E-08   0.26247E+00 0.84450E+01 
c  k            0.56427E+02      37   0.12832E-02   0.91009E+02 0.27150E+02 
c  epsilon      0.14920E+04      34   0.38628E-02   0.83402E+05 0.32269E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.0533           16.61     -0.00082611     -0.00082611
v  Velocity[Y]            -4.2469          4.2576      2.5304e-06      2.5304e-06
v  Velocity[Z]            -15.086          32.616          10.001          10.001
v  ǁVelocityǁ             0.21434          32.618          10.655          10.655
v  Pressure               -283.33          369.04          124.83          124.83
v  k                      0.12933          59.114          3.9742          3.9742
v  epsilon                0.15053          1498.5          92.556          92.556
v  TurbVisc             0.0032029         0.25098        0.024715        0.024715
v  total_pressure      1.0104e+05      1.0169e+05      1.0145e+05      1.0145e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4029.5          968.22          968.22


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.62678E-02 0.27470E+02
   Friction velocity        uet   :  0.32620E-03 0.14278E+01
   Friction velocity        uk    :  0.33247E+00 0.25202E+01
   Dimensionless distance   yplus :  0.53531E+03 0.40579E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45281E+02      39   0.26155E-01   0.15496E+02 0.84873E+01 
c  Velocity[X]                                      0.30095E+01 
c  Velocity[Y]                                      0.18947E+00 
c  Velocity[Z]                                      0.12297E+02 
c  Pressure     0.21216E-01     105   0.67658E-08   0.25327E+00 0.81408E+01 
c  k            0.57771E+02      37   0.12400E-02   0.89816E+02 0.26534E+02 
c  epsilon      0.15304E+04      34   0.37110E-02   0.81884E+05 0.31345E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.965          16.347     -0.00030012     -0.00030012
v  Velocity[Y]            -4.4443          4.4481      3.1967e-06      3.1967e-06
v  Velocity[Z]            -14.991          32.505              10              10
v  ǁVelocityǁ            0.085415          32.507          10.662          10.662
v  Pressure               -278.66          367.65          123.47          123.47
v  k                      0.13512          59.737          4.0801          4.0801
v  epsilon                0.16476          1518.5          95.188          95.188
v  TurbVisc             0.0032084         0.25469        0.025225        0.025225
v  total_pressure      1.0105e+05      1.0169e+05      1.0145e+05      1.0145e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4057.9          976.27          976.27


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.31838E-01 0.27369E+02
   Friction velocity        uet   :  0.16465E-02 0.14282E+01
   Friction velocity        uk    :  0.33400E+00 0.25367E+01
   Dimensionless distance   yplus :  0.53779E+03 0.40844E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45549E+02      39   0.26307E-01   0.14446E+02 0.81577E+01 
c  Velocity[X]                                      0.26515E+01 
c  Velocity[Y]                                      0.18606E+00 
c  Velocity[Z]                                      0.11608E+02 
c  Pressure     0.19873E-01     101   0.80704E-08   0.23497E+00 0.77421E+01 
c  k            0.59052E+02      37   0.11981E-02   0.88433E+02 0.25913E+02 
c  epsilon      0.15663E+04      34   0.35652E-02   0.79992E+05 0.30397E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.8717          16.292      0.00031265      0.00031265
v  Velocity[Y]            -4.6307          4.6245     -4.6279e-06     -4.6279e-06
v  Velocity[Z]            -14.856          32.434              10              10
v  ǁVelocityǁ             0.20531          32.436          10.668          10.668
v  Pressure               -273.27          366.92          122.49          122.49
v  k                      0.14186          60.187          4.1852          4.1852
v  epsilon                0.18179          1540.5          97.771          97.771
v  TurbVisc             0.0032116         0.25772        0.025747        0.025747
v  total_pressure      1.0105e+05      1.0169e+05      1.0145e+05      1.0145e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4084.4          984.44          984.44


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.12043E-01 0.27280E+02
   Friction velocity        uet   :  0.62264E-03 0.14280E+01
   Friction velocity        uk    :  0.33532E+00 0.25465E+01
   Dimensionless distance   yplus :  0.53991E+03 0.41003E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45798E+02      39   0.24724E-01   0.13911E+02 0.79623E+01 
c  Velocity[X]                                      0.27405E+01 
c  Velocity[Y]                                      0.18277E+00 
c  Velocity[Z]                                      0.10987E+02 
c  Pressure     0.21400E-01      97   0.63437E-08   0.25105E+00 0.75696E+01 
c  k            0.60260E+02      37   0.11575E-02   0.86928E+02 0.25299E+02 
c  epsilon      0.15995E+04      34   0.34202E-02   0.77767E+05 0.29444E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.7835          16.585       0.0010838       0.0010838
v  Velocity[Y]            -4.7276            4.76       4.281e-06       4.281e-06
v  Velocity[Z]            -14.725          32.296              10              10
v  ǁVelocityǁ             0.25763          32.299          10.674          10.674
v  Pressure               -268.46          364.34          121.07          121.07
v  k                      0.14902          60.654          4.2893          4.2893
v  epsilon                 0.2009          1555.3           100.3           100.3
v  TurbVisc             0.0032238         0.26054        0.026279        0.026279
v  total_pressure      1.0106e+05      1.0169e+05      1.0145e+05      1.0145e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4100.3          992.67          992.67


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.74216E-01 0.27142E+02
   Friction velocity        uet   :  0.38181E-02 0.14263E+01
   Friction velocity        uk    :  0.33587E+00 0.25551E+01
   Dimensionless distance   yplus :  0.54079E+03 0.41140E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         36, Physical time    0.36000E+02


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

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

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

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

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46054E+02      39   0.26555E-01   0.13134E+02 0.77208E+01 
c  Velocity[X]                                      0.25464E+01 
c  Velocity[Y]                                      0.18038E+00 
c  Velocity[Z]                                      0.10408E+02 
c  Pressure     0.19943E-01     110   0.88604E-08   0.22806E+00 0.71537E+01 
c  k            0.61385E+02      37   0.11208E-02   0.85391E+02 0.24704E+02 
c  epsilon      0.16298E+04      34   0.32853E-02   0.75396E+05 0.28507E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.6871          16.414       0.0019926       0.0019926
v  Velocity[Y]            -4.8176          4.8223     -5.8122e-06     -5.8122e-06
v  Velocity[Z]            -14.574          32.181              10              10
v  ǁVelocityǁ             0.21838          32.183          10.679          10.679
v  Pressure               -263.14          363.87          120.18          120.18
v  k                      0.15781          60.979           4.392           4.392
v  epsilon                0.22183          1566.5          102.76          102.76
v  TurbVisc             0.0032433         0.26311        0.026817        0.026817
v  total_pressure      1.0106e+05      1.0169e+05      1.0145e+05      1.0145e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0            4114            1001            1001


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.26267E-01 0.27018E+02
   Friction velocity        uet   :  0.13506E-02 0.14242E+01
   Friction velocity        uk    :  0.33623E+00 0.25582E+01
   Dimensionless distance   yplus :  0.54137E+03 0.41190E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46293E+02      39   0.25372E-01   0.12807E+02 0.76401E+01 
c  Velocity[X]                                      0.24376E+01 
c  Velocity[Y]                                      0.17655E+00 
c  Velocity[Z]                                      0.10193E+02 
c  Pressure     0.20749E-01      81   0.64435E-08   0.23842E+00 0.69816E+01 
c  k            0.62430E+02      37   0.10835E-02   0.83662E+02 0.24111E+02 
c  epsilon      0.16570E+04      34   0.31483E-02   0.72729E+05 0.27575E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.592          16.356       0.0030311       0.0030311
v  Velocity[Y]            -4.8972          4.8929      4.2074e-06      4.2074e-06
v  Velocity[Z]            -14.402          32.032          9.9999          9.9999
v  ǁVelocityǁ             0.19154          32.034          10.683          10.683
v  Pressure               -257.77          361.64          118.84          118.84
v  k                      0.16938          61.115          4.4929          4.4929
v  epsilon                0.24527          1575.9          105.13          105.13
v  TurbVisc             0.0032589         0.26504        0.027359        0.027359
v  total_pressure      1.0107e+05      1.0169e+05      1.0144e+05      1.0144e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0            4119          1009.3          1009.3


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.76209E-01 0.26888E+02
   Friction velocity        uet   :  0.43949E-02 0.14209E+01
   Friction velocity        uk    :  0.33715E+00 0.25608E+01
   Dimensionless distance   yplus :  0.54286E+03 0.41232E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46510E+02      39   0.22627E-01   0.12209E+02 0.74161E+01 
c  Velocity[X]                                      0.25343E+01 
c  Velocity[Y]                                      0.17519E+00 
c  Velocity[Z]                                      0.94994E+01 
c  Pressure     0.19808E-01     105   0.71869E-08   0.22616E+00 0.65731E+01 
c  k            0.63383E+02      37   0.10499E-02   0.81890E+02 0.23535E+02 
c  epsilon      0.16807E+04      34   0.30249E-02   0.70012E+05 0.26673E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4993           16.67       0.0042736       0.0042736
v  Velocity[Y]            -4.9809          4.9856      5.7202e-07      5.7202e-07
v  Velocity[Z]             -14.23           31.89          9.9999          9.9999
v  ǁVelocityǁ             0.20373          31.892          10.686          10.686
v  Pressure               -252.52          359.72          117.88          117.88
v  k                      0.18314          61.284          4.5918          4.5918
v  epsilon                0.27055          1578.6          107.42          107.42
v  TurbVisc             0.0032744         0.26709        0.027904        0.027904
v  total_pressure      1.0107e+05      1.0168e+05      1.0144e+05      1.0144e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4123.2          1017.6          1017.6


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.51218E-01 0.26766E+02
   Friction velocity        uet   :  0.26214E-02 0.14165E+01
   Friction velocity        uk    :  0.33847E+00 0.25578E+01
   Dimensionless distance   yplus :  0.54499E+03 0.41184E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46750E+02      39   0.24061E-01   0.11261E+02 0.70817E+01 
c  Velocity[X]                                      0.21086E+01 
c  Velocity[Y]                                      0.18055E+00 
c  Velocity[Z]                                      0.89721E+01 
c  Pressure     0.18848E-01      97   0.62017E-08   0.21214E+00 0.62534E+01 
c  k            0.64249E+02      37   0.10187E-02   0.80012E+02 0.22971E+02 
c  epsilon      0.17014E+04      34   0.29125E-02   0.67199E+05 0.25794E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4116          16.466       0.0056983       0.0056983
v  Velocity[Y]            -5.0601            5.06     -7.7729e-07     -7.7729e-07
v  Velocity[Z]            -14.059          31.723          9.9998          9.9998
v  ǁVelocityǁ             0.22971          31.725          10.689          10.689
v  Pressure               -247.89          359.27          117.22          117.22
v  k                      0.19593          61.486          4.6885          4.6885
v  epsilon                0.29806          1579.2          109.61          109.61
v  TurbVisc             0.0032958         0.26834         0.02845         0.02845
v  total_pressure      1.0108e+05      1.0168e+05      1.0144e+05      1.0144e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4118.4            1026            1026


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.60794E-01 0.26596E+02
   Friction velocity        uet   :  0.31119E-02 0.14118E+01
   Friction velocity        uk    :  0.34000E+00 0.25550E+01
   Dimensionless distance   yplus :  0.54745E+03 0.41139E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46961E+02      39   0.24989E-01   0.11016E+02 0.70143E+01 
c  Velocity[X]                                      0.22345E+01 
c  Velocity[Y]                                      0.16706E+00 
c  Velocity[Z]                                      0.86149E+01 
c  Pressure     0.19300E-01      93   0.66487E-08   0.21969E+00 0.60289E+01 
c  k            0.65032E+02      37   0.98820E-03   0.77993E+02 0.22413E+02 
c  epsilon      0.17190E+04      34   0.28101E-02   0.64339E+05 0.24945E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.3254          16.525       0.0072601       0.0072601
v  Velocity[Y]            -5.0867          5.1011      5.5858e-07      5.5858e-07
v  Velocity[Z]            -13.899          31.554          9.9998          9.9998
v  ǁVelocityǁ             0.21495          31.556          10.692          10.692
v  Pressure               -244.62          357.36          116.17          116.17
v  k                      0.20519          61.505          4.7832          4.7832
v  epsilon                 0.3267          1577.1          111.71          111.71
v  TurbVisc             0.0032987         0.26972        0.028994        0.028994
v  total_pressure      1.0108e+05      1.0168e+05      1.0144e+05      1.0144e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4113.9          1034.3          1034.3


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.83442E-01 0.26472E+02
   Friction velocity        uet   :  0.42934E-02 0.14066E+01
   Friction velocity        uk    :  0.34212E+00 0.25479E+01
   Dimensionless distance   yplus :  0.55086E+03 0.41024E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47168E+02      38   0.22861E-01   0.10615E+02 0.68225E+01 
c  Velocity[X]                                      0.22157E+01 
c  Velocity[Y]                                      0.18175E+00 
c  Velocity[Z]                                      0.82172E+01 
c  Pressure     0.19858E-01      97   0.89222E-08   0.22618E+00 0.62675E+01 
c  k            0.65727E+02      37   0.96050E-03   0.75957E+02 0.21872E+02 
c  epsilon      0.17333E+04      34   0.27219E-02   0.61518E+05 0.24133E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.2418          16.322       0.0089255       0.0089255
v  Velocity[Y]             -5.126          5.1447     -1.9673e-06     -1.9673e-06
v  Velocity[Z]            -13.749          31.375          9.9996          9.9996
v  ǁVelocityǁ             0.17939          31.377          10.694          10.694
v  Pressure               -241.94          352.53           114.4           114.4
v  k                      0.20897          61.531          4.8755          4.8755
v  epsilon                0.35716          1570.5          113.71          113.71
v  TurbVisc             0.0032969         0.27045        0.029535        0.029535
v  total_pressure      1.0108e+05      1.0168e+05      1.0144e+05      1.0144e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4102.4          1042.6          1042.6


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.16603E-01 0.26293E+02
   Friction velocity        uet   :  0.84681E-03 0.14020E+01
   Friction velocity        uk    :  0.34476E+00 0.25397E+01
   Dimensionless distance   yplus :  0.55511E+03 0.40893E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47367E+02      38   0.23318E-01   0.98945E+01 0.65808E+01 
c  Velocity[X]                                      0.19659E+01 
c  Velocity[Y]                                      0.17047E+00 
c  Velocity[Z]                                      0.77581E+01 
c  Pressure     0.18186E-01      93   0.89663E-08   0.20221E+00 0.55396E+01 
c  k            0.66344E+02      37   0.93431E-03   0.73815E+02 0.21338E+02 
c  epsilon      0.17449E+04      34   0.26408E-02   0.58663E+05 0.23342E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.1601          16.191        0.010704        0.010704
v  Velocity[Y]            -5.1749          5.1646     -1.5531e-05     -1.5531e-05
v  Velocity[Z]            -13.601          31.203          9.9997          9.9997
v  ǁVelocityǁ             0.16126          31.205          10.694          10.694
v  Pressure                  -240          354.27           114.7           114.7
v  k                      0.21311          61.406          4.9652          4.9652
v  epsilon                0.38675          1560.9          115.61          115.61
v  TurbVisc             0.0032937         0.27113        0.030071        0.030071
v  total_pressure      1.0109e+05      1.0168e+05      1.0144e+05      1.0144e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4089.3          1050.8          1050.8


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.74504E-01 0.26138E+02
   Friction velocity        uet   :  0.38064E-02 0.13991E+01
   Friction velocity        uk    :  0.34716E+00 0.25296E+01
   Dimensionless distance   yplus :  0.55898E+03 0.40730E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47564E+02      38   0.24476E-01   0.93378E+01 0.64253E+01 
c  Velocity[X]                                      0.19494E+01 
c  Velocity[Y]                                      0.16252E+00 
c  Velocity[Z]                                      0.72259E+01 
c  Pressure     0.18502E-01      89   0.84774E-08   0.20779E+00 0.53205E+01 
c  k            0.66885E+02      37   0.90866E-03   0.71558E+02 0.20808E+02 
c  epsilon      0.17538E+04      34   0.25633E-02   0.55774E+05 0.22571E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.0807          16.245        0.012534        0.012534
v  Velocity[Y]            -5.2414          5.2214     -9.4175e-06     -9.4175e-06
v  Velocity[Z]             -13.47          31.023          9.9996          9.9996
v  ǁVelocityǁ             0.15107          31.025          10.695          10.695
v  Pressure               -238.59          351.13          113.52          113.52
v  k                      0.21811          61.172          5.0523          5.0523
v  epsilon                0.41586          1551.2          117.41          117.41
v  TurbVisc              0.003293         0.27136          0.0306          0.0306
v  total_pressure      1.0109e+05      1.0168e+05      1.0144e+05      1.0144e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0            4073            1059            1059


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.68661E-01 0.25980E+02
   Friction velocity        uet   :  0.34913E-02 0.13968E+01
   Friction velocity        uk    :  0.34995E+00 0.25181E+01
   Dimensionless distance   yplus :  0.56347E+03 0.40544E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47756E+02      38   0.22723E-01   0.92194E+01 0.63015E+01 
c  Velocity[X]                                      0.19732E+01 
c  Velocity[Y]                                      0.17370E+00 
c  Velocity[Z]                                      0.70726E+01 
c  Pressure     0.20278E-01      85   0.67221E-08   0.22687E+00 0.54888E+01 
c  k            0.67354E+02      37   0.88353E-03   0.69246E+02 0.20289E+02 
c  epsilon      0.17601E+04      34   0.24931E-02   0.52947E+05 0.21831E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.004          16.375        0.014412        0.014412
v  Velocity[Y]            -5.2516          5.2722     -1.0702e-05     -1.0702e-05
v  Velocity[Z]            -13.361          30.894          9.9994          9.9994
v  ǁVelocityǁ             0.14729          30.896          10.695          10.695
v  Pressure               -237.91          346.53          111.91          111.91
v  k                      0.22342          60.923          5.1368          5.1368
v  epsilon                0.44372          1538.8          119.11          119.11
v  TurbVisc             0.0032971         0.27146         0.03112         0.03112
v  total_pressure      1.0109e+05      1.0167e+05      1.0144e+05      1.0144e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4054.4          1067.1          1067.1


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.30593E-01 0.25818E+02
   Friction velocity        uet   :  0.15565E-02 0.13949E+01
   Friction velocity        uk    :  0.35293E+00 0.25059E+01
   Dimensionless distance   yplus :  0.56827E+03 0.40349E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47915E+02      38   0.20960E-01   0.83972E+01 0.60089E+01 
c  Velocity[X]                                      0.19304E+01 
c  Velocity[Y]                                      0.16017E+00 
c  Velocity[Z]                                      0.63067E+01 
c  Pressure     0.17754E-01      77   0.78944E-08   0.19798E+00 0.49358E+01 
c  k            0.67752E+02      37   0.85932E-03   0.66821E+02 0.19768E+02 
c  epsilon      0.17642E+04      34   0.24208E-02   0.50081E+05 0.21102E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.93          16.301        0.016353        0.016353
v  Velocity[Y]            -5.3114          5.3354     -9.8815e-06     -9.8815e-06
v  Velocity[Z]            -13.258          30.827          9.9997          9.9997
v  ǁVelocityǁ             0.14666          30.829          10.695          10.695
v  Pressure               -237.34          348.35          112.55          112.55
v  k                      0.22937           60.54          5.2186          5.2186
v  epsilon                0.47024          1524.8          120.72          120.72
v  TurbVisc             0.0032625          0.2712         0.03163         0.03163
v  total_pressure      1.0109e+05      1.0167e+05      1.0144e+05      1.0144e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4034.9            1075            1075


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.58759E-01 0.25668E+02
   Friction velocity        uet   :  0.29957E-02 0.13932E+01
   Friction velocity        uk    :  0.35597E+00 0.24921E+01
   Dimensionless distance   yplus :  0.57316E+03 0.40127E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48090E+02      38   0.24923E-01   0.77862E+01 0.58338E+01 
c  Velocity[X]                                      0.16786E+01 
c  Velocity[Y]                                      0.15470E+00 
c  Velocity[Z]                                      0.59529E+01 
c  Pressure     0.17214E-01      85   0.71195E-08   0.19249E+00 0.42957E+01 
c  k            0.68081E+02      37   0.83589E-03   0.64382E+02 0.19260E+02 
c  epsilon      0.17658E+04      34   0.23562E-02   0.47333E+05 0.20407E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.8586          16.193        0.018227        0.018227
v  Velocity[Y]            -5.2431          5.2552     -1.6135e-05     -1.6135e-05
v  Velocity[Z]            -13.157          30.797          9.9996          9.9996
v  ǁVelocityǁ             0.14515          30.799          10.694          10.694
v  Pressure               -236.89          347.28             112             112
v  k                      0.23642          60.138          5.2977          5.2977
v  epsilon                0.49408          1509.8          122.24          122.24
v  TurbVisc             0.0033186         0.27085        0.032129        0.032129
v  total_pressure      1.0109e+05      1.0167e+05      1.0144e+05      1.0144e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          4012.7          1082.8          1082.8


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.64340E-01 0.25672E+02
   Friction velocity        uet   :  0.32657E-02 0.13920E+01
   Friction velocity        uk    :  0.35888E+00 0.24785E+01
   Dimensionless distance   yplus :  0.57784E+03 0.39907E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48259E+02      38   0.21237E-01   0.82187E+01 0.59454E+01 
c  Velocity[X]                                      0.17905E+01 
c  Velocity[Y]                                      0.17143E+00 
c  Velocity[Z]                                      0.62567E+01 
c  Pressure     0.20194E-01      86   0.88742E-08   0.22557E+00 0.60260E+01 
c  k            0.68349E+02      37   0.81202E-03   0.61792E+02 0.18741E+02 
c  epsilon      0.17658E+04      34   0.22869E-02   0.44525E+05 0.19709E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.7923          16.328        0.020057        0.020057
v  Velocity[Y]            -5.2651          5.2781     -2.0789e-05     -2.0789e-05
v  Velocity[Z]            -13.073          30.776          9.9993          9.9993
v  ǁVelocityǁ             0.14301          30.777          10.693          10.693
v  Pressure               -236.44          341.43           109.6           109.6
v  k                      0.24246          59.687           5.374           5.374
v  epsilon                0.51639          1494.5          123.67          123.67
v  TurbVisc             0.0033381         0.27015        0.032613        0.032613
v  total_pressure      1.0109e+05      1.0167e+05      1.0143e+05      1.0143e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3990.7          1090.6          1090.6


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.30712E-01 0.25677E+02
   Friction velocity        uet   :  0.15599E-02 0.13907E+01
   Friction velocity        uk    :  0.36141E+00 0.24633E+01
   Dimensionless distance   yplus :  0.58192E+03 0.39662E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         48, Physical time    0.48000E+02


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

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

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

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

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48388E+02      38   0.20232E-01   0.70656E+01 0.54858E+01 
c  Velocity[X]                                      0.17022E+01 
c  Velocity[Y]                                      0.14829E+00 
c  Velocity[Z]                                      0.52151E+01 
c  Pressure     0.17090E-01      85   0.75693E-08   0.18965E+00 0.49628E+01 
c  k            0.68554E+02      37   0.78774E-03   0.59133E+02 0.18221E+02 
c  epsilon      0.17638E+04      34   0.22221E-02   0.41788E+05 0.19028E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.7262          16.053        0.021839        0.021839
v  Velocity[Y]            -5.2959          5.2638     -2.6025e-05     -2.6025e-05
v  Velocity[Z]            -13.005          30.753          9.9998          9.9998
v  ǁVelocityǁ             0.13899          30.755          10.692          10.692
v  Pressure               -236.01          345.08          110.97          110.97
v  k                      0.24832          59.158          5.4475          5.4475
v  epsilon                0.53584          1479.4          125.02          125.02
v  TurbVisc             0.0033126         0.26946        0.033084        0.033084
v  total_pressure      1.0109e+05      1.0167e+05      1.0144e+05      1.0144e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3966.2          1098.2          1098.2


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655001E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.42254E-01 0.25682E+02
   Friction velocity        uet   :  0.21511E-02 0.13893E+01
   Friction velocity        uk    :  0.36379E+00 0.24481E+01
   Dimensionless distance   yplus :  0.58574E+03 0.39417E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48552E+02      38   0.24475E-01   0.65768E+01 0.53133E+01 
c  Velocity[X]                                      0.14145E+01 
c  Velocity[Y]                                      0.14769E+00 
c  Velocity[Z]                                      0.50146E+01 
c  Pressure     0.17226E-01      72   0.63907E-08   0.19212E+00 0.44028E+01 
c  k            0.68706E+02      37   0.76369E-03   0.56371E+02 0.17692E+02 
c  epsilon      0.17605E+04      34   0.21542E-02   0.39055E+05 0.18347E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.6628          16.184        0.023496        0.023496
v  Velocity[Y]            -5.2742          5.2661      -1.659e-05      -1.659e-05
v  Velocity[Z]            -12.956          30.733          9.9996          9.9996
v  ǁVelocityǁ             0.13501          30.734           10.69           10.69
v  Pressure                -235.7           342.3          109.52          109.52
v  k                      0.25385           58.64          5.5184          5.5184
v  epsilon                0.55129          1464.9           126.3           126.3
v  TurbVisc             0.0033167          0.2684        0.033538        0.033538
v  total_pressure      1.0109e+05      1.0167e+05      1.0143e+05      1.0143e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3941.7          1105.6          1105.6


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.294655000E+01
Smooth wall               5        8100         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3         100         0.294655000E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.64206E-01 0.25691E+02
   Friction velocity        uet   :  0.32815E-02 0.13878E+01
   Friction velocity        uk    :  0.36597E+00 0.24322E+01
   Dimensionless distance   yplus :  0.58926E+03 0.39162E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       8100
------------------------------------------------------------




 Write final restart files
   checkpoint at iteration         50, Physical time    0.50000E+02


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

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

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

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

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      Drift  Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48678E+02      38   0.21141E-01   0.71333E+01 0.54704E+01 
c  Velocity[X]                                      0.16599E+01 
c  Velocity[Y]                                      0.16487E+00 
c  Velocity[Z]                                      0.53085E+01 
c  Pressure     0.21081E-01      74   0.94113E-08   0.23712E+00 0.40714E+01 
c  k            0.68806E+02      37   0.73931E-03   0.53520E+02 0.17152E+02 
c  epsilon      0.17557E+04      34   0.20867E-02   0.36366E+05 0.17667E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.6067          16.248        0.025052        0.025052
v  Velocity[Y]            -5.2158           5.267     -2.2183e-05     -2.2183e-05
v  Velocity[Z]            -12.914          30.712          9.9996          9.9996
v  ǁVelocityǁ             0.13081          30.713          10.688          10.688
v  Pressure               -235.31          338.65          108.21          108.21
v  k                      0.25881          58.094          5.5864          5.5864
v  epsilon                0.56163          1451.3           127.5           127.5
v  TurbVisc             0.0032936         0.26747        0.033977        0.033977
v  total_pressure      1.0109e+05      1.0166e+05      1.0143e+05      1.0143e+05

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

   field         minimum         maximum        set mean    spatial mean
-  -----  --------------  --------------  --------------  --------------
v  Yplus               0          3916.2            1113            1113



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



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


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





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




                      END OF CALCULATION                     
                      ==================                     


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

 Destroying structures and ending computation

 ****************************
  Saving calculation results
 ****************************

