                      Code_Saturne is running
                      ***********************

 Version: 4.0
 Path:    /usr/local

 Result directory:
   /home/lgarelli/RUNS/Code_Saturne/Baffle/Baffle/RESU/20161121-0937


 Single processor Code_Saturne simulation.

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


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


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


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

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

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

                                  (R)
                      Code_Saturne

                      Version 4.0.2


  Copyright (C) 1998-2015 EDF S.A., France

  revision 4.0.2
  build Thu 13 Aug 2015 03:43:53 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 09:37:36 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/20161121-0937
  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            )
       IDEUCH =              1 (0: one-scale model          )
                               (1: two-scale model          )
                               (2: invariant wall function  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.23810E+01 (Limit Y+                    )
       ILOGPO =              1 (0: power law (forbidden for
                                              k-epsilon)    )
                               (1: one-scale log law        )
       IGRHOK =              0 (1: computed Grad(rho k)     )

   - 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
         --           --

 --- 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)
       ipsttb =              0 (Temperature    at boundary)
       ipstnu =              0 (Dimensionless thermal
                                          flux at boundary)


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


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

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


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


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

  -1: name: 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 (0.0516 s)
                                                             
       ALMAX  =    0.13568E+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           0.9749E-06  0.9749E-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  0.3917E-01  0.3917E-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    :  0.13229E-01 0.13229E-01
   Dimensionless distance   yplus :  0.21301E+02 0.21301E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39325E+00      44   0.37088E-01   0.10719E+05 0.10433E+03 
c  Velocity[X]                                      0.11765E+03 
c  Velocity[Y]                                      0.12303E+00 
c  Velocity[Z]                                      0.10601E+05 
c  Pressure     0.22802E+00     410   0.99201E-08   0.10000E+01 0.10662E+03 
c  k            0.27906E+01      47   0.23425E-05   0.19470E+02 0.96890E+02 
c  epsilon      0.50491E+00      49   0.50545E-05   0.79900E+00 0.96244E+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      1.9421e-10      1.9421e-10
v  Velocity[Y]           -0.83231         0.83231     -6.1587e-10     -6.1587e-10
v  Velocity[Z]             1.3196          27.483          9.9841          9.9841
v  ǁVelocityǁ               2.106          30.853          10.047          10.047
v  Pressure                7.3382          3795.6          1903.4          1903.4
v  k                   0.00059287          5.3021        0.065127        0.065127
v  epsilon             9.8836e-07          1.0062        0.014019        0.014019
v  TurbVisc              0.039171        0.039171        0.039171        0.039171
v  total_pressure      1.0133e+05      1.0512e+05      1.0323e+05      1.0323e+05


 TIME FOR THE TIME STEP                1:        0.58634E+00

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


 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         0.294654995E+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 :  0.77447E+00 0.23064E+02
   Friction velocity        uet   :  0.11783E+00 0.21809E+01
   Friction velocity        uk    :  0.14117E-01 0.11992E+01
   Dimensionless distance   yplus :  0.22730E+02 0.19308E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69481E+02      45   0.40760E-01   0.30709E+03 0.82768E+02 
c  Velocity[X]                                      0.11961E+03 
c  Velocity[Y]                                      0.15198E+01 
c  Velocity[Z]                                      0.18596E+03 
c  Pressure     0.23632E+00     368   0.73878E-08   0.10000E+01 0.13806E+04 
c  k            0.35970E+02      39   0.33065E-03   0.46741E+02 0.10558E+04 
c  epsilon      0.79789E+03      43   0.21196E-02   0.80910E+06 0.37847E+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]            -10.376          18.071      -0.0038312      -0.0038312
v  Velocity[Y]            -1.6799          1.6778     -1.0119e-09     -1.0119e-09
v  Velocity[Z]           -0.71226          24.965          10.011          10.011
v  ǁVelocityǁ             0.46132          24.989          10.068          10.068
v  Pressure               -181.36           405.8          110.05          110.05
v  k                   0.00060499          4.3698        0.095273        0.095273
v  epsilon             1.1064e-06          398.31          1.5762          1.5762
v  TurbVisc            5.5198e-05          2.9638        0.040904        0.040904
v  total_pressure      1.0114e+05      1.0173e+05      1.0144e+05      1.0144e+05


 TIME FOR THE TIME STEP                2:        0.47305E+00

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


 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         0.294654994E+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 :  0.12835E+00 0.20125E+02
   Friction velocity        uet   :  0.85569E-02 0.13802E+01
   Friction velocity        uk    :  0.36089E-01 0.10797E+01
   Dimensionless distance   yplus :  0.58108E+02 0.17385E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16564E+03      40   0.31310E-01   0.57316E+03 0.19450E+03 
c  Velocity[X]                                      0.24096E+03 
c  Velocity[Y]                                      0.12490E+02 
c  Velocity[Z]                                      0.31970E+03 
c  Pressure     0.16911E+00     297   0.99507E-08   0.99573E+00 0.88431E+03 
c  k            0.14367E+03      51   0.30714E-02   0.18251E+05 0.11993E+05 
c  epsilon      0.54836E+02      44   0.18774E+00   0.18495E+06 0.30177E+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]            -7.6412          20.096      -0.0025279      -0.0025279
v  Velocity[Y]            -3.1751          3.1792      -2.205e-06      -2.205e-06
v  Velocity[Z]            -4.8551          25.736          10.013          10.013
v  ǁVelocityǁ             0.45427          25.921          10.083          10.083
v  Pressure               -416.57          691.02          237.49          237.49
v  k                   0.00064258          22.865         0.35874         0.35874
v  epsilon             2.8307e-06          155.67          1.2327          1.2327
v  TurbVisc            0.00016128          14.948        0.094158        0.094158
v  total_pressure      1.0091e+05      1.0202e+05      1.0156e+05      1.0156e+05


 TIME FOR THE TIME STEP                3:        0.43202E+00

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


 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         0.294654996E+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 :  0.64071E-01 0.21935E+02
   Friction velocity        uet   :  0.33849E-02 0.12940E+01
   Friction velocity        uk    :  0.60701E-01 0.24429E+01
   Dimensionless distance   yplus :  0.97738E+02 0.39333E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12366E+04      39   0.24502E-01   0.22169E+04 0.11158E+04 
c  Velocity[X]                                      0.11761E+04 
c  Velocity[Y]                                      0.74782E+02 
c  Velocity[Z]                                      0.96603E+03 
c  Pressure     0.14997E+00     270   0.91901E-08   0.11131E+01 0.14102E+05 
c  k            0.17865E+04      48   0.20638E-03   0.70570E+05 0.27274E+05 
c  epsilon      0.17468E+05      49   0.28558E-02   0.88471E+08 0.25730E+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]            -7.3165          16.389      -0.0015993      -0.0015993
v  Velocity[Y]            -5.4159           5.418      3.8842e-07      3.8842e-07
v  Velocity[Z]            -7.6216          41.803          10.007          10.007
v  ǁVelocityǁ             0.83329          41.805          10.106          10.106
v  Pressure               -1892.6          6967.7          1356.5          1356.5
v  k                   0.00075357          40.254         0.74901         0.74901
v  epsilon             1.7669e-05          2154.4          6.9015          6.9015
v  TurbVisc            0.00019004          108.55          0.7547          0.7547
v  total_pressure           99432      1.0829e+05      1.0268e+05      1.0268e+05


 TIME FOR THE TIME STEP                4:        0.41216E+00

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


 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         0.294654997E+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 :  0.25786E+00 0.35047E+02
   Friction velocity        uet   :  0.13074E-01 0.18923E+01
   Friction velocity        uk    :  0.83693E-01 0.34751E+01
   Dimensionless distance   yplus :  0.13476E+03 0.55954E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10282E+03      44   0.68867E-01   0.67411E+04 0.40015E+03 
c  Velocity[X]                                      0.40596E+04 
c  Velocity[Y]                                      0.72998E+03 
c  Velocity[Z]                                      0.19515E+04 
c  Pressure     0.12959E+01     284   0.97982E-08   0.16152E+01 0.84571E+03 
c  k            0.64225E+02      46   0.47100E-02   0.18299E+04 0.74455E+03 
c  epsilon      0.14808E+04      46   0.26706E-01   0.11749E+08 0.14404E+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]            -62.181          40.798       -0.015676       -0.015676
v  Velocity[Y]            -25.736          25.717      2.6893e-07      2.6893e-07
v  Velocity[Z]            -26.228          40.737          9.9846          9.9846
v  ǁVelocityǁ             0.81837           62.57          10.301          10.301
v  Pressure               -797.73            2359          841.97          841.97
v  k                    0.0011997          45.625          1.0408          1.0408
v  epsilon             0.00013402          4087.1           14.28           14.28
v  TurbVisc            0.00031082          3.2294         0.14939         0.14939
v  total_pressure      1.0053e+05      1.0368e+05      1.0217e+05      1.0217e+05


 TIME FOR THE TIME STEP                5:        0.51511E+00

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


 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         0.294655028E+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 :  0.76797E-01 0.53533E+02
   Friction velocity        uet   :  0.39261E-02 0.24534E+01
   Friction velocity        uk    :  0.10802E+00 0.36997E+01
   Dimensionless distance   yplus :  0.17392E+03 0.59570E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.60644E+02      45   0.92531E-01   0.18697E+04 0.14163E+03 
c  Velocity[X]                                      0.11824E+04 
c  Velocity[Y]                                      0.10495E+03 
c  Velocity[Z]                                      0.58239E+03 
c  Pressure     0.75365E+00     340   0.76495E-08   0.25244E+01 0.95893E+03 
c  k            0.59721E+02      46   0.42067E-01   0.81455E+04 0.63420E+03 
c  epsilon      0.27126E+04      43   0.82390E-01   0.16412E+08 0.59656E+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]            -24.514          23.727       -0.013402       -0.013402
v  Velocity[Y]            -13.365          13.383     -4.2499e-06     -4.2499e-06
v  Velocity[Z]            -14.514          40.613          9.9916          9.9916
v  ǁVelocityǁ              1.3758          40.616          10.291          10.291
v  Pressure               -759.37          1006.9          326.43          326.43
v  k                    0.0026784          87.634          1.5358          1.5358
v  epsilon             0.00068706          7199.6          30.108          30.108
v  TurbVisc            0.00048992          1.3474        0.079476        0.079476
v  total_pressure      1.0057e+05      1.0233e+05      1.0165e+05      1.0165e+05


 TIME FOR THE TIME STEP                6:        0.48164E+00

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


 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         0.294655008E+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 :  0.23457E+00 0.34471E+02
   Friction velocity        uet   :  0.11285E-01 0.17204E+01
   Friction velocity        uk    :  0.13108E+00 0.50469E+01
   Dimensionless distance   yplus :  0.21106E+03 0.81262E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46664E+02      42   0.76324E-01   0.42804E+03 0.62580E+02 
c  Velocity[X]                                      0.19407E+03 
c  Velocity[Y]                                      0.28464E+02 
c  Velocity[Z]                                      0.20550E+03 
c  Pressure     0.50343E+00     284   0.82710E-08   0.25807E+01 0.38641E+03 
c  k            0.69962E+02      44   0.10780E-01   0.27685E+04 0.27294E+03 
c  epsilon      0.50143E+04      41   0.75086E-01   0.90758E+08 0.52745E+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]            -12.364           20.33      -0.0079713      -0.0079713
v  Velocity[Y]             -8.449          8.4753      3.6596e-06      3.6596e-06
v  Velocity[Z]             -12.51           39.25          9.9953          9.9953
v  ǁVelocityǁ              1.2727          39.256          10.284          10.284
v  Pressure               -585.01          568.12          179.96          179.96
v  k                    0.0052777          149.53          1.8845          1.8845
v  epsilon              0.0018524           27199          55.365          55.365
v  TurbVisc            0.00068488         0.95819         0.04877         0.04877
v  total_pressure      1.0074e+05      1.0189e+05       1.015e+05       1.015e+05


 TIME FOR THE TIME STEP                7:        0.43882E+00

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


 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         0.294655004E+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 :  0.43115E+00 0.33372E+02
   Friction velocity        uet   :  0.22645E-01 0.16474E+01
   Friction velocity        uk    :  0.15241E+00 0.66977E+01
   Dimensionless distance   yplus :  0.24540E+03 0.10784E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41492E+02      42   0.70277E-01   0.24798E+03 0.45057E+02 
c  Velocity[X]                                      0.87219E+02 
c  Velocity[Y]                                      0.13604E+02 
c  Velocity[Z]                                      0.14716E+03 
c  Pressure     0.36182E+00     271   0.76254E-08   0.23064E+01 0.77149E+02 
c  k            0.58249E+02      42   0.18621E-01   0.14459E+04 0.18584E+03 
c  epsilon      0.64778E+04      38   0.23010E-01   0.47816E+07 0.12072E+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]            -9.1352          17.623      -0.0049404      -0.0049404
v  Velocity[Y]            -5.8307          5.8888      8.1066e-06      8.1066e-06
v  Velocity[Z]            -11.929          37.601          9.9984          9.9984
v  ǁVelocityǁ              1.0653          37.609           10.28           10.28
v  Pressure                  -419           438.5          152.49          152.49
v  k                    0.0089177          110.46          2.0438          2.0438
v  epsilon              0.0037562           30040          63.722          63.722
v  TurbVisc             0.0010443         0.68774        0.037324        0.037324
v  total_pressure      1.0091e+05      1.0176e+05      1.0148e+05      1.0148e+05


 TIME FOR THE TIME STEP                8:        0.43219E+00

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


 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         0.294655004E+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 :  0.21079E+00 0.31650E+02
   Friction velocity        uet   :  0.95859E-02 0.15709E+01
   Friction velocity        uk    :  0.17202E+00 0.57565E+01
   Dimensionless distance   yplus :  0.27697E+03 0.92688E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39437E+02      42   0.61044E-01   0.17048E+03 0.36300E+02 
c  Velocity[X]                                      0.53376E+02 
c  Velocity[Y]                                      0.84779E+01 
c  Velocity[Z]                                      0.10862E+03 
c  Pressure     0.27437E+00     257   0.83747E-08   0.22114E+01 0.26098E+02 
c  k            0.49264E+02      42   0.38821E-01   0.13757E+04 0.17038E+03 
c  epsilon      0.46193E+04      38   0.17452E+00   0.15313E+08 0.21244E+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]            -7.9438          15.639      -0.0037192      -0.0037192
v  Velocity[Y]            -4.2058           4.201      4.4781e-06      4.4781e-06
v  Velocity[Z]            -11.956          36.107          9.9995          9.9995
v  ǁVelocityǁ             0.74765          36.117          10.284          10.284
v  Pressure               -342.27          377.62           144.6           144.6
v  k                     0.013624          66.464          2.1169          2.1169
v  epsilon              0.0064638           15583          60.681          60.681
v  TurbVisc             0.0013124         0.54841        0.031374        0.031374
v  total_pressure      1.0098e+05       1.017e+05      1.0147e+05      1.0147e+05


 TIME FOR THE TIME STEP                9:        0.38787E+00

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


 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         0.294655003E+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 :  0.29715E+00 0.30114E+02
   Friction velocity        uet   :  0.15085E-01 0.15055E+01
   Friction velocity        uk    :  0.18984E+00 0.43866E+01
   Dimensionless distance   yplus :  0.30567E+03 0.70630E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38470E+02      42   0.54423E-01   0.13447E+03 0.31580E+02 
c  Velocity[X]                                      0.39347E+02 
c  Velocity[Y]                                      0.62682E+01 
c  Velocity[Z]                                      0.88854E+02 
c  Pressure     0.21632E+00     243   0.67285E-08   0.20852E+01 0.15056E+02 
c  k            0.44721E+02      41   0.29249E-01   0.95767E+03 0.14616E+03 
c  epsilon      0.27044E+04      38   0.20043E+00   0.66547E+07 0.20646E+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]            -7.0128          14.612      -0.0032028      -0.0032028
v  Velocity[Y]            -3.4885           3.497      1.6996e-07      1.6996e-07
v  Velocity[Z]            -11.893          34.699              10              10
v  ǁVelocityǁ             0.60335          34.709          10.294          10.294
v  Pressure               -316.28          352.25          144.76          144.76
v  k                     0.019056          46.569          2.1673          2.1673
v  epsilon              0.0099699          6273.4          57.247          57.247
v  TurbVisc             0.0015356         0.45153        0.027787        0.027787
v  total_pressure      1.0101e+05      1.0168e+05      1.0147e+05      1.0147e+05


 TIME FOR THE TIME STEP               10:        0.36561E+00

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


 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         0.294655002E+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 :  0.17760E+00 0.28728E+02
   Friction velocity        uet   :  0.98766E-02 0.14465E+01
   Friction velocity        uk    :  0.20579E+00 0.37116E+01
   Dimensionless distance   yplus :  0.33136E+03 0.59762E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38084E+02      41   0.48493E-01   0.10827E+03 0.27886E+02 
c  Velocity[X]                                      0.28631E+02 
c  Velocity[Y]                                      0.47470E+01 
c  Velocity[Z]                                      0.74890E+02 
c  Pressure     0.17863E+00     228   0.99353E-08   0.19289E+01 0.16828E+02 
c  k            0.42502E+02      41   0.16951E-01   0.69215E+03 0.12596E+03 
c  epsilon      0.18554E+04      38   0.12945E+00   0.27493E+07 0.19674E+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]             -6.496          14.897      -0.0030364      -0.0030364
v  Velocity[Y]             -3.102          3.1072      1.7503e-06      1.7503e-06
v  Velocity[Z]            -11.893           33.34              10              10
v  ǁVelocityǁ             0.48186          33.349          10.309          10.309
v  Pressure               -301.52           346.2          147.93          147.93
v  k                     0.025294          38.127          2.2149          2.2149
v  epsilon               0.014207          3914.3          55.594          55.594
v  TurbVisc             0.0017694         0.37731        0.025424        0.025424
v  total_pressure      1.0102e+05      1.0167e+05      1.0147e+05      1.0147e+05


 TIME FOR THE TIME STEP               11:        0.42293E+00

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


 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         0.294655002E+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 :  0.61855E-01 0.27429E+02
   Friction velocity        uet   :  0.32382E-02 0.13916E+01
   Friction velocity        uk    :  0.21995E+00 0.30659E+01
   Dimensionless distance   yplus :  0.35415E+03 0.49365E+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


 Time for restart files:    0.11910E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.37963E+02      41   0.44512E-01   0.93135E+02 0.25391E+02 
c  Velocity[X]                                      0.23100E+02 
c  Velocity[Y]                                      0.40750E+01 
c  Velocity[Z]                                      0.65961E+02 
c  Pressure     0.14567E+00     187   0.94326E-08   0.17472E+01 0.16763E+02 
c  k            0.41310E+02      41   0.98129E-02   0.52548E+03 0.10873E+03 
c  epsilon      0.15035E+04      38   0.66956E-01   0.14131E+07 0.17077E+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]            -6.2008          15.435      -0.0031389      -0.0031389
v  Velocity[Y]             -3.334          3.4037     -9.5025e-07     -9.5025e-07
v  Velocity[Z]            -12.135          32.073          10.001          10.001
v  ǁVelocityǁ             0.47109          32.084          10.327          10.327
v  Pressure               -298.86          358.94          151.64          151.64
v  k                     0.031851          38.868          2.2645          2.2645
v  epsilon                 0.0191          2410.1          55.281          55.281
v  TurbVisc             0.0020088         0.31801        0.023783        0.023783
v  total_pressure      1.0103e+05      1.0168e+05      1.0148e+05      1.0148e+05


 TIME FOR THE TIME STEP               12:        0.37845E+00

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


 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         0.294654998E+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 :  0.17500E+00 0.26990E+02
   Friction velocity        uet   :  0.13807E-01 0.13414E+01
   Friction velocity        uk    :  0.23268E+00 0.26491E+01
   Dimensionless distance   yplus :  0.37465E+03 0.42654E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38028E+02      41   0.40818E-01   0.79429E+02 0.23056E+02 
c  Velocity[X]                                      0.16414E+02 
c  Velocity[Y]                                      0.34938E+01 
c  Velocity[Z]                                      0.59521E+02 
c  Pressure     0.10623E+00     201   0.90128E-08   0.13563E+01 0.15212E+02 
c  k            0.40599E+02      40   0.64064E-02   0.42133E+03 0.95596E+02 
c  epsilon      0.13419E+04      37   0.35133E-01   0.83357E+06 0.14168E+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]            -5.8479          15.843       -0.003269       -0.003269
v  Velocity[Y]            -3.9207          3.9703      -8.691e-07      -8.691e-07
v  Velocity[Z]            -12.255          31.386          10.002          10.002
v  ǁVelocityǁ             0.37925          31.408          10.347          10.347
v  Pressure               -298.68           376.9          154.35          154.35
v  k                     0.038805          40.445          2.3166          2.3166
v  epsilon               0.024539          1429.3          55.662          55.662
v  TurbVisc             0.0018165         0.27304        0.022614        0.022614
v  total_pressure      1.0103e+05       1.017e+05      1.0148e+05      1.0148e+05


 TIME FOR THE TIME STEP               13:        0.34862E+00

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


 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         0.294655002E+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 :  0.24066E+00 0.26810E+02
   Friction velocity        uet   :  0.15270E-01 0.13026E+01
   Friction velocity        uk    :  0.24437E+00 0.26109E+01
   Dimensionless distance   yplus :  0.39346E+03 0.42040E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38221E+02      41   0.38876E-01   0.68778E+02 0.21141E+02 
c  Velocity[X]                                      0.12971E+02 
c  Velocity[Y]                                      0.31427E+01 
c  Velocity[Z]                                      0.52664E+02 
c  Pressure     0.73034E-01     201   0.93715E-08   0.93231E+00 0.13870E+02 
c  k            0.40166E+02      40   0.48022E-02   0.34961E+03 0.85189E+02 
c  epsilon      0.12567E+04      37   0.21156E-01   0.54683E+06 0.11854E+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]             -5.676          16.042      -0.0032725      -0.0032725
v  Velocity[Y]            -4.2769          4.3139      3.8979e-07      3.8979e-07
v  Velocity[Z]            -12.436          31.081          10.002          10.002
v  ǁVelocityǁ             0.49647          31.095          10.368          10.368
v  Pressure               -299.06          392.31          156.15          156.15
v  k                     0.045931          42.077          2.3714          2.3714
v  epsilon               0.030395          1353.1          56.382          56.382
v  TurbVisc            0.00082672         0.23476        0.021775        0.021775
v  total_pressure      1.0103e+05      1.0172e+05      1.0148e+05      1.0148e+05


 TIME FOR THE TIME STEP               14:        0.34947E+00

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


 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         0.294655002E+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 :  0.14567E+00 0.26561E+02
   Friction velocity        uet   :  0.12625E-01 0.12885E+01
   Friction velocity        uk    :  0.25483E+00 0.25600E+01
   Dimensionless distance   yplus :  0.41031E+03 0.41220E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38493E+02      41   0.38788E-01   0.60437E+02 0.19462E+02 
c  Velocity[X]                                      0.10509E+02 
c  Velocity[Y]                                      0.26727E+01 
c  Velocity[Z]                                      0.47256E+02 
c  Pressure     0.54589E-01     231   0.99291E-08   0.70698E+00 0.12395E+02 
c  k            0.39935E+02      39   0.39726E-02   0.29603E+03 0.76482E+02 
c  epsilon      0.12032E+04      36   0.15273E-01   0.39763E+06 0.10232E+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]             -5.463          16.143      -0.0032032      -0.0032032
v  Velocity[Y]            -3.9988          4.0554       6.033e-06       6.033e-06
v  Velocity[Z]            -12.772          31.012          10.002          10.002
v  ǁVelocityǁ             0.34654          31.019           10.39           10.39
v  Pressure               -303.05          399.58          155.68          155.68
v  k                      0.05305          44.171          2.4295          2.4295
v  epsilon               0.036538            1284          57.281          57.281
v  TurbVisc            0.00034031         0.21393        0.021179        0.021179
v  total_pressure      1.0102e+05      1.0172e+05      1.0148e+05      1.0148e+05


 TIME FOR THE TIME STEP               15:        0.37091E+00

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


 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         0.294655003E+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 :  0.20246E+00 0.26508E+02
   Friction velocity        uet   :  0.15369E-01 0.12896E+01
   Friction velocity        uk    :  0.22743E+00 0.25062E+01
   Dimensionless distance   yplus :  0.36620E+03 0.40353E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.38838E+02      41   0.35201E-01   0.53999E+02 0.18084E+02 
c  Velocity[X]                                      0.85060E+01 
c  Velocity[Y]                                      0.22979E+01 
c  Velocity[Z]                                      0.43195E+02 
c  Pressure     0.47541E-01     257   0.90101E-08   0.62620E+00 0.12386E+02 
c  k            0.39886E+02      39   0.34403E-02   0.25396E+03 0.68897E+02 
c  epsilon      0.11651E+04      36   0.12385E-01   0.31135E+06 0.90673E+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]             -5.238           16.14      -0.0030778      -0.0030778
v  Velocity[Y]            -3.3621          3.2942      5.1541e-06      5.1541e-06
v  Velocity[Z]            -12.981          31.148          10.002          10.002
v  ǁVelocityǁ             0.44187          31.156          10.412          10.412
v  Pressure               -301.13          403.01          154.42          154.42
v  k                     0.059992            45.7          2.4913          2.4913
v  epsilon               0.042893          1218.5          58.307          58.307
v  TurbVisc            0.00018774         0.21405        0.020772        0.020772
v  total_pressure      1.0102e+05      1.0173e+05      1.0148e+05      1.0148e+05


 TIME FOR THE TIME STEP               16:        0.37665E+00

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


 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         0.294655002E+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 :  0.27591E+00 0.26530E+02
   Friction velocity        uet   :  0.19929E-01 0.13011E+01
   Friction velocity        uk    :  0.18173E+00 0.24503E+01
   Dimensionless distance   yplus :  0.29261E+03 0.39453E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39181E+02      41   0.33729E-01   0.47854E+02 0.16736E+02 
c  Velocity[X]                                      0.74145E+01 
c  Velocity[Y]                                      0.19103E+01 
c  Velocity[Z]                                      0.38529E+02 
c  Pressure     0.39021E-01     244   0.92895E-08   0.52699E+00 0.12263E+02 
c  k            0.40000E+02      39   0.30438E-02   0.21921E+03 0.62054E+02 
c  epsilon      0.11375E+04      36   0.10572E-01   0.25235E+06 0.81130E+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]            -5.0937          16.211      -0.0029885      -0.0029885
v  Velocity[Y]            -3.1576          3.2115      5.2613e-06      5.2613e-06
v  Velocity[Z]            -13.381          31.322          10.002          10.002
v  ǁVelocityǁ             0.32306          31.324          10.433          10.433
v  Pressure               -304.55           403.1          153.26          153.26
v  k                     0.066734          47.113          2.5569          2.5569
v  epsilon               0.049346          1152.3          59.445          59.445
v  TurbVisc            0.00018623         0.21558        0.020517        0.020517
v  total_pressure      1.0102e+05      1.0173e+05      1.0148e+05      1.0148e+05


 TIME FOR THE TIME STEP               17:        0.37258E+00

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


 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         0.294655002E+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 :  0.24823E+00 0.26631E+02
   Friction velocity        uet   :  0.13371E-01 0.13181E+01
   Friction velocity        uk    :  0.19773E+00 0.23933E+01
   Dimensionless distance   yplus :  0.31837E+03 0.38536E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.39588E+02      41   0.34046E-01   0.43246E+02 0.15630E+02 
c  Velocity[X]                                      0.67497E+01 
c  Velocity[Y]                                      0.15174E+01 
c  Velocity[Z]                                      0.34979E+02 
c  Pressure     0.35706E-01     271   0.89455E-08   0.50331E+00 0.12736E+02 
c  k            0.40265E+02      39   0.27261E-02   0.19029E+03 0.55934E+02 
c  epsilon      0.11183E+04      36   0.92006E-02   0.20866E+06 0.72941E+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]            -4.8966          16.002      -0.0028561      -0.0028561
v  Velocity[Y]            -2.7775           2.848      1.9801e-06      1.9801e-06
v  Velocity[Z]            -13.658          31.452          10.002          10.002
v  ǁVelocityǁ             0.40257          31.457          10.454          10.454
v  Pressure               -303.35          399.75          150.47          150.47
v  k                     0.073223          48.343          2.6266          2.6266
v  epsilon               0.055783          1173.5          60.703          60.703
v  TurbVisc            0.00035264         0.21694        0.020384        0.020384
v  total_pressure      1.0102e+05      1.0172e+05      1.0148e+05      1.0148e+05


 TIME FOR THE TIME STEP               18:        0.39359E+00

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


 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         0.294655002E+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 :  0.19458E+00 0.26731E+02
   Friction velocity        uet   :  0.10519E-01 0.13362E+01
   Friction velocity        uk    :  0.25145E+00 0.23450E+01
   Dimensionless distance   yplus :  0.40487E+03 0.37758E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40009E+02      41   0.30918E-01   0.38557E+02 0.14545E+02 
c  Velocity[X]                                      0.56795E+01 
c  Velocity[Y]                                      0.11872E+01 
c  Velocity[Z]                                      0.31690E+02 
c  Pressure     0.32773E-01     257   0.93796E-08   0.45835E+00 0.12111E+02 
c  k            0.40698E+02      38   0.24484E-02   0.16593E+03 0.50426E+02 
c  epsilon      0.11075E+04      35   0.80116E-02   0.17417E+06 0.65540E+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]            -4.6919          16.083       -0.002764       -0.002764
v  Velocity[Y]            -2.7271          2.7501      1.1128e-06      1.1128e-06
v  Velocity[Z]            -13.991          31.607          10.002          10.002
v  ǁVelocityǁ             0.29367          31.611          10.474          10.474
v  Pressure               -304.78          398.57          148.87          148.87
v  k                     0.079346          49.342          2.7008          2.7008
v  epsilon               0.062156          1220.9          62.098          62.098
v  TurbVisc            0.00075721         0.21857        0.020354        0.020354
v  total_pressure      1.0102e+05      1.0172e+05      1.0147e+05      1.0147e+05


 TIME FOR THE TIME STEP               19:        0.38215E+00

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


 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         0.294655002E+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 :  0.11197E+00 0.26873E+02
   Friction velocity        uet   :  0.73254E-02 0.13551E+01
   Friction velocity        uk    :  0.29275E+00 0.23006E+01
   Dimensionless distance   yplus :  0.47137E+03 0.37042E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40461E+02      41   0.31719E-01   0.34502E+02 0.13564E+02 
c  Velocity[X]                                      0.50585E+01 
c  Velocity[Y]                                      0.95260E+00 
c  Velocity[Z]                                      0.28491E+02 
c  Pressure     0.28111E-01     257   0.84413E-08   0.39434E+00 0.12198E+02 
c  k            0.41261E+02      38   0.22118E-02   0.14579E+03 0.45592E+02 
c  epsilon      0.11041E+04      35   0.69495E-02   0.14614E+06 0.58743E+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]            -4.5523          16.401      -0.0026526      -0.0026526
v  Velocity[Y]            -2.2719          2.2641      -3.017e-07      -3.017e-07
v  Velocity[Z]            -14.254          31.762          10.002          10.002
v  ǁVelocityǁ             0.25763          31.767          10.493          10.493
v  Pressure               -304.05          395.15           146.6           146.6
v  k                     0.085097          50.297          2.7791          2.7791
v  epsilon               0.068363          1248.9          63.632          63.632
v  TurbVisc             0.0016251         0.22044        0.020411        0.020411
v  total_pressure      1.0102e+05      1.0172e+05      1.0147e+05      1.0147e+05


 TIME FOR THE TIME STEP               20:        0.38515E+00

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


 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         0.294655002E+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 :  0.21569E+00 0.26970E+02
   Friction velocity        uet   :  0.11630E-01 0.13712E+01
   Friction velocity        uk    :  0.29819E+00 0.22682E+01
   Dimensionless distance   yplus :  0.48013E+03 0.36520E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40912E+02      40   0.30351E-01   0.31680E+02 0.12808E+02 
c  Velocity[X]                                      0.48488E+01 
c  Velocity[Y]                                      0.78019E+00 
c  Velocity[Z]                                      0.26051E+02 
c  Pressure     0.27422E-01     285   0.78381E-08   0.38287E+00 0.11953E+02 
c  k            0.41990E+02      38   0.20109E-02   0.12958E+03 0.41449E+02 
c  epsilon      0.11089E+04      35   0.60111E-02   0.12347E+06 0.52598E+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]            -4.3808          16.224      -0.0025351      -0.0025351
v  Velocity[Y]            -2.3398          2.4913     -5.4748e-08     -5.4748e-08
v  Velocity[Z]            -14.396          31.994          10.002          10.002
v  ǁVelocityǁ             0.26751          31.997          10.512          10.512
v  Pressure               -305.24          392.03          144.23          144.23
v  k                     0.090474          51.087          2.8621          2.8621
v  epsilon               0.074335          1280.6          65.343          65.343
v  TurbVisc             0.0027607          0.2219        0.020541        0.020541
v  total_pressure      1.0102e+05      1.0172e+05      1.0147e+05      1.0147e+05


 TIME FOR THE TIME STEP               21:        0.39863E+00

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


 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         0.294655002E+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 :  0.10623E+00 0.27083E+02
   Friction velocity        uet   :  0.58320E-02 0.13848E+01
   Friction velocity        uk    :  0.30308E+00 0.22389E+01
   Dimensionless distance   yplus :  0.48800E+03 0.36050E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41351E+02      40   0.30431E-01   0.28618E+02 0.12067E+02 
c  Velocity[X]                                      0.41986E+01 
c  Velocity[Y]                                      0.59251E+00 
c  Velocity[Z]                                      0.23827E+02 
c  Pressure     0.24289E-01     256   0.94875E-08   0.33613E+00 0.11462E+02 
c  k            0.42840E+02      38   0.18589E-02   0.11727E+03 0.38090E+02 
c  epsilon      0.11209E+04      35   0.53029E-02   0.10693E+06 0.47505E+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]             -4.205          16.362      -0.0024571      -0.0024571
v  Velocity[Y]            -2.3705          2.1902      1.4764e-06      1.4764e-06
v  Velocity[Z]            -14.653          32.206          10.002          10.002
v  ǁVelocityǁ             0.16633          32.216           10.53           10.53
v  Pressure               -304.66          392.65           143.3           143.3
v  k                     0.095473          51.767          2.9491          2.9491
v  epsilon               0.080109          1299.1          67.219          67.219
v  TurbVisc              0.003161         0.22405        0.020735        0.020735
v  total_pressure      1.0102e+05      1.0172e+05      1.0147e+05      1.0147e+05


 TIME FOR THE TIME STEP               22:        0.37778E+00

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


 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 :  0.22737E+00 0.27207E+02
   Friction velocity        uet   :  0.12516E-01 0.13971E+01
   Friction velocity        uk    :  0.30747E+00 0.22246E+01
   Dimensionless distance   yplus :  0.49506E+03 0.35820E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41796E+02      40   0.31665E-01   0.26560E+02 0.11527E+02 
c  Velocity[X]                                      0.41628E+01 
c  Velocity[Y]                                      0.51850E+00 
c  Velocity[Z]                                      0.21879E+02 
c  Pressure     0.25531E-01     286   0.93529E-08   0.35217E+00 0.11683E+02 
c  k            0.43842E+02      38   0.17452E-02   0.10839E+03 0.35493E+02 
c  epsilon      0.11403E+04      34   0.48366E-02   0.95591E+05 0.43534E+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]            -4.0677          16.544      -0.0024019      -0.0024019
v  Velocity[Y]            -2.2522           2.254     -4.0635e-06     -4.0635e-06
v  Velocity[Z]            -14.805           32.26          10.002          10.002
v  ǁVelocityǁ             0.23149          32.265          10.547          10.547
v  Pressure                -305.1          387.33          140.42          140.42
v  k                      0.10009           52.52          3.0403          3.0403
v  epsilon               0.085656          1322.9          69.272          69.272
v  TurbVisc             0.0031904         0.22574        0.020981        0.020981
v  total_pressure      1.0102e+05      1.0171e+05      1.0147e+05      1.0147e+05


 TIME FOR THE TIME STEP               23:        0.39445E+00

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


 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         0.294655002E+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 :  0.19374E+00 0.27359E+02
   Friction velocity        uet   :  0.10451E-01 0.14047E+01
   Friction velocity        uk    :  0.31140E+00 0.22213E+01
   Dimensionless distance   yplus :  0.50140E+03 0.35766E+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


 Time for restart files:    0.12905E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42211E+02      40   0.27370E-01   0.25356E+02 0.11154E+02 
c  Velocity[X]                                      0.42603E+01 
c  Velocity[Y]                                      0.42717E+00 
c  Velocity[Z]                                      0.20669E+02 
c  Pressure     0.25726E-01     273   0.98820E-08   0.35613E+00 0.11530E+02 
c  k            0.44955E+02      37   0.16644E-02   0.10211E+03 0.33492E+02 
c  epsilon      0.11660E+04      34   0.46069E-02   0.88695E+05 0.40621E+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]            -3.9489           16.27      -0.0023243      -0.0023243
v  Velocity[Y]            -2.5461          2.5516      4.8249e-07      4.8249e-07
v  Velocity[Z]            -14.957           32.42          10.002          10.002
v  ǁVelocityǁ             0.15344          32.424          10.563          10.563
v  Pressure               -304.16          382.77           137.4           137.4
v  k                      0.10431          53.053          3.1349          3.1349
v  epsilon               0.091076            1334          71.475          71.475
v  TurbVisc              0.003212         0.22762        0.021274        0.021274
v  total_pressure      1.0102e+05      1.0171e+05      1.0146e+05      1.0146e+05


 TIME FOR THE TIME STEP               24:        0.41711E+00

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


 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         0.294655002E+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 :  0.42297E-01 0.27478E+02
   Friction velocity        uet   :  0.23528E-02 0.14123E+01
   Friction velocity        uk    :  0.31485E+00 0.22503E+01
   Dimensionless distance   yplus :  0.50695E+03 0.36233E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42612E+02      40   0.28894E-01   0.22777E+02 0.10524E+02 
c  Velocity[X]                                      0.35582E+01 
c  Velocity[Y]                                      0.32685E+00 
c  Velocity[Z]                                      0.18892E+02 
c  Pressure     0.21679E-01     244   0.98010E-08   0.28869E+00 0.10642E+02 
c  k            0.46182E+02      37   0.16004E-02   0.97840E+02 0.31991E+02 
c  epsilon      0.11974E+04      34   0.45028E-02   0.84923E+05 0.38580E+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]            -3.7993            16.2      -0.0022272      -0.0022272
v  Velocity[Y]            -2.5951          2.5891     -2.1865e-06     -2.1865e-06
v  Velocity[Z]            -15.086           32.52          10.002          10.002
v  ǁVelocityǁ             0.20857          32.523          10.578          10.578
v  Pressure               -303.34          384.02          136.74          136.74
v  k                      0.10806          53.798          3.2325          3.2325
v  epsilon                0.09646            1355          73.822          73.822
v  TurbVisc             0.0032195         0.22983        0.021606        0.021606
v  total_pressure      1.0102e+05      1.0171e+05      1.0146e+05      1.0146e+05


 TIME FOR THE TIME STEP               25:        0.37853E+00

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


 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         0.294655002E+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 :  0.15822E+00 0.27544E+02
   Friction velocity        uet   :  0.82027E-02 0.14171E+01
   Friction velocity        uk    :  0.31789E+00 0.22959E+01
   Dimensionless distance   yplus :  0.51184E+03 0.36967E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42997E+02      40   0.30227E-01   0.21710E+02 0.10222E+02 
c  Velocity[X]                                      0.35338E+01 
c  Velocity[Y]                                      0.31739E+00 
c  Velocity[Z]                                      0.17859E+02 
c  Pressure     0.24387E-01     271   0.89999E-08   0.32316E+00 0.10585E+02 
c  k            0.47494E+02      37   0.15487E-02   0.94982E+02 0.30830E+02 
c  epsilon      0.12332E+04      34   0.44618E-02   0.83236E+05 0.37128E+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]            -3.6802          16.428      -0.0021622      -0.0021622
v  Velocity[Y]            -2.9848          2.9854     -4.4645e-06     -4.4645e-06
v  Velocity[Z]            -15.124          32.635          10.001          10.001
v  ǁVelocityǁ             0.16763          32.638          10.591          10.591
v  Pressure               -301.89          379.52          134.25          134.25
v  k                      0.11148          54.495          3.3326          3.3326
v  epsilon                0.10199          1368.1          76.278          76.278
v  TurbVisc             0.0032129         0.23205        0.021972        0.021972
v  total_pressure      1.0102e+05       1.017e+05      1.0146e+05      1.0146e+05


 TIME FOR THE TIME STEP               26:        0.41158E+00

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


 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         0.294655002E+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 :  0.97281E-01 0.27628E+02
   Friction velocity        uet   :  0.54627E-02 0.14215E+01
   Friction velocity        uk    :  0.32060E+00 0.23420E+01
   Dimensionless distance   yplus :  0.51621E+03 0.37710E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43359E+02      40   0.26169E-01   0.21059E+02 0.10017E+02 
c  Velocity[X]                                      0.38819E+01 
c  Velocity[Y]                                      0.27286E+00 
c  Velocity[Z]                                      0.16905E+02 
c  Pressure     0.23961E-01     257   0.98660E-08   0.32101E+00 0.10596E+02 
c  k            0.48867E+02      37   0.15041E-02   0.93256E+02 0.29954E+02 
c  epsilon      0.12721E+04      34   0.44328E-02   0.82941E+05 0.36101E+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]             -3.579          16.224       -0.002036       -0.002036
v  Velocity[Y]            -3.0184          3.0307     -9.3333e-07     -9.3333e-07
v  Velocity[Z]            -15.219          32.662          10.001          10.001
v  ǁVelocityǁ             0.13588          32.665          10.604          10.604
v  Pressure               -299.49          375.17          131.48          131.48
v  k                      0.11461           55.14          3.4347          3.4347
v  epsilon                 0.1079          1382.8          78.822          78.822
v  TurbVisc             0.0032079         0.23439        0.022367        0.022367
v  total_pressure      1.0103e+05       1.017e+05      1.0146e+05      1.0146e+05


 TIME FOR THE TIME STEP               27:        0.40357E+00

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


 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         0.294655002E+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 :  0.54897E-01 0.27642E+02
   Friction velocity        uet   :  0.29107E-02 0.14245E+01
   Friction velocity        uk    :  0.32307E+00 0.23787E+01
   Dimensionless distance   yplus :  0.52019E+03 0.38300E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43693E+02      40   0.24411E-01   0.19156E+02 0.95331E+01 
c  Velocity[X]                                      0.33411E+01 
c  Velocity[Y]                                      0.22748E+00 
c  Velocity[Z]                                      0.15587E+02 
c  Pressure     0.20005E-01     244   0.87110E-08   0.25876E+00 0.96015E+01 
c  k            0.50288E+02      37   0.14586E-02   0.91968E+02 0.29209E+02 
c  epsilon      0.13133E+04      34   0.43668E-02   0.82944E+05 0.35230E+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]            -3.4493          16.318      -0.0019483      -0.0019483
v  Velocity[Y]            -3.4166          3.4089      4.8754e-07      4.8754e-07
v  Velocity[Z]            -15.224          32.717          10.001          10.001
v  ǁVelocityǁ             0.15369           32.72          10.616          10.616
v  Pressure               -297.35          375.91          130.69          130.69
v  k                      0.11746           55.89          3.5384          3.5384
v  epsilon                0.11453          1399.8          81.429          81.429
v  TurbVisc             0.0032039         0.23686        0.022788        0.022788
v  total_pressure      1.0103e+05       1.017e+05      1.0146e+05      1.0146e+05


 TIME FOR THE TIME STEP               28:        0.43170E+00

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


 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         0.294655002E+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 :  0.29419E-01 0.27648E+02
   Friction velocity        uet   :  0.15324E-02 0.14254E+01
   Friction velocity        uk    :  0.32533E+00 0.24137E+01
   Dimensionless distance   yplus :  0.52383E+03 0.38865E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44039E+02      40   0.27617E-01   0.18195E+02 0.92551E+01 
c  Velocity[X]                                      0.32378E+01 
c  Velocity[Y]                                      0.22729E+00 
c  Velocity[Z]                                      0.14730E+02 
c  Pressure     0.21986E-01     271   0.86471E-08   0.27716E+00 0.94451E+01 
c  k            0.51720E+02      37   0.14144E-02   0.91034E+02 0.28555E+02 
c  epsilon      0.13554E+04      34   0.42712E-02   0.82975E+05 0.34426E+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]            -3.3398          16.413      -0.0017747      -0.0017747
v  Velocity[Y]             -3.645          3.6275     -3.5404e-06     -3.5404e-06
v  Velocity[Z]            -15.207          32.704          10.001          10.001
v  ǁVelocityǁ             0.12681          32.707          10.627          10.627
v  Pressure               -293.66          373.52          128.94          128.94
v  k                      0.12029          56.686          3.6431          3.6431
v  epsilon                0.12201            1413          84.069          84.069
v  TurbVisc             0.0032025          0.2397        0.023231        0.023231
v  total_pressure      1.0103e+05       1.017e+05      1.0145e+05      1.0145e+05


 TIME FOR THE TIME STEP               29:        0.44765E+00

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


 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         0.294655002E+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 :  0.14949E-01 0.27616E+02
   Friction velocity        uet   :  0.77908E-03 0.14261E+01
   Friction velocity        uk    :  0.32742E+00 0.24418E+01
   Dimensionless distance   yplus :  0.52719E+03 0.39317E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44350E+02      39   0.27655E-01   0.17758E+02 0.91004E+01 
c  Velocity[X]                                      0.34766E+01 
c  Velocity[Y]                                      0.21055E+00 
c  Velocity[Z]                                      0.14071E+02 
c  Pressure     0.23286E-01     257   0.94438E-08   0.29121E+00 0.93494E+01 
c  k            0.53160E+02      37   0.13692E-02   0.90113E+02 0.27932E+02 
c  epsilon      0.13976E+04      34   0.41554E-02   0.82745E+05 0.33613E+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]             -3.251          16.579      -0.0015182      -0.0015182
v  Velocity[Y]            -3.8483          3.8388     -4.1171e-06     -4.1171e-06
v  Velocity[Z]            -15.187          32.698          10.001          10.001
v  ǁVelocityǁ             0.18304          32.701          10.637          10.637
v  Pressure               -290.75           369.3          126.75          126.75
v  k                      0.12325          57.411          3.7487          3.7487
v  epsilon                 0.1306          1435.8          86.738          86.738
v  TurbVisc             0.0032036          0.2426        0.023694        0.023694
v  total_pressure      1.0103e+05      1.0169e+05      1.0145e+05      1.0145e+05


 TIME FOR THE TIME STEP               30:        0.42614E+00

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


 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         0.294655002E+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 :  0.81895E-02 0.27590E+02
   Friction velocity        uet   :  0.42925E-03 0.14246E+01
   Friction velocity        uk    :  0.32931E+00 0.24715E+01
   Dimensionless distance   yplus :  0.53024E+03 0.39795E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44648E+02      39   0.26341E-01   0.16961E+02 0.89291E+01 
c  Velocity[X]                                      0.31646E+01 
c  Velocity[Y]                                      0.19182E+00 
c  Velocity[Z]                                      0.13604E+02 
c  Pressure     0.21448E-01     243   0.94173E-08   0.26117E+00 0.86808E+01 
c  k            0.54573E+02      37   0.13237E-02   0.89281E+02 0.27354E+02 
c  epsilon      0.14390E+04      34   0.40185E-02   0.82226E+05 0.32804E+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]            -3.1378          16.341      -0.0011992      -0.0011992
v  Velocity[Y]             -4.061          4.0662      5.1867e-08      5.1867e-08
v  Velocity[Z]            -15.105          32.635          10.001          10.001
v  ǁVelocityǁ             0.22732          32.637          10.645          10.645
v  Pressure               -286.49          371.25          126.29          126.29
v  k                      0.12686          58.039          3.8548          3.8548
v  epsilon                0.14102          1466.9          89.409          89.409
v  TurbVisc             0.0032063         0.24642        0.024175        0.024175
v  total_pressure      1.0104e+05       1.017e+05      1.0145e+05      1.0145e+05


 TIME FOR THE TIME STEP               31:        0.40442E+00

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


 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         0.294655002E+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 :  0.39752E-01 0.27520E+02
   Friction velocity        uet   :  0.20583E-02 0.14276E+01
   Friction velocity        uk    :  0.33108E+00 0.24964E+01
   Dimensionless distance   yplus :  0.53308E+03 0.40196E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.44938E+02      39   0.27578E-01   0.16135E+02 0.86787E+01 
c  Velocity[X]                                      0.30458E+01 
c  Velocity[Y]                                      0.20559E+00 
c  Velocity[Z]                                      0.12883E+02 
c  Pressure     0.22888E-01     258   0.89712E-08   0.27372E+00 0.85246E+01 
c  k            0.55958E+02      37   0.12789E-02   0.88357E+02 0.26779E+02 
c  epsilon      0.14792E+04      34   0.38666E-02   0.81218E+05 0.31948E+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]            -3.0392          16.324      -0.0008071      -0.0008071
v  Velocity[Y]            -4.2374          4.2488     -3.0319e-06     -3.0319e-06
v  Velocity[Z]            -15.039          32.592          10.001          10.001
v  ǁVelocityǁ             0.22011          32.594          10.653          10.653
v  Pressure               -282.33          368.82           124.6           124.6
v  k                      0.13141          58.777          3.9609          3.9609
v  epsilon                 0.1526          1493.1          92.063          92.063
v  TurbVisc             0.0032102         0.24983        0.024671        0.024671
v  total_pressure      1.0104e+05      1.0169e+05      1.0145e+05      1.0145e+05


 TIME FOR THE TIME STEP               32:        0.42247E+00

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


 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         0.294655003E+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 :  0.17936E-01 0.27452E+02
   Friction velocity        uet   :  0.93273E-03 0.14288E+01
   Friction velocity        uk    :  0.33274E+00 0.25150E+01
   Dimensionless distance   yplus :  0.53576E+03 0.40494E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45220E+02      39   0.24821E-01   0.15586E+02 0.84597E+01 
c  Velocity[X]                                      0.30752E+01 
c  Velocity[Y]                                      0.21069E+00 
c  Velocity[Z]                                      0.12300E+02 
c  Pressure     0.22741E-01     230   0.98015E-08   0.27049E+00 0.84026E+01 
c  k            0.57290E+02      37   0.12373E-02   0.87455E+02 0.26227E+02 
c  epsilon      0.15173E+04      34   0.37213E-02   0.80023E+05 0.31101E+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]            -2.9433          16.506     -0.00029431     -0.00029431
v  Velocity[Y]            -4.4451          4.4313      -6.633e-06      -6.633e-06
v  Velocity[Z]            -14.941          32.487              10              10
v  ǁVelocityǁ            0.078049          32.489          10.661          10.661
v  Pressure               -277.64          364.22          122.71          122.71
v  k                      0.13706          59.375          4.0666          4.0666
v  epsilon                0.16664          1512.7          94.686          94.686
v  TurbVisc             0.0032108         0.25349        0.025181        0.025181
v  total_pressure      1.0105e+05      1.0169e+05      1.0145e+05      1.0145e+05


 TIME FOR THE TIME STEP               33:        0.39682E+00

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


 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         0.294655002E+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 :  0.36113E-01 0.27350E+02
   Friction velocity        uet   :  0.18665E-02 0.14289E+01
   Friction velocity        uk    :  0.33428E+00 0.25317E+01
   Dimensionless distance   yplus :  0.53823E+03 0.40764E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45489E+02      39   0.25444E-01   0.14441E+02 0.81436E+01 
c  Velocity[X]                                      0.26687E+01 
c  Velocity[Y]                                      0.17983E+00 
c  Velocity[Z]                                      0.11593E+02 
c  Pressure     0.19184E-01     270   0.88176E-08   0.22387E+00 0.79225E+01 
c  k            0.58564E+02      37   0.11977E-02   0.86389E+02 0.25669E+02 
c  epsilon      0.15533E+04      34   0.35801E-02   0.78428E+05 0.30218E+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]            -2.8556          16.183      0.00027882      0.00027882
v  Velocity[Y]             -4.625          4.6328     -8.3922e-06     -8.3922e-06
v  Velocity[Z]            -14.805          32.407              10              10
v  ǁVelocityǁ              0.2141           32.41          10.667          10.667
v  Pressure               -272.41          367.49          122.85          122.85
v  k                      0.14356          59.802          4.1718          4.1718
v  epsilon                0.18345          1533.7           97.27           97.27
v  TurbVisc             0.0032152         0.25648        0.025703        0.025703
v  total_pressure      1.0105e+05      1.0169e+05      1.0145e+05      1.0145e+05


 TIME FOR THE TIME STEP               34:        0.40264E+00

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


 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         0.294655002E+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 :  0.26644E-01 0.27276E+02
   Friction velocity        uet   :  0.13766E-02 0.14282E+01
   Friction velocity        uk    :  0.33559E+00 0.25417E+01
   Dimensionless distance   yplus :  0.54035E+03 0.40926E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.45754E+02      39   0.25820E-01   0.13854E+02 0.80012E+01 
c  Velocity[X]                                      0.26017E+01 
c  Velocity[Y]                                      0.18696E+00 
c  Velocity[Z]                                      0.11066E+02 
c  Pressure     0.19954E-01     231   0.98903E-08   0.23019E+00 0.75534E+01 
c  k            0.59770E+02      37   0.11578E-02   0.85159E+02 0.25110E+02 
c  epsilon      0.15866E+04      34   0.34362E-02   0.76468E+05 0.29320E+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]            -2.7709          16.506        0.001034        0.001034
v  Velocity[Y]            -4.6904          4.7166      3.7687e-06      3.7687e-06
v  Velocity[Z]            -14.673          32.274              10              10
v  ǁVelocityǁ             0.22138          32.276          10.673          10.673
v  Pressure               -267.52          365.23          121.41          121.41
v  k                      0.15038          60.279          4.2761          4.2761
v  epsilon                0.20256          1547.4          99.805          99.805
v  TurbVisc             0.0032246         0.25929        0.026234        0.026234
v  total_pressure      1.0106e+05      1.0169e+05      1.0145e+05      1.0145e+05


 TIME FOR THE TIME STEP               35:        0.37175E+00

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


 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         0.294655002E+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 :  0.86343E-01 0.27133E+02
   Friction velocity        uet   :  0.48123E-02 0.14262E+01
   Friction velocity        uk    :  0.33612E+00 0.25507E+01
   Dimensionless distance   yplus :  0.54120E+03 0.41070E+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


 Time for restart files:    0.11832E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46009E+02      39   0.25083E-01   0.13651E+02 0.78575E+01 
c  Velocity[X]                                      0.28254E+01 
c  Velocity[Y]                                      0.19029E+00 
c  Velocity[Z]                                      0.10636E+02 
c  Pressure     0.21355E-01     243   0.77200E-08   0.24645E+00 0.77680E+01 
c  k            0.60897E+02      37   0.11200E-02   0.83810E+02 0.24554E+02 
c  epsilon      0.16170E+04      34   0.32905E-02   0.74171E+05 0.28412E+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]            -2.6768          16.489       0.0019722       0.0019722
v  Velocity[Y]             -4.803           4.789      1.3044e-06      1.3044e-06
v  Velocity[Z]            -14.522          32.158          9.9999          9.9999
v  ǁVelocityǁ             0.19914           32.16          10.678          10.678
v  Pressure               -262.22          360.69          119.27          119.27
v  k                      0.15906          60.585          4.3789          4.3789
v  epsilon                0.22329          1558.1          102.27          102.27
v  TurbVisc             0.0032458         0.26185        0.026773        0.026773
v  total_pressure      1.0106e+05      1.0169e+05      1.0144e+05      1.0144e+05


 TIME FOR THE TIME STEP               36:        0.39363E+00

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


 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         0.294655002E+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 :  0.36427E-01 0.27007E+02
   Friction velocity        uet   :  0.18717E-02 0.14238E+01
   Friction velocity        uk    :  0.33642E+00 0.25543E+01
   Dimensionless distance   yplus :  0.54168E+03 0.41127E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46258E+02      39   0.23977E-01   0.12847E+02 0.76330E+01 
c  Velocity[X]                                      0.23217E+01 
c  Velocity[Y]                                      0.17648E+00 
c  Velocity[Z]                                      0.10348E+02 
c  Pressure     0.17888E-01     229   0.77667E-08   0.20276E+00 0.70216E+01 
c  k            0.61947E+02      37   0.10844E-02   0.82337E+02 0.24001E+02 
c  epsilon      0.16444E+04      34   0.31574E-02   0.71716E+05 0.27513E+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]            -2.5837          16.261        0.003047        0.003047
v  Velocity[Y]             -4.929          4.9216     -1.0006e-06     -1.0006e-06
v  Velocity[Z]            -14.353          32.004          9.9999          9.9999
v  ǁVelocityǁ             0.22197          32.006          10.682          10.682
v  Pressure               -256.77          363.45          119.49          119.49
v  k                      0.17052          60.737          4.4801          4.4801
v  epsilon                  0.246          1566.5          104.65          104.65
v  TurbVisc             0.0032645          0.2638        0.027316        0.027316
v  total_pressure      1.0107e+05      1.0169e+05      1.0144e+05      1.0144e+05


 TIME FOR THE TIME STEP               37:        0.37222E+00

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


 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         0.294655002E+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 :  0.83870E-01 0.26876E+02
   Friction velocity        uet   :  0.43090E-02 0.14201E+01
   Friction velocity        uk    :  0.33730E+00 0.25571E+01
   Dimensionless distance   yplus :  0.54309E+03 0.41173E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46496E+02      39   0.23265E-01   0.12212E+02 0.74150E+01 
c  Velocity[X]                                      0.24945E+01 
c  Velocity[Y]                                      0.18770E+00 
c  Velocity[Z]                                      0.95297E+01 
c  Pressure     0.18472E-01     229   0.98657E-08   0.21120E+00 0.65480E+01 
c  k            0.62909E+02      37   0.10517E-02   0.80775E+02 0.23459E+02 
c  epsilon      0.16686E+04      34   0.30360E-02   0.69158E+05 0.26637E+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]            -2.4929          16.212       0.0042715       0.0042715
v  Velocity[Y]            -4.9748           4.972     -3.2999e-06     -3.2999e-06
v  Velocity[Z]            -14.183          31.862          9.9999          9.9999
v  ǁVelocityǁ             0.24509          31.864          10.686          10.686
v  Pressure               -251.56          361.25           118.5           118.5
v  k                      0.18408          60.935          4.5795          4.5795
v  epsilon                0.27174          1568.5          106.95          106.95
v  TurbVisc             0.0032804         0.26584        0.027862        0.027862
v  total_pressure      1.0107e+05      1.0169e+05      1.0144e+05      1.0144e+05


 TIME FOR THE TIME STEP               38:        0.37829E+00

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


 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         0.294655002E+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 :  0.57739E-01 0.26741E+02
   Friction velocity        uet   :  0.29533E-02 0.14158E+01
   Friction velocity        uk    :  0.33864E+00 0.25544E+01
   Dimensionless distance   yplus :  0.54525E+03 0.41130E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46736E+02      39   0.23074E-01   0.11644E+02 0.71536E+01 
c  Velocity[X]                                      0.23536E+01 
c  Velocity[Y]                                      0.18036E+00 
c  Velocity[Z]                                      0.91099E+01 
c  Pressure     0.18686E-01     228   0.86925E-08   0.21139E+00 0.67523E+01 
c  k            0.63790E+02      37   0.10198E-02   0.79007E+02 0.22911E+02 
c  epsilon      0.16898E+04      34   0.29236E-02   0.66437E+05 0.25767E+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]            -2.4038          16.566       0.0056708       0.0056708
v  Velocity[Y]            -5.0498          5.0343     -1.1556e-05     -1.1556e-05
v  Velocity[Z]            -14.023          31.692          9.9997          9.9997
v  ǁVelocityǁ             0.18812          31.694           10.69           10.69
v  Pressure               -246.97          356.98          116.68          116.68
v  k                      0.19657          61.167          4.6771          4.6771
v  epsilon                0.29931          1569.8          109.17          109.17
v  TurbVisc             0.0033015         0.26709        0.028409        0.028409
v  total_pressure      1.0108e+05      1.0168e+05      1.0144e+05      1.0144e+05


 TIME FOR THE TIME STEP               39:        0.37794E+00

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


 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 :  0.57068E-01 0.26583E+02
   Friction velocity        uet   :  0.29194E-02 0.14109E+01
   Friction velocity        uk    :  0.34023E+00 0.25516E+01
   Dimensionless distance   yplus :  0.54781E+03 0.41085E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46960E+02      39   0.22448E-01   0.11042E+02 0.70130E+01 
c  Velocity[X]                                      0.21311E+01 
c  Velocity[Y]                                      0.16188E+00 
c  Velocity[Z]                                      0.87495E+01 
c  Pressure     0.15373E-01     203   0.95845E-08   0.17292E+00 0.60670E+01 
c  k            0.64591E+02      37   0.98879E-03   0.77114E+02 0.22369E+02 
c  epsilon      0.17081E+04      34   0.28170E-02   0.63621E+05 0.24919E+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]            -2.3171          16.111        0.007193        0.007193
v  Velocity[Y]            -5.1166          5.1285     -1.4418e-05     -1.4418e-05
v  Velocity[Z]            -13.867          31.524          9.9997          9.9997
v  ǁVelocityǁ             0.16588          31.526          10.692          10.692
v  Pressure               -243.94          359.08          116.89          116.89
v  k                      0.20552          61.182          4.7726          4.7726
v  epsilon                0.32745          1567.5           111.3           111.3
v  TurbVisc             0.0032996         0.26851        0.028956        0.028956
v  total_pressure      1.0108e+05      1.0168e+05      1.0144e+05      1.0144e+05


 TIME FOR THE TIME STEP               40:        0.35730E+00

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


 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         0.294655002E+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 :  0.86332E-01 0.26430E+02
   Friction velocity        uet   :  0.44407E-02 0.14055E+01
   Friction velocity        uk    :  0.34220E+00 0.25443E+01
   Dimensionless distance   yplus :  0.55099E+03 0.40967E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47175E+02      38   0.23378E-01   0.10269E+02 0.67539E+01 
c  Velocity[X]                                      0.21220E+01 
c  Velocity[Y]                                      0.16992E+00 
c  Velocity[Z]                                      0.79767E+01 
c  Pressure     0.17239E-01     242   0.92256E-08   0.19483E+00 0.57579E+01 
c  k            0.65310E+02      37   0.95939E-03   0.75102E+02 0.21829E+02 
c  epsilon      0.17235E+04      34   0.27181E-02   0.60734E+05 0.24085E+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]            -2.2335          16.376       0.0088567       0.0088567
v  Velocity[Y]            -5.1089          5.1392     -8.0942e-06     -8.0942e-06
v  Velocity[Z]            -13.711          31.355          9.9997          9.9997
v  ǁVelocityǁ             0.16237          31.357          10.694          10.694
v  Pressure               -241.49          356.09          115.74          115.74
v  k                      0.20926          61.229          4.8658          4.8658
v  epsilon                  0.358          1560.8          113.34          113.34
v  TurbVisc             0.0032978         0.26924        0.029499        0.029499
v  total_pressure      1.0108e+05      1.0168e+05      1.0144e+05      1.0144e+05


 TIME FOR THE TIME STEP               41:        0.38439E+00

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


 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 :  0.16215E-01 0.26271E+02
   Friction velocity        uet   :  0.82656E-03 0.14009E+01
   Friction velocity        uk    :  0.34493E+00 0.25358E+01
   Dimensionless distance   yplus :  0.55538E+03 0.40830E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47387E+02      38   0.23926E-01   0.10013E+02 0.66029E+01 
c  Velocity[X]                                      0.21819E+01 
c  Velocity[Y]                                      0.17442E+00 
c  Velocity[Z]                                      0.76563E+01 
c  Pressure     0.19344E-01     243   0.76154E-08   0.21739E+00 0.58935E+01 
c  k            0.65953E+02      37   0.93118E-03   0.72948E+02 0.21288E+02 
c  epsilon      0.17362E+04      34   0.26255E-02   0.57783E+05 0.23266E+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]            -2.1529          16.567        0.010644        0.010644
v  Velocity[Y]             -5.202          5.1746       -1.39e-05       -1.39e-05
v  Velocity[Z]            -13.579          31.164          9.9995          9.9995
v  ǁVelocityǁ             0.16925          31.166          10.696          10.696
v  Pressure               -239.89           351.8          114.08          114.08
v  k                      0.21339          61.107          4.9568          4.9568
v  epsilon                0.38733            1552          115.29          115.29
v  TurbVisc             0.0032948         0.26997        0.030038        0.030038
v  total_pressure      1.0109e+05      1.0168e+05      1.0144e+05      1.0144e+05


 TIME FOR THE TIME STEP               42:        0.38416E+00

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


 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         0.294655002E+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 :  0.69274E-01 0.26113E+02
   Friction velocity        uet   :  0.35376E-02 0.13982E+01
   Friction velocity        uk    :  0.34737E+00 0.25258E+01
   Dimensionless distance   yplus :  0.55932E+03 0.40669E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47586E+02      38   0.22421E-01   0.95538E+01 0.64679E+01 
c  Velocity[X]                                      0.19306E+01 
c  Velocity[Y]                                      0.15845E+00 
c  Velocity[Z]                                      0.74647E+01 
c  Pressure     0.16282E-01     200   0.98490E-08   0.18234E+00 0.51383E+01 
c  k            0.66525E+02      37   0.90431E-03   0.70687E+02 0.20749E+02 
c  epsilon      0.17464E+04      34   0.25414E-02   0.54829E+05 0.22466E+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]            -2.0742          16.173        0.012486        0.012486
v  Velocity[Y]            -5.2155          5.1908     -1.6349e-05     -1.6349e-05
v  Velocity[Z]            -13.455          30.983          9.9996          9.9996
v  ǁVelocityǁ             0.17645          30.985          10.697          10.697
v  Pressure               -238.91           352.9          114.28          114.28
v  k                       0.2183          60.894          5.0453          5.0453
v  epsilon                0.41603          1542.7          117.15          117.15
v  TurbVisc             0.0032942          0.2702         0.03057         0.03057
v  total_pressure      1.0109e+05      1.0168e+05      1.0144e+05      1.0144e+05


 TIME FOR THE TIME STEP               43:        0.35942E+00

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


 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         0.294655002E+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 :  0.73854E-01 0.25940E+02
   Friction velocity        uet   :  0.37534E-02 0.13964E+01
   Friction velocity        uk    :  0.35007E+00 0.25141E+01
   Dimensionless distance   yplus :  0.56366E+03 0.40480E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47779E+02      38   0.24578E-01   0.87894E+01 0.61879E+01 
c  Velocity[X]                                      0.17886E+01 
c  Velocity[Y]                                      0.16828E+00 
c  Velocity[Z]                                      0.68324E+01 
c  Pressure     0.17799E-01     242   0.97049E-08   0.19954E+00 0.49337E+01 
c  k            0.67023E+02      37   0.87998E-03   0.68409E+02 0.20225E+02 
c  epsilon      0.17538E+04      34   0.24681E-02   0.51981E+05 0.21706E+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]             -1.998          16.163        0.014336        0.014336
v  Velocity[Y]            -5.2803          5.2391     -1.6093e-05     -1.6093e-05
v  Velocity[Z]            -13.355          30.881          9.9995          9.9995
v  ǁVelocityǁ             0.18598          30.882          10.697          10.697
v  Pressure               -238.48          349.97          113.25          113.25
v  k                      0.22377           60.65          5.1311          5.1311
v  epsilon                0.44375            1531           118.9           118.9
v  TurbVisc             0.0032984         0.27035        0.031093        0.031093
v  total_pressure      1.0109e+05      1.0167e+05      1.0144e+05      1.0144e+05


 TIME FOR THE TIME STEP               44:        0.38063E+00

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


 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         0.294655002E+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 :  0.25899E-01 0.25784E+02
   Friction velocity        uet   :  0.13170E-02 0.13954E+01
   Friction velocity        uk    :  0.35294E+00 0.25017E+01
   Dimensionless distance   yplus :  0.56829E+03 0.40281E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47969E+02      38   0.22847E-01   0.88041E+01 0.61312E+01 
c  Velocity[X]                                      0.19995E+01 
c  Velocity[Y]                                      0.17274E+00 
c  Velocity[Z]                                      0.66319E+01 
c  Pressure     0.19716E-01     242   0.89757E-08   0.22058E+00 0.54202E+01 
c  k            0.67451E+02      37   0.85475E-03   0.65997E+02 0.19698E+02 
c  epsilon      0.17590E+04      34   0.23980E-02   0.49138E+05 0.20962E+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]            -1.9243          16.361        0.016266        0.016266
v  Velocity[Y]            -5.2237          5.2073     -2.5639e-05     -2.5639e-05
v  Velocity[Z]             -13.26          30.831          9.9994          9.9994
v  ǁVelocityǁ             0.18949          30.832          10.697          10.697
v  Pressure               -238.22          345.38          111.45          111.45
v  k                      0.22983          60.276          5.2142          5.2142
v  epsilon                0.47022            1518          120.56          120.56
v  TurbVisc              0.003273         0.27009        0.031606        0.031606
v  total_pressure      1.0109e+05      1.0167e+05      1.0144e+05      1.0144e+05


 TIME FOR THE TIME STEP               45:        0.37709E+00

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


 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         0.294655002E+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 :  0.51706E-01 0.25704E+02
   Friction velocity        uet   :  0.26350E-02 0.13947E+01
   Friction velocity        uk    :  0.35585E+00 0.24877E+01
   Dimensionless distance   yplus :  0.57297E+03 0.40056E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48127E+02      38   0.21483E-01   0.80297E+01 0.59140E+01 
c  Velocity[X]                                      0.16820E+01 
c  Velocity[Y]                                      0.16093E+00 
c  Velocity[Z]                                      0.61868E+01 
c  Pressure     0.15965E-01     214   0.81333E-08   0.17654E+00 0.48581E+01 
c  k            0.67813E+02      37   0.83005E-03   0.63494E+02 0.19170E+02 
c  epsilon      0.17619E+04      34   0.23328E-02   0.46344E+05 0.20238E+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]            -1.8531          15.951        0.018175        0.018175
v  Velocity[Y]            -5.2535          5.2749     -1.8173e-05     -1.8173e-05
v  Velocity[Z]             -13.17          30.814          9.9997          9.9997
v  ǁVelocityǁ             0.19039          30.816          10.697          10.697
v  Pressure               -237.97           348.6          112.39          112.39
v  k                      0.23604          59.892          5.2947          5.2947
v  epsilon                0.49457          1504.1          122.13          122.13
v  TurbVisc             0.0032713         0.26978        0.032108        0.032108
v  total_pressure      1.0109e+05      1.0167e+05      1.0144e+05      1.0144e+05


 TIME FOR THE TIME STEP               46:        0.36590E+00

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


 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         0.294654999E+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 :  0.73018E-01 0.25712E+02
   Friction velocity        uet   :  0.37045E-02 0.13938E+01
   Friction velocity        uk    :  0.35871E+00 0.24736E+01
   Dimensionless distance   yplus :  0.57757E+03 0.39829E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48304E+02      38   0.25045E-01   0.74722E+01 0.56713E+01 
c  Velocity[X]                                      0.16220E+01 
c  Velocity[Y]                                      0.16208E+00 
c  Velocity[Z]                                      0.56882E+01 
c  Pressure     0.17804E-01     243   0.93917E-08   0.19923E+00 0.45006E+01 
c  k            0.68111E+02      37   0.80563E-03   0.60898E+02 0.18640E+02 
c  epsilon      0.17628E+04      34   0.22676E-02   0.43570E+05 0.19527E+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]            -1.7843          16.355        0.020018        0.020018
v  Velocity[Y]            -5.2488          5.2479     -2.1535e-05     -2.1535e-05
v  Velocity[Z]            -13.102          30.808          9.9996          9.9996
v  ǁVelocityǁ             0.18706           30.81          10.696          10.696
v  Pressure               -237.67          345.59           111.1           111.1
v  k                      0.24235          59.455          5.3723          5.3723
v  epsilon                0.51659          1490.1          123.62          123.62
v  TurbVisc             0.0032646         0.26907        0.032596        0.032596
v  total_pressure      1.0109e+05      1.0167e+05      1.0144e+05      1.0144e+05


 TIME FOR THE TIME STEP               47:        0.37608E+00

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


 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         0.294655002E+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 :  0.22037E-01 0.25727E+02
   Friction velocity        uet   :  0.11188E-02 0.13929E+01
   Friction velocity        uk    :  0.36143E+00 0.24581E+01
   Dimensionless distance   yplus :  0.58196E+03 0.39578E+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


 Time for restart files:    0.12287E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48465E+02      38   0.22098E-01   0.76451E+01 0.56992E+01 
c  Velocity[X]                                      0.17285E+01 
c  Velocity[Y]                                      0.16340E+00 
c  Velocity[Z]                                      0.57533E+01 
c  Pressure     0.19954E-01     243   0.92268E-08   0.22262E+00 0.43952E+01 
c  k            0.68347E+02      37   0.78111E-03   0.58206E+02 0.18105E+02 
c  epsilon      0.17619E+04      34   0.22022E-02   0.40842E+05 0.18829E+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]            -1.7179          16.295        0.021787        0.021787
v  Velocity[Y]            -5.2388          5.2256     -1.4762e-05     -1.4762e-05
v  Velocity[Z]             -13.04          30.804          9.9995          9.9995
v  ǁVelocityǁ             0.17926          30.806          10.695          10.695
v  Pressure               -237.44          341.99          109.75          109.75
v  k                      0.24869          58.945          5.4473          5.4473
v  epsilon                0.53592          1476.5          125.02          125.02
v  TurbVisc             0.0032707         0.26843         0.03307         0.03307
v  total_pressure      1.0109e+05      1.0167e+05      1.0143e+05      1.0143e+05


 TIME FOR THE TIME STEP               48:        0.39002E+00

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


 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         0.294655002E+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 :  0.37390E-01 0.25735E+02
   Friction velocity        uet   :  0.19027E-02 0.13918E+01
   Friction velocity        uk    :  0.36402E+00 0.24428E+01
   Dimensionless distance   yplus :  0.58612E+03 0.39333E+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      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48607E+02      38   0.21438E-01   0.68131E+01 0.54099E+01 
c  Velocity[X]                                      0.15702E+01 
c  Velocity[Y]                                      0.14735E+00 
c  Velocity[Z]                                      0.50956E+01 
c  Pressure     0.14869E-01     244   0.99288E-08   0.16544E+00 0.39749E+01 
c  k            0.68526E+02      37   0.75659E-03   0.55445E+02 0.17564E+02 
c  epsilon      0.17593E+04      34   0.21326E-02   0.38125E+05 0.18132E+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]            -1.6538          16.005        0.023493        0.023493
v  Velocity[Y]            -5.2612           5.231     -2.3574e-05     -2.3574e-05
v  Velocity[Z]                -13          30.799          9.9997          9.9997
v  ǁVelocityǁ             0.16917          30.801          10.693          10.693
v  Pressure               -237.06          344.82          110.49          110.49
v  k                      0.25417          58.442          5.5194          5.5194
v  epsilon                0.55102          1463.7          126.34          126.34
v  TurbVisc             0.0033028         0.26741        0.033529        0.033529
v  total_pressure      1.0109e+05      1.0167e+05      1.0144e+05      1.0144e+05


 TIME FOR THE TIME STEP               49:        0.38017E+00

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


 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         0.294654998E+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 :  0.76957E-01 0.25747E+02
   Friction velocity        uet   :  0.38999E-02 0.13905E+01
   Friction velocity        uk    :  0.36609E+00 0.24267E+01
   Dimensionless distance   yplus :  0.58946E+03 0.39073E+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


 Time for restart files:    0.11856E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48751E+02      38   0.23148E-01   0.63978E+01 0.52184E+01 
c  Velocity[X]                                      0.15239E+01 
c  Velocity[Y]                                      0.15356E+00 
c  Velocity[Z]                                      0.47204E+01 
c  Pressure     0.17534E-01     231   0.96411E-08   0.19658E+00 0.39282E+01 
c  k            0.68655E+02      37   0.73066E-03   0.52574E+02 0.17010E+02 
c  epsilon      0.17555E+04      34   0.20602E-02   0.35421E+05 0.17432E+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]            -1.6492           16.09         0.02506         0.02506
v  Velocity[Y]            -5.2503           5.235     -1.6382e-05     -1.6382e-05
v  Velocity[Z]            -12.964          30.796          9.9997          9.9997
v  ǁVelocityǁ             0.15528          30.798          10.691          10.691
v  Pressure               -236.79          341.87          109.22          109.22
v  k                      0.25913          57.921          5.5888          5.5888
v  epsilon                0.56132            1452          127.58          127.58
v  TurbVisc             0.0033903         0.26648        0.033971        0.033971
v  total_pressure      1.0109e+05      1.0167e+05      1.0143e+05      1.0143e+05


 TIME FOR THE TIME STEP               50:        0.45852E+00

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.17365E-04
      -----------------------                                



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




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


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

 Destroying structures and ending computation

Calculation time summary:

  User CPU time:             39.108 s
  System CPU time:            0.452 s

  Elapsed time:              20.291 s
  CPU / elapsed time          1.950

Memory use summary:

  Total memory used:                             356.176 MiB
  Theoretical instrumented dynamic memory:        27.137 MiB

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

