commande : 
 ./cs_solver --param RANS-2D

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

                                  (R)
                      Code_Saturne

                      Version 4.0.3


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

  révision 4.0.3
  build mar. 08 déc. 2015 18:46:43 CET
  Version MPI 2.1 (Open MPI 1.6.5)


  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.

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


Configuration locale du cas :

  Date :               lun. 02 mai 2016 10:56:15 CEST
  Système :            Linux 3.16.0-50-generic
  Machine :            olivier
  Processeur :         model name	: AMD Athlon(tm) 5350 APU with Radeon(tm) R3
  Mémoire :            3 Mo
  Utilisateur :        olivier (Olivier)
  Répertoire :         /home/olivier/AMIR/TEST/CAS1/RESU/20160502-1056
  méthode de lecture : entrées/sorties standard, accès série
  méthode d'écriture : entrées/sorties standard, accès série

 Lecture des méta-données du fichier: "mesh_input/mesh_01"
 Lecture des méta-données du fichier: "mesh_input/mesh_02"
 Lecture des méta-données du fichier: "mesh_input/mesh_03"

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

                   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    =    0.10000E+04 (Reference density           )
       VISCL0 =    0.10000E-02 (Ref. molecular dyn. visc.   )
       CP0    =    0.41820E+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  =             60 (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-omega SST         (ITURB = 60)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.63000E+01 (Characteristic velocity     )
       IKECOU =              0 (k-epsilon coupling mode     )
       IGRAKE =              1 (Account for gravity         )
       RELAXV =    0.10000E+01 for k      (Relaxation)
       RELAXV =    0.10000E+01 for omega  (Relaxation)

   - 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-omega SST         (ITURB = 60)
       CKWSK1 =    0.11765E+01 (sigma_k1 constant           )
       CKWSK2 =    0.10000E+01 (sigma_k2 constant           )
       CKWSW1 =    0.20000E+01 (sigma_omega1 constant       )
       CKWSW2 =    0.11682E+01 (sigma_omega2 constant       )
       CKWBT1 =    0.75000E-01 (beta1 constant              )
       CKWBT2 =    0.82800E-01 (beta2 constant              )
       CKWGM1 =    0.53933E+00 (gamma1 constant             )
       CKWGM2 =    0.41667E+00 (gamma2 constant             )
       CKWA1  =    0.31000E+00 (a1 constant to compute mu_t )
       CKWC1  =    0.10000E+02 (c1 const. for prod. limiter )
       CMU    =    0.90000E-01 (Cmu (or Beta*) constant for )
                                    omega/epsilon conversion)


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


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

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


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

       IDTVAR =              0 (0 cst; 1,2 var (t, t-space  )
       IPTLRO =              0 (1: rho-related DT clipping  )
       COUMAX =    0.10000E+01 (Maximum target CFL          )
       FOUMAX =    0.10000E+02 (Maximum target Fourier      )
       VARRDT =    0.10000E+00 (For var. DT, max. increase  )
       DTMIN  =    0.50000E-07 (Minimum time step           )
       DTMAX  =    0.50000E-03 (Maximum time step           )
       DTREF  =    0.50000E-06 (Reference time step         )

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

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

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

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

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

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


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

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

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

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


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


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

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

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


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


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

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


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

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


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


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

------------------------------------
 Variable              EPSILO IDIRCL
------------------------------------
 Velocity          0.1000E-07      1
 Pressure          0.1000E-07      1
 k                 0.1000E-07      1
 omega             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 =            100 (Final time step required    )

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


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


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

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

 --- Post-processed variables


Velocity
Pressure
k
omega
TurbVisc
CourantNb
FourierNb
total_pressure
         --           --

 --- Probe history files
       NTHIST =              1 (Output frequency     )
       FRHIST =     -.10000E+01 (Output frequency (s) )
       NCAPT  =              9 (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 omega                         -1
         9 LamVisc                       -1
        10 TurbVisc                      -1
        11 CourantNb                     -1
        12 FourierNb                     -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 omega                          0
        10 TurbVisc                    -999
        11 CourantNb                   -999
        12 FourierNb                   -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)


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


Gestionnaires de sorties pour post traitement :
-----------------------------------------------

  -1: nom: results
      répertoire: postprocessing
      format: EnSight Gold
      options: binary
      dépendence en temps: maillage fixe
      sorties: tous les 10 pas de temps et à la fin du calcul


 Lecture du fichier :  mesh_input/mesh_01
 Fin de la lecture :  mesh_input/mesh_01

 Lecture du fichier :  mesh_input/mesh_02
 Fin de la lecture :  mesh_input/mesh_02

 Lecture du fichier :  mesh_input/mesh_03
 Fin de la lecture :  mesh_input/mesh_03


 -------------------------------------------------------
  Recollement numéro 1 :

  Critère de sélection : "join3 and join4"

  Paramètres de recollement :
    Fraction de la plus petite arête incidente :         0.10000
    Angle maximum entre plans de faces recollées :      25.00000

  Paramètres de recollement avancés :
    Niveau de verbosité :                                 1
    Niveau de visualisation :                             1
    Profondeur max. pour construction de l'arbre :       30
    Nombre max. de boîtes par feuille :                  25
    Rapport max. de boîtes liées / initiales :      5.00000
    Rapport max. de boîtes pour la distribution :   2.00000
    Multiplicateur de tolérance de fusion :         1.00000
    Facteur pré-fusion :                            0.05000
    Mode de calcul de la tolérance :                      1
    Mode de calcul des intersections :                    1
    Nombre max. de suppressions d'équivalences :        500
    Nombre max. de sous-faces par face :               200

  Avant recollement
     Nombre de cellules :       57000
     Nombre de faces internes : 113130
     Nombre de faces de bord :  115740
     Nombre de sommets :        115746

   Nombre global de faces frontières sélectionnées pour le recollement :          0

  Sélection d'éléments effectuée.

Arrêt du recollement: aucune face sélectionnée...

  Après recollement
     Nombre de cellules :       57000
     Nombre de faces internes : 113130
     Nombre de faces de bord :  115740
     Nombre de sommets :        115746


  Joining  1 completed (0.0648 s).

 -------------------------------------------------------
  Recollement numéro 2 :

  Critère de sélection : "join5 and join6"

  Paramètres de recollement :
    Fraction de la plus petite arête incidente :         0.10000
    Angle maximum entre plans de faces recollées :      25.00000

  Paramètres de recollement avancés :
    Niveau de verbosité :                                 1
    Niveau de visualisation :                             1
    Profondeur max. pour construction de l'arbre :       30
    Nombre max. de boîtes par feuille :                  25
    Rapport max. de boîtes liées / initiales :      5.00000
    Rapport max. de boîtes pour la distribution :   2.00000
    Multiplicateur de tolérance de fusion :         1.00000
    Facteur pré-fusion :                            0.05000
    Mode de calcul de la tolérance :                      1
    Mode de calcul des intersections :                    1
    Nombre max. de suppressions d'équivalences :        500
    Nombre max. de sous-faces par face :               200

  Avant recollement
     Nombre de cellules :       57000
     Nombre de faces internes : 113130
     Nombre de faces de bord :  115740
     Nombre de sommets :        115746

   Nombre global de faces frontières sélectionnées pour le recollement :          0

  Sélection d'éléments effectuée.

Arrêt du recollement: aucune face sélectionnée...

  Après recollement
     Nombre de cellules :       57000
     Nombre de faces internes : 113130
     Nombre de faces de bord :  115740
     Nombre de sommets :        115746


  Joining  2 completed (0.0643 s).

  Fin des étapes de recollement :

    Temps écoulé :                    0.13

 Nombre de cellules :                                  57000

 ----------------------------------------------------------
 Nombre de cellules + cellules halo :                  57000


 ----------------------------------------------------------
 Nombre de faces internes :                            113130

 ----------------------------------------------------------
 Nombre de faces de bord :                             115740

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

 Histogramme du nombre de faces internes par cellule :

    valeur minimale =                2
    valeur maximale =                4

      1 : [          2 ;          3 [ =         12
      2 : [          3 ;          4 ] =      56988

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

 Écriture du fichier : mesh_output
 Fin de l'écriture :  mesh_output

 Renumérotation du maillage:

   renumérotation des cellules :
     pré-numérotation                              none
     cellules adjacentes aux halos en dernier :    non
     numérotation :                                none

   renumérotation des faces internes :
     pré-ordonnancement par cellules adjacentes :  id le plus bas en premier
     faces adjacentes aux halos en dernier :       non
     numérotation :                                none

   renumérotation des faces de bord :
     numérotation :                                none

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

 Largeur de bande de la matrice pour maillage volumique :        16900
 Profil/lignes de la matrice pour le maillage volumique :        177

 Coordonnées du maillage         minimale    et maximale
                       X : -1.1000000e-02  9.0680000e-02
                       Y : -9.8685533e-03  5.0003000e-03
                       Z : -2.5451939e-18  5.0000000e-06
 Maillage
     Nombre de cellules :       57000
     Nombre de faces internes : 113130
     Nombre de faces de bord :  115740
     Nombre de sommets :        115746

 Groupes :
    "Symmetry12"
       faces de bord :            34000
    "Symmetry3"
       faces de bord :            40000
    "Symmetry45"
       faces de bord :            40000
    "conv"
       faces de bord :              120
    "div"
       faces de bord :              200
    "div2"
       faces de bord :              100
    "entree"
       faces de bord :              100
    "fluid"
       cellules :                 57000
    "join3"
       faces de bord :              100
    "join4"
       faces de bord :              100
    "join5"
       faces de bord :              100
    "join6"
       faces de bord :              100
    "sortie"
       faces de bord :              100
    "wall12"
       faces de bord :              220
    "wall3"
       faces de bord :              200
    "wall4"
       faces de bord :              300

 --- Information sur les volumes
       Volume de controle minimal =  4.2944887e-16
       Volume de controle maximal =  4.1513359e-12
       Volume total du domaine    =  3.8388330e-09

  Critère 1 : orthogonalité :
    Nombre de mauvaises cellules détecté : 0 -->   0 %

  Critère 2 : décentrement :
    Nombre de mauvaises cellules détecté : 1 -->   0 %

  Critère 3 : qualité du gradient moindres-carrés :
    Nombre de mauvaises cellules détecté : 0 -->   0 %

  Critère 4 : ratio des volumes de cellules :
    Nombre de mauvaises cellules détecté : 0 -->   0 %

  Critère 5 : culpabilité par association :
    Nombre de mauvaises cellules détecté : 0 -->   0 %

 Attention :
 ---------
    Un défaut de qualité de maillage a été détecté

    Le maillage devrait être revu en fonction des critères indiqués.

    Le calcul sera effectué mais la qualité de la solution peut être dégradée...

 Computing geometric quantities (0.307 s)
                                                             
       ALMAX  =    0.15759E-02 (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                 0.2381E-01  0.2381E-01
  omega             0.9792E+02  0.9792E+02
 ---------------------------------

                dt  0.5000E-06  0.5000E-06
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.500000000E-06   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1000E+04  0.1000E+04
  molecular_viscos  0.1000E-02  0.1000E-02
  turbulent_viscos  0.2432E+00  0.2432E+00
 -----------------------------------------

Warning : free inlet outlet boundary conditions
          without external head loss definition
Warning : free inlet outlet boundary conditions
          without external head loss definition
Warning : free inlet outlet boundary conditions
          without external head loss definition
Warning : free inlet outlet boundary conditions
          without external head loss definition


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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         100
Smooth wall               5        1140
Rough wall                6           0
Symmetry                  4      114000
Free outlet               3         100
Free inlet               13         400
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 =    0.12390E-03   0.16534E-02   0.25000E-05



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100         0.000000000E+00
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.000000000E+00
Free inlet               13         400         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    :  0.15178E-01 0.18677E-01
   Dimensionless distance   yplus :  0.35460E-01 0.66650E-01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1140
   Total number of wall faces                   :       1140
------------------------------------------------------------


                                                             
 ** WALL DISTANCE                                            
    -------------                                            
                                                             
  Min distance =    0.23584E-05 Max distance =    0.49568E-02
                                                             
     (Distance calculation done in       1321 iterations)


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.25696E-03      86   0.10627E-03   0.61497E+07 0.20000E+07 
c  Velocity[X]                                      0.60912E+07 
c  Velocity[Y]                                      0.58505E+05 
c  Velocity[Z]                                      0.21723E+01 
c  Pressure     0.21798E-04    2622   0.49729E-01   0.10000E+01 0.20000E+07 
c  k            0.29657E-02      50   0.25643E-04   0.13813E+01 0.69937E+05 
c  omega        0.51342E+07      62   0.50934E-03   0.54000E+23 0.20000E+07 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  0          15.884          2.0956         0.44719
v  Velocity[Y]        -0.00012156          3.7162         0.19485        0.026364
v  Velocity[Z]           -0.36219         0.45806     -1.7785e-06     -5.7274e-08
v  ǁVelocityǁ                   0          16.112          2.1175         0.44923
v  Pressure                -31655       1.526e+08      1.8761e+07      5.7479e+06
v  k                    0.0053617        0.023814        0.022968        0.023752
v  omega                   97.921      5.8131e+09      1.8016e+08      1.0612e+07
v  TurbVisc               0.24319         0.24319         0.24319         0.24319
v  CourantNb                    0               0               0               0
v  FourierNb            0.0012526          9.9986          1.5455         0.16445
v  total_pressure           69670       1.527e+08      1.8862e+07      5.8492e+06


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012526          9.9986          1.5455         0.16445


 TIME FOR THE TIME STEP                1:        0.14688E+02

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


 INSTANT    0.100000000E-05   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.730491142E-08
Free inlet               13         400         0.157502139E-03
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 : -0.25941E+01 0.14907E+01
   Friction velocity        uet   :  0.00000E+00 0.16641E+01
   Friction velocity        uk    :  0.51764E-02 0.25387E+01
   Dimensionless distance   yplus :  0.12770E-01 0.61340E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          6
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42684E-01      10   0.27985E-04   0.59477E+04 0.61197E+05 
c  Velocity[X]                                      0.52770E+04 
c  Velocity[Y]                                      0.67061E+03 
c  Velocity[Z]                                      0.43374E-01 
c  Pressure     0.75613E-05    2350   0.58826E-02   0.99900E+00 0.20000E+07 
c  k            0.29656E-02       6   0.85793E-07   0.65262E+01 0.15277E+06 
c  omega        0.41993E+09       4   0.25398E-07   0.13373E+23 0.19811E+07 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]        -0.00018043          17.195          2.1342          0.4545
v  Velocity[Y]         -0.0031024          4.3933         0.20784        0.028602
v  Velocity[Z]           -0.32381          0.3985      6.5643e-08     -1.9084e-08
v  ǁVelocityǁ                   0          17.348          2.1581         0.45677
v  Pressure                -70777      2.6909e+06      4.1381e+05           94210
v  k                   2.3892e-05         0.02388        0.020465        0.023536
v  omega                    85.61      2.9127e+09       9.101e+07      5.3845e+06
v  TurbVisc             9.242e-10         0.24319         0.12052         0.22158
v  CourantNb                    0          0.2646        0.021682       0.0035923
v  FourierNb           0.00012507           1.987          0.2084        0.052141
v  total_pressure           30548      2.7923e+06      5.1514e+05      1.9553e+05


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012526           1.987         0.23009        0.055733


 TIME FOR THE TIME STEP                2:        0.99810E+01

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


 INSTANT    0.150000000E-05   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.887320844E-23
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.145726557E-07
Free inlet               13         400         0.157494875E-03
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 : -0.32368E+01 0.14781E+01
   Friction velocity        uet   :  0.00000E+00 0.17458E+01
   Friction velocity        uk    :  0.89315E-04 0.26143E+01
   Dimensionless distance   yplus :  0.22034E-03 0.63165E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          6
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43949E-01      10   0.42232E-04   0.60874E+03 0.19545E+05 
c  Velocity[X]                                      0.59797E+03 
c  Velocity[Y]                                      0.10738E+02 
c  Velocity[Z]                                      0.39687E-01 
c  Pressure     0.32960E-05    2418   0.79594E-02   0.66888E+00 0.18603E+08 
c  k            0.29651E-02       6   0.78184E-08   0.27872E+00 0.31597E+05 
c  omega        0.10642E+09       4   0.50351E-07   0.33429E+22 0.19622E+07 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k         -9.5786e-05                             4
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0001281          16.856          2.1365         0.45554
v  Velocity[Y]         -0.0067167          4.3957         0.20921        0.028819
v  Velocity[Z]           -0.28108         0.34127      7.5589e-07     -4.3478e-09
v  ǁVelocityǁ          8.0091e-12          17.021          2.1607         0.45784
v  Pressure                -31767      3.4438e+05           33750         -8357.7
v  k                   2.0543e-07        0.023935         0.02007        0.023493
v  omega                   78.898      1.4622e+09       4.639e+07      2.7666e+06
v  TurbVisc            9.3164e-12          0.2432         0.11904         0.22072
v  CourantNb                    0         0.39119        0.021572       0.0035958
v  FourierNb           0.00013877          1.9513         0.20485        0.051371
v  total_pressure           69558       4.457e+05      1.3507e+05           92967


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012527          1.9514         0.22643        0.054967


 TIME FOR THE TIME STEP                3:        0.10613E+02

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


 INSTANT    0.200000000E-05   TIME STEP NUMBER               4
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.669216581E-23
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.217759965E-07
Free inlet               13         400         0.157487675E-03
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 : -0.26200E+01 0.14820E+01
   Friction velocity        uet   :  0.11562E-05 0.16712E+01
   Friction velocity        uk    :  0.35214E-05 0.25410E+01
   Dimensionless distance   yplus :  0.87285E-05 0.61395E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          5
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43510E-01      16   0.76366E-04   0.23895E+03 0.12246E+05 
c  Velocity[X]                                      0.23742E+03 
c  Velocity[Y]                                      0.15053E+01 
c  Velocity[Z]                                      0.26920E-01 
c  Pressure     0.38038E-05    2095   0.17886E-02   0.10176E+01 0.46297E+07 
c  k            0.29650E-02       5   0.58745E-08   0.82635E-01 0.17212E+05 
c  omega        0.27358E+08       4   0.97314E-07   0.83538E+21 0.19243E+07 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k         -0.00016983                             5
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.055711          16.377          2.1351         0.45592
v  Velocity[Y]          -0.015627          4.2995         0.20885        0.028749
v  Velocity[Z]           -0.24467         0.29358      9.4969e-07     -1.8668e-10
v  ǁVelocityǁ          4.6814e-09          16.534          2.1595         0.45824
v  Pressure           -1.1816e+05           77991          8267.8          -11419
v  k                   3.4969e-09        0.024035        0.019897        0.023471
v  omega                   75.813      7.3691e+08      2.4035e+07      1.4532e+06
v  TurbVisc            1.5942e-13          0.2432         0.11832         0.22035
v  CourantNb           7.4386e-13         0.38772        0.021544       0.0035956
v  FourierNb           0.00015758          1.9255         0.20266        0.050891
v  total_pressure          -16839      1.7932e+05      1.0959e+05           89906


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012527          1.9255          0.2242        0.054486


 TIME FOR THE TIME STEP                4:        0.97485E+01

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


 INSTANT    0.250000000E-05   TIME STEP NUMBER               5
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.971101153E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.332557455E-07
Free inlet               13         400         0.157476195E-03
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 : -0.21405E+01 0.14876E+01
   Friction velocity        uet   :  0.33848E-04 0.16124E+01
   Friction velocity        uk    :  0.33848E-04 0.24792E+01
   Dimensionless distance   yplus :  0.84514E-04 0.59901E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          4
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43473E-01       9   0.34157E-04   0.12298E+03 0.87836E+04 
c  Velocity[X]                                      0.12235E+03 
c  Velocity[Y]                                      0.61467E+00 
c  Velocity[Z]                                      0.18888E-01 
c  Pressure     0.32601E-05    2283   0.41519E-02   0.10846E+01 0.13247E+07 
c  k            0.29649E-02       5   0.78837E-08   0.48345E-01 0.13169E+05 
c  omega        0.72463E+07       5   0.19843E-06   0.20844E+21 0.18486E+07 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k         -0.00028524                             8
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.054968          16.092          2.1345         0.45632
v  Velocity[Y]          -0.035511          4.2978         0.20884        0.028735
v  Velocity[Z]           -0.21345         0.25328      9.9708e-07      9.0802e-10
v  ǁVelocityǁ          4.0348e-08          16.249          2.1588         0.45864
v  Pressure                -31595       1.114e+05           21401         -8439.8
v  k                   1.1731e-10        0.028215        0.019807        0.023457
v  omega                   74.859      3.7424e+08      1.2811e+07      7.9204e+05
v  TurbVisc             5.371e-15          0.2432          0.1146         0.21981
v  CourantNb           1.7737e-10         0.37648        0.021533       0.0035954
v  FourierNb           0.00018453          1.3229         0.19089        0.049757
v  total_pressure           69730      2.1272e+05      1.2273e+05           92885


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012528           1.323         0.21242        0.053352


 TIME FOR THE TIME STEP                5:        0.99119E+01

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


 INSTANT    0.300000000E-05   TIME STEP NUMBER               6
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.446641180E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.442673997E-07
Free inlet               13         400         0.157465183E-03
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 : -0.18225E+01 0.14958E+01
   Friction velocity        uet   :  0.10180E-03 0.15775E+01
   Friction velocity        uk    :  0.10180E-03 0.24346E+01
   Dimensionless distance   yplus :  0.25192E-03 0.58823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          3
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43489E-01       9   0.44541E-04   0.75227E+02 0.68685E+04 
c  Velocity[X]                                      0.74647E+02 
c  Velocity[Y]                                      0.56659E+00 
c  Velocity[Z]                                      0.13487E-01 
c  Pressure     0.36490E-05    2324   0.42536E-02   0.14478E+01 0.41577E+06 
c  k            0.29649E-02       5   0.13642E-07   0.58237E-01 0.14457E+05 
c  omega        0.20458E+07       5   0.31919E-06   0.51677E+20 0.17009E+07 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k         -0.00043187                             8
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.082472          15.992           2.134          0.4567
v  Velocity[Y]          -0.040125          4.2948         0.20893        0.028743
v  Velocity[Z]           -0.18644         0.21908      9.9975e-07      1.1597e-09
v  ǁVelocityǁ          2.3958e-08          16.148          2.1584         0.45903
v  Pressure                -31645      1.1774e+05           28363         -6397.6
v  k                   7.7797e-12        0.052347        0.019781        0.023448
v  omega                   75.189      1.9287e+08      7.1561e+06       4.575e+05
v  TurbVisc            3.5223e-16          0.2432         0.11436         0.21965
v  CourantNb           8.6503e-10         0.36743        0.021525       0.0035954
v  FourierNb           0.00021596          1.2707         0.18951        0.049446
v  total_pressure           69680      2.1906e+05      1.2969e+05           94927


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012529          1.2708         0.21103        0.053042


 TIME FOR THE TIME STEP                6:        0.10014E+02

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


 INSTANT    0.350000000E-05   TIME STEP NUMBER               7
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.299897401E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.557479461E-07
Free inlet               13         400         0.157453703E-03
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 : -0.15611E+01 0.15099E+01
   Friction velocity        uet   :  0.42592E-04 0.15540E+01
   Friction velocity        uk    :  0.42592E-04 0.23954E+01
   Dimensionless distance   yplus :  0.10538E-03 0.57877E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          2
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43502E-01       9   0.50694E-04   0.50942E+02 0.56514E+04 
c  Velocity[X]                                      0.50429E+02 
c  Velocity[Y]                                      0.50334E+00 
c  Velocity[Z]                                      0.96807E-02 
c  Pressure     0.28498E-05    2366   0.59220E-02   0.13071E+01 0.17359E+06 
c  k            0.29648E-02       5   0.23618E-07   0.12524E+00 0.21202E+05 
c  omega        0.65819E+06       6   0.55029E-06   0.12516E+20 0.14325E+07 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k          -0.0005203                             4
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.091992          15.937          2.1335         0.45704
v  Velocity[Y]          -0.052434          4.2854         0.20899         0.02875
v  Velocity[Z]           -0.16306         0.18999      9.8591e-07       1.149e-09
v  ǁVelocityǁ          1.6917e-08           16.09           2.158         0.45937
v  Pressure                -31573      1.1885e+05           27895         -7277.6
v  k                    1.045e-12        0.094434        0.019825        0.023441
v  omega                   76.329      1.0212e+08      4.2982e+06      2.8739e+05
v  TurbVisc            4.4334e-17         0.24424         0.11394         0.21948
v  CourantNb           2.6897e-10         0.36109        0.021512       0.0035953
v  FourierNb           0.00025104          1.2724         0.18814        0.049145
v  total_pressure           69752      2.2017e+05      1.2922e+05           94047


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001253          1.2725         0.20965        0.052741


 TIME FOR THE TIME STEP                7:        0.11087E+02

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


 INSTANT    0.400000000E-05   TIME STEP NUMBER               8
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.120219878E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.664302003E-07
Free inlet               13         400         0.157443020E-03
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 : -0.13206E+01 0.15357E+01
   Friction velocity        uet   :  0.78079E-04 0.15372E+01
   Friction velocity        uk    :  0.78079E-04 0.23574E+01
   Dimensionless distance   yplus :  0.19501E-03 0.56959E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          2
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43514E-01       9   0.34024E-04   0.36835E+02 0.48051E+04 
c  Velocity[X]                                      0.36391E+02 
c  Velocity[Y]                                      0.43695E+00 
c  Velocity[Z]                                      0.70498E-02 
c  Pressure     0.28586E-05    2330   0.52848E-02   0.15002E+01 0.92864E+05 
c  k            0.29648E-02       5   0.38172E-07   0.30042E+00 0.32827E+05 
c  omega        0.26569E+06       6   0.48537E-06   0.28041E+19 0.10161E+07 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k         -0.00035235                             3
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.095287          15.905          2.1331         0.45735
v  Velocity[Y]          -0.048044          4.2695         0.20905        0.028757
v  Velocity[Z]           -0.14279         0.16517      9.6142e-07      1.0339e-09
v  ǁVelocityǁ          1.9081e-09          16.057          2.1575         0.45969
v  Pressure                -31689      1.2003e+05           29329         -6953.4
v  k                   2.7395e-13         0.16219        0.019957        0.023438
v  omega                   78.005      6.5396e+07      2.8609e+06      2.0143e+05
v  TurbVisc            1.0646e-17          0.2432         0.11329         0.21929
v  CourantNb           1.0605e-09         0.35644        0.021501       0.0035953
v  FourierNb            0.0002894          1.2538         0.18569        0.048764
v  total_pressure           69636      2.2136e+05      1.3065e+05           94372


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001253          1.2539         0.20719         0.05236


 TIME FOR THE TIME STEP                8:        0.11234E+02

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


 INSTANT    0.450000000E-05   TIME STEP NUMBER               9
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.459925345E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.771433161E-07
Free inlet               13         400         0.157432307E-03
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 : -0.10915E+01 0.15639E+01
   Friction velocity        uet   :  0.25595E-04 0.15256E+01
   Friction velocity        uk    :  0.25595E-04 0.23198E+01
   Dimensionless distance   yplus :  0.63916E-04 0.56049E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          2
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43524E-01       9   0.38501E-04   0.27904E+02 0.41818E+04 
c  Velocity[X]                                      0.27503E+02 
c  Velocity[Y]                                      0.39604E+00 
c  Velocity[Z]                                      0.51328E-02 
c  Pressure     0.22396E-05    2355   0.60229E-02   0.13201E+01 0.13139E+06 
c  k            0.29648E-02       5   0.56113E-07   0.62648E+00 0.47355E+05 
c  omega        0.15415E+06       6   0.31174E-06   0.58941E+18 0.59213E+06 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k         -3.0586e-06                             1
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.09266          15.888          2.1326         0.45764
v  Velocity[Y]          -0.049359          4.2504          0.2091        0.028762
v  Velocity[Z]           -0.12523         0.14394      9.3202e-07      8.8166e-10
v  ǁVelocityǁ          7.6786e-08          16.038           2.157         0.45998
v  Pressure                -31587      1.2085e+05           28741         -7869.8
v  k                   1.6112e-13         0.26084        0.020187        0.023438
v  omega                   80.055      5.3472e+07      2.1429e+06       1.579e+05
v  TurbVisc            4.2645e-18         0.24385         0.11291         0.21916
v  CourantNb           5.5533e-10         0.35297         0.02149       0.0035953
v  FourierNb           0.00031828          1.2189         0.18434        0.048499
v  total_pressure           69738      2.2218e+05      1.3007e+05           93455


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012531           1.219         0.20583        0.052095


 TIME FOR THE TIME STEP                9:        0.10246E+02

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


 INSTANT    0.500000000E-05   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.175485074E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.870886530E-07
Free inlet               13         400         0.157422362E-03
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 : -0.87298E+00 0.15936E+01
   Friction velocity        uet   :  0.11319E-03 0.15178E+01
   Friction velocity        uk    :  0.11319E-03 0.22828E+01
   Dimensionless distance   yplus :  0.28001E-03 0.55157E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          2
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43533E-01       9   0.39201E-04   0.21982E+02 0.37114E+04 
c  Velocity[X]                                      0.21610E+02 
c  Velocity[Y]                                      0.36782E+00 
c  Velocity[Z]                                      0.37464E-02 
c  Pressure     0.21660E-05    2351   0.53713E-02   0.14233E+01 0.66548E+05 
c  k            0.29648E-02       5   0.75072E-07   0.10607E+01 0.61483E+05 
c  omega        0.12341E+06       6   0.21225E-06   0.15122E+18 0.33783E+06 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.090637          15.881          2.1321         0.45791
v  Velocity[Y]          -0.043267          4.2308         0.20913        0.028768
v  Velocity[Z]           -0.11001         0.12576      8.9949e-07      7.1677e-10
v  ǁVelocityǁ          3.4675e-08          16.029          2.1565         0.46025
v  Pressure                -31740      1.2136e+05           29497         -7734.7
v  k                   1.6987e-13         0.39086        0.020513        0.023441
v  omega                   82.364      5.0034e+07      1.7613e+06      1.3411e+05
v  TurbVisc            3.0612e-18          0.2432         0.11244         0.21902
v  CourantNb           1.0878e-09         0.35035        0.021481       0.0035953
v  FourierNb           0.00034659          1.2062          0.1825        0.048203
v  total_pressure           69585      2.2268e+05      1.3082e+05           93590


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012532          1.2064         0.20398        0.051798


 TIME FOR THE TIME STEP               10:        0.10208E+02

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


 INSTANT    0.550000000E-05   TIME STEP NUMBER              11
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.399405451E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.970032974E-07
Free inlet               13         400         0.157412447E-03
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 : -0.66900E+00 0.16234E+01
   Friction velocity        uet   :  0.12660E-03 0.15128E+01
   Friction velocity        uk    :  0.12660E-03 0.22477E+01
   Dimensionless distance   yplus :  0.31325E-03 0.54307E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          1
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43541E-01       8   0.46119E-04   0.17782E+02 0.33378E+04 
c  Velocity[X]                                      0.17443E+02 
c  Velocity[Y]                                      0.33586E+00 
c  Velocity[Z]                                      0.27246E-02 
c  Pressure     0.17364E-05    2338   0.56672E-02   0.12602E+01 0.90318E+05 
c  k            0.29648E-02       6   0.93261E-07   0.14816E+01 0.72383E+05 
c  omega        0.11435E+06       6   0.23931E-06   0.51171E+17 0.20780E+06 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.087139           15.88          2.1317         0.45817
v  Velocity[Y]          -0.041164          4.2206         0.20917        0.028774
v  Velocity[Z]          -0.096793         0.11012      8.6676e-07      5.7012e-10
v  ǁVelocityǁ          8.3722e-08          16.026          2.1561         0.46051
v  Pressure                -31602      1.2167e+05           29118         -8393.1
v  k                   2.1824e-13         0.55019        0.020916        0.023446
v  omega                   84.876      4.9207e+07      1.5371e+06      1.1963e+05
v  TurbVisc            3.4483e-18         0.24319          0.1121          0.2189
v  CourantNb           1.2419e-09         0.34885        0.021472       0.0035952
v  FourierNb           0.00037786          1.1933         0.18125         0.04796
v  total_pressure           69723      2.2299e+05      1.3044e+05           92932


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012532          1.1935         0.20272        0.051555


 TIME FOR THE TIME STEP               11:        0.10057E+02

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


 INSTANT    0.600000000E-05   TIME STEP NUMBER              12
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.548112169E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.106352102E-06
Free inlet               13         400         0.157403098E-03
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 : -0.48278E+00 0.16513E+01
   Friction velocity        uet   :  0.10020E-03 0.15100E+01
   Friction velocity        uk    :  0.10020E-03 0.22151E+01
   Dimensionless distance   yplus :  0.24798E-03 0.53521E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          1
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43549E-01       8   0.39796E-04   0.14709E+02 0.30355E+04 
c  Velocity[X]                                      0.14395E+02 
c  Velocity[Y]                                      0.31116E+00 
c  Velocity[Z]                                      0.20601E-02 
c  Pressure     0.15979E-05    2324   0.51115E-02   0.12723E+01 0.48559E+05 
c  k            0.29648E-02       6   0.11078E-06   0.17875E+01 0.79051E+05 
c  omega        0.11168E+06       6   0.12294E-06   0.21111E+17 0.13730E+06 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.084815          15.881          2.1312         0.45841
v  Velocity[Y]          -0.035903          4.1949         0.20919        0.028779
v  Velocity[Z]          -0.085315        0.096653      8.3179e-07      4.3651e-10
v  ǁVelocityǁ          9.0914e-08          16.024          2.1556         0.46075
v  Pressure                -31788      1.2176e+05           29362         -8479.5
v  k                   2.9586e-13         0.74279         0.02137        0.023452
v  omega                   84.275      4.9017e+07      1.3921e+06      1.0991e+05
v  TurbVisc            4.5053e-18         0.24331         0.11175         0.21878
v  CourantNb           1.2924e-09         0.34949        0.021464       0.0035952
v  FourierNb           0.00041192          1.1768         0.17997        0.047717
v  total_pressure           69537      2.2308e+05      1.3069e+05           92845


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012533          1.1769         0.20143        0.051312


 TIME FOR THE TIME STEP               12:        0.10194E+02

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


 INSTANT    0.650000000E-05   TIME STEP NUMBER              13
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.615312516E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.115577050E-06
Free inlet               13         400         0.157393873E-03
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 : -0.31444E+00 0.16759E+01
   Friction velocity        uet   :  0.56770E-04 0.15087E+01
   Friction velocity        uk    :  0.56770E-04 0.21855E+01
   Dimensionless distance   yplus :  0.14057E-03 0.52804E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          1
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43555E-01       8   0.39818E-04   0.12401E+02 0.27871E+04 
c  Velocity[X]                                      0.12115E+02 
c  Velocity[Y]                                      0.28487E+00 
c  Velocity[Z]                                      0.15343E-02 
c  Pressure     0.13244E-05    2334   0.50675E-02   0.11504E+01 0.58149E+05 
c  k            0.29648E-02       6   0.12554E-06   0.19351E+01 0.81634E+05 
c  omega        0.11081E+06       6   0.13393E-06   0.99193E+16 0.95638E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.086395          15.881          2.1308         0.45864
v  Velocity[Y]          -0.036451          4.1418         0.20922        0.028784
v  Velocity[Z]          -0.075335        0.085015      7.9602e-07      3.0893e-10
v  ǁVelocityǁ          5.8556e-08          16.021          2.1552         0.46099
v  Pressure                -31615      1.2183e+05           29164         -8881.1
v  k                    3.981e-13         0.95427        0.021851         0.02346
v  omega                   83.653       4.897e+07      1.2915e+06      1.0292e+05
v  TurbVisc            6.1321e-18         0.24319         0.11135         0.21866
v  CourantNb           4.3678e-10         0.35002        0.021456       0.0035952
v  FourierNb           0.00044865          1.1525          0.1786        0.047475
v  total_pressure           69710      2.2315e+05      1.3049e+05           92444


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012533          1.1527         0.20005         0.05107


 TIME FOR THE TIME STEP               13:        0.10260E+02

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


 INSTANT    0.700000000E-05   TIME STEP NUMBER              14
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.423380764E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.124433078E-06
Free inlet               13         400         0.157385017E-03
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 : -0.16681E+00 0.16987E+01
   Friction velocity        uet   :  0.27535E-03 0.15088E+01
   Friction velocity        uk    :  0.27535E-03 0.21593E+01
   Dimensionless distance   yplus :  0.68776E-03 0.52171E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          1
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43562E-01       8   0.41838E-04   0.10554E+02 0.25710E+04 
c  Velocity[X]                                      0.10289E+02 
c  Velocity[Y]                                      0.26343E+00 
c  Velocity[Z]                                      0.11406E-02 
c  Pressure     0.12906E-05    2319   0.46336E-02   0.12163E+01 0.38498E+05 
c  k            0.29649E-02       6   0.13646E-06   0.19177E+01 0.80536E+05 
c  omega        0.11047E+06       6   0.61651E-07   0.51973E+16 0.69931E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.087994          15.894          2.1304         0.45887
v  Velocity[Y]          -0.037486          4.1209         0.20923        0.028788
v  Velocity[Z]          -0.066651        0.075681      7.6105e-07      1.9542e-10
v  ǁVelocityǁ          5.9139e-09          16.032          2.1547         0.46122
v  Pressure                -31825      1.2224e+05           29661         -8827.5
v  k                   5.2796e-13          1.1701        0.022339        0.023468
v  omega                   83.243      4.8957e+07      1.2179e+06           97637
v  TurbVisc            8.2595e-18         0.24319         0.11094         0.21855
v  CourantNb            4.403e-10         0.35246        0.021449       0.0035953
v  FourierNb           0.00048805          1.1282         0.17728        0.047239
v  total_pressure           69500      2.2356e+05      1.3099e+05           92498


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012534          1.1284         0.19873        0.050834


 TIME FOR THE TIME STEP               14:        0.10211E+02

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


 INSTANT    0.750000000E-05   TIME STEP NUMBER              15
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.605812863E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.133259701E-06
Free inlet               13         400         0.157376191E-03
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 : -0.38441E-01 0.17222E+01
   Friction velocity        uet   :  0.51331E-04 0.15097E+01
   Friction velocity        uk    :  0.51331E-04 0.21364E+01
   Dimensionless distance   yplus :  0.12682E-03 0.51619E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          1
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43568E-01       8   0.40433E-04   0.91098E+01 0.23886E+04 
c  Velocity[X]                                      0.88666E+01 
c  Velocity[Y]                                      0.24235E+00 
c  Velocity[Z]                                      0.90744E-03 
c  Pressure     0.10491E-05    2304   0.47986E-02   0.10684E+01 0.47349E+05 
c  k            0.29650E-02       6   0.14099E-06   0.17558E+01 0.76299E+05 
c  omega        0.11031E+06       6   0.75178E-07   0.29776E+16 0.53293E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.087977          15.908            2.13         0.45909
v  Velocity[Y]          -0.038648          4.1036         0.20925        0.028792
v  Velocity[Z]          -0.059087        0.068668      7.2513e-07      8.9643e-11
v  ǁVelocityǁ          2.3631e-08          16.045          2.1543         0.46143
v  Pressure                -31625      1.2242e+05           29440         -9167.7
v  k                    6.829e-13           1.386        0.022813        0.023476
v  omega                   82.993      4.8952e+07      1.1618e+06           93496
v  TurbVisc            1.0957e-17         0.24319         0.11062         0.21846
v  CourantNb           2.1887e-10         0.35302        0.021443       0.0035953
v  FourierNb           0.00053013          1.1183         0.17616        0.047027
v  total_pressure           69700      2.2374e+05      1.3076e+05           92157


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012535          1.1185          0.1976        0.050623


 TIME FOR THE TIME STEP               15:        0.10128E+02

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


 INSTANT    0.800000000E-05   TIME STEP NUMBER              16
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.879008648E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.141769637E-06
Free inlet               13         400         0.157367681E-03
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 0.17417E+01
   Friction velocity        uet   :  0.30604E-04 0.15102E+01
   Friction velocity        uk    :  0.30604E-04 0.21165E+01
   Dimensionless distance   yplus :  0.75587E-04 0.51139E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43573E-01       8   0.44919E-04   0.79603E+01 0.22327E+04 
c  Velocity[X]                                      0.77231E+01 
c  Velocity[Y]                                      0.23652E+00 
c  Velocity[Z]                                      0.68781E-03 
c  Pressure     0.97790E-06    2289   0.42463E-02   0.10709E+01 0.27783E+05 
c  k            0.29650E-02       6   0.14121E-06   0.14964E+01 0.69718E+05 
c  omega        0.11022E+06       6   0.34639E-07   0.18245E+16 0.41921E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.087704          15.924          2.1296          0.4593
v  Velocity[Y]          -0.039618          4.0887         0.20926        0.028795
v  Velocity[Z]          -0.052479        0.062265      6.9008e-07     -7.6853e-12
v  ǁVelocityǁ          2.3395e-08           16.06          2.1539         0.46165
v  Pressure                -31859      1.2252e+05           29639         -9231.3
v  k                      8.7e-13          1.6042        0.023257        0.023483
v  omega                   82.867      4.8949e+07      1.1178e+06           90160
v  TurbVisc            1.4175e-17         0.24319         0.11037         0.21837
v  CourantNb           7.3764e-10         0.35394        0.021437       0.0035953
v  FourierNb           0.00057494          1.1112         0.17521        0.046839
v  total_pressure           69466      2.2385e+05      1.3096e+05           92094


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012535          1.1114         0.19665        0.050435


 TIME FOR THE TIME STEP               16:        0.10092E+02

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


 INSTANT    0.850000000E-05   TIME STEP NUMBER              17
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.127647539E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.150210490E-06
Free inlet               13         400         0.157359240E-03
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 0.17594E+01
   Friction velocity        uet   :  0.11037E-03 0.15108E+01
   Friction velocity        uk    :  0.11037E-03 0.20999E+01
   Dimensionless distance   yplus :  0.27267E-03 0.50736E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43579E-01       8   0.49976E-04   0.70061E+01 0.20945E+04 
c  Velocity[X]                                      0.67938E+01 
c  Velocity[Y]                                      0.21177E+00 
c  Velocity[Z]                                      0.52087E-03 
c  Pressure     0.76044E-06    2284   0.41950E-02   0.89245E+00 0.35779E+05 
c  k            0.29651E-02       6   0.13639E-06   0.11972E+01 0.61737E+05 
c  omega        0.11016E+06       6   0.47329E-07   0.11777E+16 0.33801E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.086264          15.932          2.1292         0.45951
v  Velocity[Y]          -0.040312            4.08         0.20927        0.028798
v  Velocity[Z]            -0.0467        0.056423      6.5746e-07     -8.7537e-11
v  ǁVelocityǁ          3.3177e-08          16.068          2.1535         0.46185
v  Pressure                -31635      1.2233e+05           29284         -9552.6
v  k                   1.0855e-12          1.8098         0.02366         0.02349
v  omega                   82.834      4.8947e+07      1.0824e+06           87419
v  TurbVisc             1.806e-17         0.24328         0.11018          0.2183
v  CourantNb           1.5555e-09          0.3544        0.021431       0.0035954
v  FourierNb           0.00062253           1.104         0.17442        0.046671
v  total_pressure           69690      2.2365e+05      1.3061e+05           91772


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012536          1.1042         0.19585        0.050266


 TIME FOR THE TIME STEP               17:        0.10128E+02

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


 INSTANT    0.900000000E-05   TIME STEP NUMBER              18
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.748905416E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.158374717E-06
Free inlet               13         400         0.157351075E-03
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 0.17744E+01
   Friction velocity        uet   :  0.12686E-03 0.15111E+01
   Friction velocity        uk    :  0.12686E-03 0.20860E+01
   Dimensionless distance   yplus :  0.31345E-03 0.50400E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43584E-01       8   0.55913E-04   0.62296E+01 0.19750E+04 
c  Velocity[X]                                      0.60174E+01 
c  Velocity[Y]                                      0.21182E+00 
c  Velocity[Z]                                      0.41053E-03 
c  Pressure     0.63048E-06    2252   0.35352E-02   0.79065E+00 0.22530E+05 
c  k            0.29652E-02       6   0.12761E-06   0.90781E+00 0.53264E+05 
c  omega        0.11011E+06       6   0.21135E-07   0.79336E+15 0.27819E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.084407          15.931          2.1289         0.45971
v  Velocity[Y]          -0.040837          4.0588         0.20928        0.028801
v  Velocity[Z]          -0.041638        0.051101      6.2528e-07     -1.5928e-10
v  ǁVelocityǁ          2.3345e-08          16.066          2.1531         0.46205
v  Pressure                -31893      1.2181e+05           29039         -9790.8
v  k                    1.336e-12          1.9968        0.024017        0.023496
v  omega                   82.883      4.8946e+07      1.0534e+06           85126
v  TurbVisc            2.2536e-17         0.24319         0.11005         0.21824
v  CourantNb           1.3447e-09         0.35423        0.021426       0.0035954
v  FourierNb           0.00067298          1.0967         0.17376        0.046517
v  total_pressure           69432      2.2314e+05      1.3036e+05           91534


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012536          1.0969         0.19519        0.050112


 TIME FOR THE TIME STEP               18:        0.99661E+01

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


 INSTANT    0.950000000E-05   TIME STEP NUMBER              19
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.383023398E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.166402947E-06
Free inlet               13         400         0.157343047E-03
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 0.17868E+01
   Friction velocity        uet   :  0.10106E-03 0.15112E+01
   Friction velocity        uk    :  0.10106E-03 0.20747E+01
   Dimensionless distance   yplus :  0.25237E-03 0.50128E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43589E-01       8   0.55398E-04   0.55798E+01 0.18691E+04 
c  Velocity[X]                                      0.53871E+01 
c  Velocity[Y]                                      0.19230E+00 
c  Velocity[Z]                                      0.31796E-03 
c  Pressure     0.43161E-06    2215   0.27027E-02   0.57695E+00 0.27980E+05 
c  k            0.29653E-02       6   0.11686E-06   0.65896E+00 0.45005E+05 
c  omega        0.11008E+06       6   0.32938E-07   0.55398E+15 0.23295E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015676          15.791          2.1285          0.4599
v  Velocity[Y]          -0.041224          4.0541         0.20929        0.028805
v  Velocity[Z]          -0.037196        0.046258      5.9396e-07     -2.1398e-10
v  ǁVelocityǁ          1.9441e-08          15.927          2.1528         0.46225
v  Pressure                -31646      1.2098e+05           28478          -10128
v  k                   1.5721e-12           2.164        0.024327        0.023501
v  omega                   83.004      4.8945e+07      1.0291e+06           83183
v  TurbVisc            2.7738e-17          0.2435         0.10998         0.21819
v  CourantNb           1.6794e-09         0.35388        0.021421       0.0035955
v  FourierNb           0.00072638          1.0892         0.17325        0.046384
v  total_pressure           69679      2.2231e+05       1.298e+05           91197


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012537          1.0895         0.19467        0.049979


 TIME FOR THE TIME STEP               19:        0.98708E+01

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


 INSTANT    0.100000000E-04   TIME STEP NUMBER              20
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.695510261E-23
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.174180232E-06
Free inlet               13         400         0.157335270E-03
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 0.17968E+01
   Friction velocity        uet   :  0.10312E-03 0.15107E+01
   Friction velocity        uk    :  0.10312E-03 0.20652E+01
   Dimensionless distance   yplus :  0.25498E-03 0.49898E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43593E-01       8   0.54217E-04   0.49769E+01 0.17651E+04 
c  Velocity[X]                                      0.47981E+01 
c  Velocity[Y]                                      0.17848E+00 
c  Velocity[Z]                                      0.25188E-03 
c  Pressure     0.31755E-06    2153   0.25885E-02   0.45083E+00 0.18552E+05 
c  k            0.29653E-02       6   0.10663E-06   0.46228E+00 0.37426E+05 
c  omega        0.11005E+06       6   0.13958E-07   0.39905E+15 0.19804E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015942          15.818          2.1281         0.46009
v  Velocity[Y]           -0.04132          4.0366          0.2093        0.028807
v  Velocity[Z]          -0.033293        0.041882      5.6424e-07     -2.4944e-10
v  ǁVelocityǁ          2.1356e-08          15.954          2.1524         0.46244
v  Pressure                -31925         1.2e+05           28066          -10393
v  k                   1.8573e-12          2.3131        0.024592        0.023505
v  omega                   83.196      4.8944e+07      1.0085e+06           81512
v  TurbVisc            3.2502e-17         0.24366         0.10999         0.21815
v  CourantNb           1.0163e-09          0.3517        0.021416       0.0035956
v  FourierNb           0.00078283          1.0817         0.17291        0.046269
v  total_pressure           69400      2.2132e+05      1.2939e+05           90932


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012537           1.082         0.19432        0.049865


 TIME FOR THE TIME STEP               20:        0.97000E+01

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


 INSTANT    0.105000000E-04   TIME STEP NUMBER              21
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.179452956E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.181836320E-06
Free inlet               13         400         0.157327614E-03
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 0.18050E+01
   Friction velocity        uet   :  0.56994E-04 0.15082E+01
   Friction velocity        uk    :  0.56994E-04 0.20559E+01
   Dimensionless distance   yplus :  0.14084E-03 0.49675E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43597E-01       8   0.53894E-04   0.45165E+01 0.16815E+04 
c  Velocity[X]                                      0.43400E+01 
c  Velocity[Y]                                      0.17630E+00 
c  Velocity[Z]                                      0.19683E-03 
c  Pressure     0.31311E-06    2118   0.17325E-02   0.47076E+00 0.61288E+04 
c  k            0.29654E-02       6   0.96423E-07   0.31598E+00 0.30755E+05 
c  omega        0.11004E+06       6   0.25017E-07   0.29528E+15 0.17058E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015707          15.705          2.1278         0.46027
v  Velocity[Y]          -0.041464          4.0349          0.2093         0.02881
v  Velocity[Z]          -0.029856        0.037946      5.3652e-07     -2.7362e-10
v  ǁVelocityǁ          5.3098e-08          15.842           2.152         0.46262
v  Pressure                -31650       1.195e+05           28149          -10350
v  k                   2.1777e-12          2.4447        0.024815        0.023508
v  omega                    83.46      4.8944e+07      9.9085e+05           80064
v  TurbVisc            3.8529e-17         0.24319         0.11007         0.21812
v  CourantNb           4.7139e-10         0.35174         0.02141       0.0035956
v  FourierNb           0.00084243          1.0887         0.17272        0.046177
v  total_pressure           69675      2.2083e+05      1.2947e+05           90975


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012538           1.089         0.19413        0.049772


 TIME FOR THE TIME STEP               21:        0.95567E+01

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


 INSTANT    0.110000000E-04   TIME STEP NUMBER              22
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.492414803E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.189466511E-06
Free inlet               13         400         0.157319984E-03
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 0.18118E+01
   Friction velocity        uet   :  0.12807E-03 0.15061E+01
   Friction velocity        uk    :  0.12807E-03 0.20484E+01
   Dimensionless distance   yplus :  0.31645E-03 0.49492E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43601E-01       8   0.43286E-04   0.40772E+01 0.15975E+04 
c  Velocity[X]                                      0.39156E+01 
c  Velocity[Y]                                      0.16141E+00 
c  Velocity[Z]                                      0.16038E-03 
c  Pressure     0.21955E-06    2117   0.19579E-02   0.34896E+00 0.15659E+05 
c  k            0.29654E-02       6   0.87251E-07   0.21191E+00 0.25062E+05 
c  omega        0.11002E+06       6   0.99464E-08   0.22364E+15 0.14862E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015679          15.742          2.1275         0.46046
v  Velocity[Y]          -0.042856          4.0213         0.20931        0.028811
v  Velocity[Z]          -0.026825        0.034395      5.0892e-07     -2.9678e-10
v  ǁVelocityǁ          2.5805e-08           15.88          2.1517         0.46281
v  Pressure                -31949      1.1921e+05           27895          -10558
v  k                   2.5287e-12           2.561        0.025002         0.02351
v  omega                   83.793      4.8943e+07      9.7549e+05           78792
v  TurbVisc            4.5203e-17         0.24319          0.1102          0.2181
v  CourantNb           7.4764e-10         0.35027        0.021406       0.0035957
v  FourierNb            0.0009053          1.0972         0.17267        0.046101
v  total_pressure           69376      2.2053e+05      1.2922e+05           90767


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012538          1.0976         0.19408        0.049696


 TIME FOR THE TIME STEP               22:        0.95742E+01

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


 INSTANT    0.115000000E-04   TIME STEP NUMBER              23
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.540478520E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.197000105E-06
Free inlet               13         400         0.157312450E-03
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 0.18174E+01
   Friction velocity        uet   :  0.93821E-04 0.15024E+01
   Friction velocity        uk    :  0.93821E-04 0.20408E+01
   Dimensionless distance   yplus :  0.23424E-03 0.49310E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43605E-01       8   0.47151E-04   0.37054E+01 0.15229E+04 
c  Velocity[X]                                      0.35550E+01 
c  Velocity[Y]                                      0.15024E+00 
c  Velocity[Z]                                      0.12551E-03 
c  Pressure     0.29108E-06    2120   0.13846E-02   0.48723E+00 0.14600E+05 
c  k            0.29654E-02       6   0.78399E-07   0.14053E+00 0.20327E+05 
c  omega        0.11001E+06       6   0.20886E-07   0.17282E+15 0.13076E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015478           15.77          2.1271         0.46064
v  Velocity[Y]          -0.044201          4.0074         0.20931        0.028813
v  Velocity[Z]          -0.024148        0.031192      4.8307e-07      -3.117e-10
v  ǁVelocityǁ          3.5254e-08          15.908          2.1513         0.46299
v  Pressure                -31650      1.1977e+05           28290          -10344
v  k                   2.9163e-12          2.6631        0.025157        0.023512
v  omega                   84.202      4.8943e+07      9.6201e+05           77669
v  TurbVisc            5.2501e-17          0.2432         0.11035         0.21808
v  CourantNb           5.2533e-10         0.35058        0.021401       0.0035958
v  FourierNb           0.00097156          1.0899          0.1727        0.046034
v  total_pressure           69675       2.211e+05      1.2961e+05           90981


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012539          1.0902          0.1941         0.04963


 TIME FOR THE TIME STEP               23:        0.96977E+01

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


 INSTANT    0.120000000E-04   TIME STEP NUMBER              24
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.973068131E-23
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.204602732E-06
Free inlet               13         400         0.157304847E-03
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 0.18221E+01
   Friction velocity        uet   :  0.12574E-03 0.14990E+01
   Friction velocity        uk    :  0.12574E-03 0.20343E+01
   Dimensionless distance   yplus :  0.31069E-03 0.49153E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43609E-01       8   0.48559E-04   0.33852E+01 0.14556E+04 
c  Velocity[X]                                      0.32367E+01 
c  Velocity[Y]                                      0.14835E+00 
c  Velocity[Z]                                      0.10160E-03 
c  Pressure     0.27651E-06    2139   0.19328E-02   0.48587E+00 0.11823E+05 
c  k            0.29655E-02       6   0.70346E-07   0.92905E-01 0.16475E+05 
c  omega        0.11000E+06       6   0.77350E-08   0.13585E+15 0.11603E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015455          15.794          2.1268         0.46082
v  Velocity[Y]          -0.045503          3.9969         0.20931        0.028813
v  Velocity[Z]          -0.021775        0.028301      4.5806e-07     -3.1741e-10
v  ǁVelocityǁ          6.3936e-08          15.933           2.151         0.46318
v  Pressure                -31967      1.2048e+05           28453          -10363
v  k                   3.3257e-12          2.7525        0.025285        0.023513
v  omega                   84.672      4.8943e+07      9.5008e+05           76666
v  TurbVisc            6.0552e-17         0.24319         0.11042         0.21805
v  CourantNb           1.3026e-09         0.35082        0.021397       0.0035958
v  FourierNb            0.0010413          1.0825          0.1727        0.045956
v  total_pressure           69358       2.218e+05      1.2978e+05           90962


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012539          1.0829         0.19409        0.049552


 TIME FOR THE TIME STEP               24:        0.98099E+01

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


 INSTANT    0.125000000E-04   TIME STEP NUMBER              25
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.829684773E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.212206934E-06
Free inlet               13         400         0.157297243E-03
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 0.18259E+01
   Friction velocity        uet   :  0.59375E-04 0.14958E+01
   Friction velocity        uk    :  0.59375E-04 0.20287E+01
   Dimensionless distance   yplus :  0.14824E-03 0.49017E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         25, Physical time    0.12500E-04


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

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Variables principales écrites dans le fichier de reprise : 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                            
  Coefficients de C.L. écrits dans le fichier de reprise : checkpoint/auxiliary
   End writing the wall distance                        
 End writing


 Time for restart files:    0.31117E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43613E-01       8   0.49826E-04   0.31115E+01 0.13955E+04 
c  Velocity[X]                                      0.29660E+01 
c  Velocity[Y]                                      0.14544E+00 
c  Velocity[Z]                                      0.80243E-04 
c  Pressure     0.30804E-06    2149   0.18809E-02   0.56716E+00 0.13162E+05 
c  k            0.29655E-02       6   0.63019E-07   0.61844E-01 0.13408E+05 
c  omega        0.10999E+06       6   0.18840E-07   0.10841E+15 0.10371E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015362          15.814          2.1265           0.461
v  Velocity[Y]          -0.046762          3.9964          0.2093        0.028814
v  Velocity[Z]          -0.019666        0.025688      4.3406e-07     -3.1606e-10
v  ǁVelocityǁ          3.8952e-08          15.953          2.1507         0.46336
v  Pressure                -31648      1.2106e+05           28785          -10202
v  k                   3.7692e-12           2.831         0.02539        0.023514
v  omega                   85.167      4.8943e+07      9.3945e+05           75769
v  TurbVisc            6.9056e-17         0.24319          0.1104         0.21802
v  CourantNb           1.0519e-09           0.351        0.021393       0.0035959
v  FourierNb            0.0011148          1.0751         0.17249        0.045864
v  total_pressure           69677      2.2238e+05      1.3011e+05           91123


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001254          1.0755         0.19388        0.049459


 TIME FOR THE TIME STEP               25:        0.10145E+02

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


 INSTANT    0.130000000E-04   TIME STEP NUMBER              26
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.815192956E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.219835875E-06
Free inlet               13         400         0.157289614E-03
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 0.18291E+01
   Friction velocity        uet   :  0.13454E-03 0.14929E+01
   Friction velocity        uk    :  0.13454E-03 0.20239E+01
   Dimensionless distance   yplus :  0.33248E-03 0.48901E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43616E-01       8   0.53553E-04   0.28635E+01 0.13387E+04 
c  Velocity[X]                                      0.27176E+01 
c  Velocity[Y]                                      0.14583E+00 
c  Velocity[Z]                                      0.64955E-04 
c  Pressure     0.27651E-06    2169   0.22325E-02   0.53249E+00 0.11506E+05 
c  k            0.29655E-02       6   0.56545E-07   0.41975E-01 0.11026E+05 
c  omega        0.10998E+06       6   0.65020E-08   0.87618E+14 0.93292E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.01532          15.831          2.1262         0.46118
v  Velocity[Y]           -0.04798           3.979          0.2093        0.028814
v  Velocity[Z]          -0.017789        0.023329      4.1107e-07      -3.163e-10
v  ǁVelocityǁ          7.7066e-08          15.969          2.1504         0.46354
v  Pressure                -31986      1.2167e+05           28852          -10271
v  k                   4.2405e-12          2.8998        0.025475        0.023514
v  omega                   85.681      4.8943e+07      9.2992e+05           74957
v  TurbVisc            7.8265e-17         0.24321         0.11025         0.21796
v  CourantNb           1.6315e-09         0.35138        0.021389        0.003596
v  FourierNb            0.0011919          1.0697         0.17189        0.045731
v  total_pressure           69339      2.2299e+05      1.3018e+05           91054


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001254          1.0701         0.19328        0.049327


 TIME FOR THE TIME STEP               26:        0.99135E+01

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


 INSTANT    0.135000000E-04   TIME STEP NUMBER              27
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.326154731E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.227444132E-06
Free inlet               13         400         0.157282006E-03
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 0.18318E+01
   Friction velocity        uet   :  0.13953E-03 0.14905E+01
   Friction velocity        uk    :  0.13953E-03 0.20200E+01
   Dimensionless distance   yplus :  0.34477E-03 0.48805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43620E-01       8   0.50065E-04   0.26429E+01 0.12860E+04 
c  Velocity[X]                                      0.25224E+01 
c  Velocity[Y]                                      0.12040E+00 
c  Velocity[Z]                                      0.52275E-04 
c  Pressure     0.25845E-06    2147   0.20515E-02   0.51955E+00 0.75152E+04 
c  k            0.29655E-02       6   0.50776E-07   0.29597E-01 0.92459E+04 
c  omega        0.10998E+06       6   0.18089E-07   0.71655E+14 0.84405E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015256          15.831          2.1259         0.46136
v  Velocity[Y]          -0.049163          3.9648          0.2093        0.028814
v  Velocity[Z]          -0.016112        0.021199      3.8859e-07     -3.1762e-10
v  ǁVelocityǁ           5.414e-08          15.969          2.1501         0.46372
v  Pressure                -31654       1.221e+05           28944          -10231
v  k                   4.7482e-12          2.9604        0.025545        0.023514
v  omega                   86.029      4.8943e+07      9.2132e+05           74223
v  TurbVisc            8.8053e-17         0.24323         0.11017         0.21792
v  CourantNb           1.5231e-09          0.3518        0.021385       0.0035961
v  FourierNb            0.0012526          1.0692         0.17151        0.045624
v  total_pressure           69671      2.2342e+05      1.3027e+05           91094


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012541          1.0694          0.1929         0.04922


 TIME FOR THE TIME STEP               27:        0.98667E+01

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


 INSTANT    0.140000000E-04   TIME STEP NUMBER              28
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.618414443E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.235013976E-06
Free inlet               13         400         0.157274436E-03
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 0.18341E+01
   Friction velocity        uet   :  0.20729E-04 0.14893E+01
   Friction velocity        uk    :  0.20729E-04 0.20171E+01
   Dimensionless distance   yplus :  0.51752E-04 0.48737E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43623E-01       8   0.50376E-04   0.24758E+01 0.12447E+04 
c  Velocity[X]                                      0.23545E+01 
c  Velocity[Y]                                      0.12131E+00 
c  Velocity[Z]                                      0.41943E-04 
c  Pressure     0.21490E-06    2150   0.20296E-02   0.44977E+00 0.90856E+04 
c  k            0.29654E-02       6   0.46703E-07   0.22129E-01 0.79872E+04 
c  omega        0.10997E+06       6   0.55874E-08   0.59174E+14 0.76736E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015221           15.69          2.1256         0.46154
v  Velocity[Y]          -0.050312          3.9689         0.20929        0.028813
v  Velocity[Z]           -0.01462        0.019274      3.6751e-07     -3.0688e-10
v  ǁVelocityǁ          8.8989e-08          15.829          2.1498          0.4639
v  Pressure                -31898       1.224e+05           28883          -10332
v  k                   5.2866e-12          3.0153        0.025601        0.023514
v  omega                   86.343      4.8943e+07      9.1352e+05           73552
v  TurbVisc            9.8594e-17         0.24325         0.11004         0.21788
v  CourantNb           1.8048e-09         0.35029        0.021381       0.0035962
v  FourierNb            0.0012526          1.0938         0.17093        0.045499
v  total_pressure           69427      2.2372e+05      1.3021e+05           90993


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012541           1.094         0.19231        0.049095


 TIME FOR THE TIME STEP               28:        0.98714E+01

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


 INSTANT    0.145000000E-04   TIME STEP NUMBER              29
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.666914369E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.242546615E-06
Free inlet               13         400         0.157266903E-03
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 0.18362E+01
   Friction velocity        uet   :  0.14369E-03 0.14776E+01
   Friction velocity        uk    :  0.14369E-03 0.20071E+01
   Dimensionless distance   yplus :  0.35529E-03 0.48494E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43626E-01       8   0.51402E-04   0.22725E+01 0.11925E+04 
c  Velocity[X]                                      0.21489E+01 
c  Velocity[Y]                                      0.12357E+00 
c  Velocity[Z]                                      0.33641E-04 
c  Pressure     0.18852E-06    2132   0.17623E-02   0.40690E+00 0.49990E+04 
c  k            0.29654E-02       6   0.40048E-07   0.17331E-01 0.70642E+04 
c  omega        0.10997E+06       6   0.18206E-07   0.49355E+14 0.70104E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015179          15.713          2.1253         0.46171
v  Velocity[Y]          -0.051425          4.0311         0.20929        0.028812
v  Velocity[Z]          -0.013289        0.017533      3.4752e-07     -2.9314e-10
v  ǁVelocityǁ          7.2529e-08          15.855          2.1495         0.46408
v  Pressure                -31658      1.2256e+05           28860          -10343
v  k                   5.8601e-12          3.0605        0.025646        0.023513
v  omega                   86.661      4.8943e+07      9.0641e+05           72940
v  TurbVisc            1.0977e-16         0.24327         0.10997         0.21784
v  CourantNb           1.7296e-09         0.34897        0.021378       0.0035963
v  FourierNb            0.0012525          1.0971         0.17054        0.045398
v  total_pressure           69667      2.2389e+05      1.3018e+05           90982


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012542          1.0974         0.19191        0.048994


 TIME FOR THE TIME STEP               29:        0.98404E+01

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


 INSTANT    0.150000000E-04   TIME STEP NUMBER              30
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.416207557E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.250030053E-06
Free inlet               13         400         0.157259420E-03
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 0.18379E+01
   Friction velocity        uet   :  0.12219E-03 0.14787E+01
   Friction velocity        uk    :  0.12219E-03 0.20066E+01
   Dimensionless distance   yplus :  0.30219E-03 0.48482E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43629E-01       8   0.55258E-04   0.21055E+01 0.11478E+04 
c  Velocity[X]                                      0.19842E+01 
c  Velocity[Y]                                      0.12128E+00 
c  Velocity[Z]                                      0.27463E-04 
c  Pressure     0.64604E-07    1998   0.16160E-02   0.14562E+00 0.20993E+05 
c  k            0.29654E-02       6   0.37699E-07   0.14784E-01 0.65225E+04 
c  omega        0.10996E+06       5   0.53966E-08   0.41481E+14 0.64291E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015133          15.737           2.125         0.46189
v  Velocity[Y]          -0.052502          3.9959         0.20928        0.028811
v  Velocity[Z]          -0.012099        0.015946      3.2871e-07     -2.7511e-10
v  ǁVelocityǁ          7.1946e-08          15.878          2.1492         0.46425
v  Pressure                -31917      1.2217e+05           28316          -10661
v  k                    6.464e-12          3.1021        0.025681        0.023512
v  omega                    86.98      4.8942e+07       8.999e+05           72376
v  TurbVisc            1.2168e-16         0.24396         0.10987          0.2178
v  CourantNb           1.8707e-09         0.34912        0.021374       0.0035964
v  FourierNb            0.0012525          1.0925         0.17007         0.04529
v  total_pressure           69408       2.235e+05      1.2964e+05           90664


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012542          1.0928         0.19144        0.048886


 TIME FOR THE TIME STEP               30:        0.94143E+01

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


 INSTANT    0.155000000E-04   TIME STEP NUMBER              31
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.283761724E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.257366375E-06
Free inlet               13         400         0.157252084E-03
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 0.18393E+01
   Friction velocity        uet   :  0.49938E-04 0.14780E+01
   Friction velocity        uk    :  0.49938E-04 0.20049E+01
   Dimensionless distance   yplus :  0.12348E-03 0.48442E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43632E-01       8   0.47320E-04   0.19830E+01 0.11139E+04 
c  Velocity[X]                                      0.18799E+01 
c  Velocity[Y]                                      0.10313E+00 
c  Velocity[Z]                                      0.22344E-04 
c  Pressure     0.22601E-06    2043   0.73948E-03   0.52951E+00 0.26492E+05 
c  k            0.29654E-02       6   0.33129E-07   0.13171E-01 0.61558E+04 
c  omega        0.10996E+06       5   0.18729E-07   0.35166E+14 0.59210E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015092          15.624          2.1248         0.46206
v  Velocity[Y]          -0.053545          3.9812         0.20927         0.02881
v  Velocity[Z]          -0.011036        0.014503      3.1062e-07     -2.5724e-10
v  ǁVelocityǁ          6.8098e-08          15.765          2.1489         0.46443
v  Pressure                -31656      1.2262e+05           29023          -10263
v  k                   7.1151e-12          3.1381        0.025709        0.023512
v  omega                   87.317      4.8942e+07      8.9393e+05           71858
v  TurbVisc            1.3422e-16         0.24534            0.11          0.2178
v  CourantNb           1.7918e-09         0.34941        0.021371       0.0035966
v  FourierNb            0.0012525          1.0924          0.1701        0.045241
v  total_pressure           69669      2.2394e+05      1.3035e+05           91062


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012543          1.0928         0.19147        0.048838


 TIME FOR THE TIME STEP               31:        0.95514E+01

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


 INSTANT    0.160000000E-04   TIME STEP NUMBER              32
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.485096193E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.264893659E-06
Free inlet               13         400         0.157244556E-03
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 0.18406E+01
   Friction velocity        uet   :  0.14788E-03 0.14784E+01
   Friction velocity        uk    :  0.14788E-03 0.20042E+01
   Dimensionless distance   yplus :  0.36574E-03 0.48426E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43635E-01       8   0.51666E-04   0.18418E+01 0.10735E+04 
c  Velocity[X]                                      0.17391E+01 
c  Velocity[Y]                                      0.10267E+00 
c  Velocity[Z]                                      0.18211E-04 
c  Pressure     0.11558E-06    2113   0.20063E-02   0.28057E+00 0.17714E+05 
c  k            0.29654E-02       5   0.30727E-07   0.12248E-01 0.59368E+04 
c  omega        0.10996E+06       5   0.51854E-08   0.29995E+14 0.54698E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015116          15.653          2.1245         0.46223
v  Velocity[Y]          -0.054556          3.9611         0.20926        0.028807
v  Velocity[Z]          -0.010081        0.013195      2.9345e-07     -2.3693e-10
v  ǁVelocityǁ          5.0499e-08          15.794          2.1487          0.4646
v  Pressure                -31925        1.23e+05           28765          -10487
v  k                   7.7566e-12          3.1697        0.025729        0.023511
v  omega                   87.632      4.8942e+07      8.8842e+05           71376
v  TurbVisc            1.4775e-16         0.24462         0.10963         0.21773
v  CourantNb            1.853e-09          0.3481        0.021367       0.0035967
v  FourierNb            0.0012525          1.0902         0.16899        0.045066
v  total_pressure           69400      2.2432e+05      1.3009e+05           90838


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012543          1.0906         0.19036        0.048663


 TIME FOR THE TIME STEP               32:        0.97513E+01

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


 INSTANT    0.165000000E-04   TIME STEP NUMBER              33
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.724752388E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.272300782E-06
Free inlet               13         400         0.157237149E-03
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 0.18415E+01
   Friction velocity        uet   :  0.88399E-04 0.14774E+01
   Friction velocity        uk    :  0.88399E-04 0.20027E+01
   Dimensionless distance   yplus :  0.22070E-03 0.48389E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43638E-01       8   0.54536E-04   0.17265E+01 0.10393E+04 
c  Velocity[X]                                      0.16224E+01 
c  Velocity[Y]                                      0.10404E+00 
c  Velocity[Z]                                      0.15026E-04 
c  Pressure     0.22709E-06    2102   0.11157E-02   0.56054E+00 0.18613E+05 
c  k            0.29653E-02       5   0.27103E-07   0.11699E-01 0.58037E+04 
c  omega        0.10996E+06       5   0.19534E-07   0.25789E+14 0.50729E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015043          15.545          2.1242         0.46241
v  Velocity[Y]          -0.055718          4.0211         0.20925        0.028806
v  Velocity[Z]         -0.0092239        0.012011      2.7747e-07     -2.1092e-10
v  ǁVelocityǁ          4.1282e-08          15.688          2.1484         0.46478
v  Pressure                -31655      1.2359e+05           29285          -10202
v  k                   8.4626e-12          3.1968        0.025745         0.02351
v  omega                   87.954      4.8942e+07      8.8332e+05           70931
v  TurbVisc            1.6107e-16          0.2458         0.10968         0.21771
v  CourantNb            1.758e-09         0.34668        0.021364       0.0035968
v  FourierNb            0.0012525          1.0879         0.16892        0.045007
v  total_pressure           69670      2.2492e+05      1.3061e+05           91123


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012544          1.0884         0.19029        0.048603


 TIME FOR THE TIME STEP               33:        0.97021E+01

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


 INSTANT    0.170000000E-04   TIME STEP NUMBER              34
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.682973305E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.279829019E-06
Free inlet               13         400         0.157229621E-03
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 0.18423E+01
   Friction velocity        uet   :  0.76078E-04 0.14760E+01
   Friction velocity        uk    :  0.76078E-04 0.20010E+01
   Dimensionless distance   yplus :  0.18994E-03 0.48347E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43641E-01       8   0.54231E-04   0.16312E+01 0.10102E+04 
c  Velocity[X]                                      0.15137E+01 
c  Velocity[Y]                                      0.11748E+00 
c  Velocity[Z]                                      0.12279E-04 
c  Pressure     0.45370E-07    1772   0.19445E-02   0.11630E+00 0.30522E+05 
c  k            0.29653E-02       5   0.25645E-07   0.11397E-01 0.57302E+04 
c  omega        0.10995E+06       5   0.52204E-08   0.22279E+14 0.47161E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.014089          15.597           2.124         0.46258
v  Velocity[Y]           -0.05694          3.9971         0.20924        0.028803
v  Velocity[Z]         -0.0084504        0.010936      2.6229e-07     -1.8473e-10
v  ǁVelocityǁ          4.2612e-08           15.74          2.1481         0.46495
v  Pressure                -31935      1.2316e+05           28839          -10655
v  k                   9.1221e-12          3.2221        0.025755        0.023508
v  omega                   88.253      4.8942e+07      8.7859e+05           70515
v  TurbVisc            1.7573e-16         0.24337         0.10934         0.21765
v  CourantNb           1.9047e-09         0.34642        0.021361       0.0035969
v  FourierNb            0.0012525          1.0856         0.16786        0.044842
v  total_pressure           69390      2.2448e+05      1.3016e+05           90670


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012544           1.086         0.18922        0.048439


 TIME FOR THE TIME STEP               34:        0.86080E+01

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


 INSTANT    0.175000000E-04   TIME STEP NUMBER              35
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.109824382E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.287106109E-06
Free inlet               13         400         0.157222344E-03
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 0.18429E+01
   Friction velocity        uet   :  0.23317E-04 0.14736E+01
   Friction velocity        uk    :  0.23317E-04 0.19986E+01
   Dimensionless distance   yplus :  0.57701E-04 0.48291E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43643E-01       8   0.51008E-04   0.15276E+01 0.97759E+03 
c  Velocity[X]                                      0.14168E+01 
c  Velocity[Y]                                      0.11083E+00 
c  Velocity[Z]                                      0.10075E-04 
c  Pressure     0.16776E-06    2061   0.89578E-03   0.44398E+00 0.27107E+05 
c  k            0.29653E-02       5   0.22499E-07   0.11151E-01 0.56708E+04 
c  omega        0.10996E+06       5   0.20537E-07   0.19390E+14 0.44003E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.014426          15.645          2.1237         0.46275
v  Velocity[Y]          -0.058141          3.9755         0.20923        0.028801
v  Velocity[Z]         -0.0077531        0.009956      2.4831e-07     -1.5102e-10
v  ǁVelocityǁ          4.7658e-08          15.787          2.1479         0.46512
v  Pressure                -31656      1.2339e+05           29000          -10279
v  k                   9.8472e-12          3.2427        0.025761        0.023507
v  omega                   88.551      4.8942e+07      8.7419e+05           70129
v  TurbVisc            1.8909e-16         0.24612         0.10957         0.21766
v  CourantNb           2.6028e-09         0.34691        0.021358        0.003597
v  FourierNb            0.0012525          1.0832         0.16826        0.044842
v  total_pressure           69669      2.2472e+05      1.3033e+05           91046


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012545          1.0836         0.18962        0.048439


 TIME FOR THE TIME STEP               35:        0.95579E+01

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


 INSTANT    0.180000000E-04   TIME STEP NUMBER              36
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.102318364E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.294597295E-06
Free inlet               13         400         0.157214853E-03
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 0.18434E+01
   Friction velocity        uet   :  0.20816E-04 0.14715E+01
   Friction velocity        uk    :  0.20816E-04 0.19967E+01
   Dimensionless distance   yplus :  0.51510E-04 0.48243E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43646E-01       8   0.48983E-04   0.14388E+01 0.94872E+03 
c  Velocity[X]                                      0.13416E+01 
c  Velocity[Y]                                      0.97139E-01 
c  Velocity[Z]                                      0.84376E-05 
c  Pressure     0.16569E-06    2128   0.18329E-02   0.45046E+00 0.14811E+05 
c  k            0.29653E-02       5   0.19027E-07   0.10852E-01 0.55973E+04 
c  omega        0.10995E+06       5   0.52991E-08   0.16932E+14 0.41128E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.013666          15.679          2.1235         0.46292
v  Velocity[Y]          -0.059324          3.9652         0.20922        0.028797
v  Velocity[Z]         -0.0071282       0.0090733      2.3505e-07     -1.1927e-10
v  ǁVelocityǁ          6.4277e-08           15.82          2.1476         0.46529
v  Pressure                -31939      1.2399e+05           29233          -10406
v  k                   1.0609e-11          3.2596        0.025764        0.023506
v  omega                   88.804      4.8942e+07      8.7009e+05           69765
v  TurbVisc            2.0433e-16         0.24341         0.10932         0.21762
v  CourantNb           4.7334e-09         0.34781        0.021355       0.0035972
v  FourierNb            0.0012525          1.0807         0.16721        0.044682
v  total_pressure           69386      2.2532e+05      1.3056e+05           90919


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012545          1.0812         0.18857        0.048279


 TIME FOR THE TIME STEP               36:        0.98111E+01

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


 INSTANT    0.185000000E-04   TIME STEP NUMBER              37
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.127469825E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.302007064E-06
Free inlet               13         400         0.157207443E-03
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 0.18446E+01
   Friction velocity        uet   :  0.12592E-03 0.14701E+01
   Friction velocity        uk    :  0.12592E-03 0.19953E+01
   Dimensionless distance   yplus :  0.31160E-03 0.48209E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43648E-01       8   0.43038E-04   0.13435E+01 0.91677E+03 
c  Velocity[X]                                      0.12654E+01 
c  Velocity[Y]                                      0.78172E-01 
c  Velocity[Z]                                      0.69291E-05 
c  Pressure     0.14625E-06    2130   0.15694E-02   0.40775E+00 0.99448E+04 
c  k            0.29652E-02       5   0.18207E-07   0.10658E-01 0.55502E+04 
c  omega        0.10995E+06       5   0.21700E-07   0.14901E+14 0.38586E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.01369           15.71          2.1232         0.46309
v  Velocity[Y]          -0.060488          3.9469         0.20921        0.028795
v  Velocity[Z]         -0.0065693       0.0082719      2.2257e-07     -8.7255e-11
v  ǁVelocityǁ          2.9253e-09          15.851          2.1474         0.46547
v  Pressure                -31657      1.2413e+05           29218          -10283
v  k                   1.1401e-11          3.2747        0.025764        0.023505
v  omega                   89.054      4.8942e+07      8.6625e+05           69427
v  TurbVisc            2.2015e-16         0.24635         0.10912         0.21757
v  CourantNb           3.4649e-09         0.34873        0.021352       0.0035973
v  FourierNb            0.0012525          1.0763         0.16686        0.044587
v  total_pressure           69668      2.2546e+05      1.3054e+05           91042


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012546          1.0768         0.18821        0.048185


 TIME FOR THE TIME STEP               37:        0.98094E+01

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


 INSTANT    0.190000000E-04   TIME STEP NUMBER              38
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.109116755E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.309457429E-06
Free inlet               13         400         0.157199993E-03
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 0.18455E+01
   Friction velocity        uet   :  0.14351E-04 0.14691E+01
   Friction velocity        uk    :  0.14351E-04 0.19942E+01
   Dimensionless distance   yplus :  0.35838E-04 0.48183E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43651E-01       8   0.57906E-04   0.13044E+01 0.90329E+03 
c  Velocity[X]                                      0.12212E+01 
c  Velocity[Y]                                      0.83175E-01 
c  Velocity[Z]                                      0.57047E-05 
c  Pressure     0.16121E-06    2120   0.16843E-02   0.45183E+00 0.76273E+04 
c  k            0.29652E-02       5   0.15227E-07   0.10351E-01 0.54733E+04 
c  omega        0.10995E+06       5   0.55139E-08   0.13138E+14 0.36239E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.013118          15.722           2.123         0.46326
v  Velocity[Y]          -0.061634          3.9963         0.20919         0.02879
v  Velocity[Z]          -0.006064       0.0075509      2.1065e-07     -5.9891e-11
v  ǁVelocityǁ          3.4607e-08          15.863          2.1471         0.46564
v  Pressure                -31943      1.2456e+05           29393          -10330
v  k                   1.2237e-11          3.2868        0.025762        0.023504
v  omega                   89.293      4.8942e+07      8.6265e+05           69106
v  TurbVisc            2.3663e-16         0.24344         0.10901         0.21754
v  CourantNb           5.3385e-09         0.34931        0.021349       0.0035974
v  FourierNb            0.0012525          1.0701         0.16623        0.044478
v  total_pressure           69382      2.2589e+05      1.3072e+05           90995


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012546          1.0707         0.18758        0.048075


 TIME FOR THE TIME STEP               38:        0.11573E+02

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


 INSTANT    0.195000000E-04   TIME STEP NUMBER              39
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.381666305E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.316895110E-06
Free inlet               13         400         0.157192555E-03
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 0.18467E+01
   Friction velocity        uet   :  0.79994E-04 0.14692E+01
   Friction velocity        uk    :  0.79993E-04 0.19940E+01
   Dimensionless distance   yplus :  0.19816E-03 0.48177E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43653E-01       8   0.53700E-04   0.12672E+01 0.89030E+03 
c  Velocity[X]                                      0.11832E+01 
c  Velocity[Y]                                      0.83972E-01 
c  Velocity[Z]                                      0.47189E-05 
c  Pressure     0.10279E-06    1953   0.10902E-02   0.29691E+00 0.29360E+05 
c  k            0.29652E-02       5   0.17486E-07   0.10166E-01 0.54279E+04 
c  omega        0.10995E+06       5   0.22975E-07   0.11681E+14 0.34172E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0094343          15.606          2.1227         0.46343
v  Velocity[Y]          -0.062762          3.9684         0.20919        0.028788
v  Velocity[Z]         -0.0056092       0.0068943      1.9928e-07     -3.6316e-11
v  ǁVelocityǁ          1.0561e-07          15.748          2.1469          0.4658
v  Pressure                -31667      1.2389e+05           28683          -10741
v  k                   1.3125e-11          3.3015        0.025758        0.023502
v  omega                   89.527      4.8942e+07      8.5928e+05           68807
v  TurbVisc            2.5402e-16         0.24345         0.10887         0.21751
v  CourantNb           3.3671e-09         0.34833        0.021346       0.0035976
v  FourierNb            0.0012525          1.0643          0.1658        0.044383
v  total_pressure           69658      2.2522e+05      1.3001e+05           90584


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012547          1.0648         0.18715        0.047981


 TIME FOR THE TIME STEP               39:        0.10934E+02

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


 INSTANT    0.200000000E-04   TIME STEP NUMBER              40
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.711827691E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.324062267E-06
Free inlet               13         400         0.157185388E-03
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 0.18478E+01
   Friction velocity        uet   :  0.73741E-04 0.14587E+01
   Friction velocity        uk    :  0.73741E-04 0.19861E+01
   Dimensionless distance   yplus :  0.18205E-03 0.47988E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43655E-01       8   0.56555E-04   0.11518E+01 0.84881E+03 
c  Velocity[X]                                      0.10685E+01 
c  Velocity[Y]                                      0.83306E-01 
c  Velocity[Z]                                      0.39207E-05 
c  Pressure     0.70144E-07    1892   0.76361E-03   0.20826E+00 0.10265E+05 
c  k            0.29652E-02       5   0.13150E-07   0.98039E-02 0.53340E+04 
c  omega        0.10995E+06       5   0.57920E-08   0.10385E+14 0.32226E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0081042          15.644          2.1225         0.46359
v  Velocity[Y]          -0.063873          3.9482         0.20918        0.028785
v  Velocity[Z]         -0.0051974        0.006304      1.8883e-07     -6.2567e-12
v  ǁVelocityǁ          1.0627e-07          15.785          2.1466         0.46597
v  Pressure                -31954      1.2316e+05           28399          -10760
v  k                   1.4054e-11          3.3106        0.025752        0.023501
v  omega                    89.78      4.8942e+07       8.561e+05           68522
v  TurbVisc            2.7242e-16         0.25324         0.10934         0.21755
v  CourantNb           8.3715e-09         0.34715        0.021343       0.0035977
v  FourierNb            0.0012525          1.2718         0.16704        0.044477
v  total_pressure           69371      2.2448e+05      1.2972e+05           90565


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012547          1.2722         0.18838        0.048075


 TIME FOR THE TIME STEP               40:        0.91703E+01

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


 INSTANT    0.205000000E-04   TIME STEP NUMBER              41
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.396820512E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.331295401E-06
Free inlet               13         400         0.157178155E-03
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 0.18487E+01
   Friction velocity        uet   :  0.28718E-03 0.14611E+01
   Friction velocity        uk    :  0.28718E-03 0.19877E+01
   Dimensionless distance   yplus :  0.71731E-03 0.48025E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43658E-01       8   0.51862E-04   0.11085E+01 0.83269E+03 
c  Velocity[X]                                      0.10184E+01 
c  Velocity[Y]                                      0.90122E-01 
c  Velocity[Z]                                      0.32967E-05 
c  Pressure     0.42152E-07    1670   0.63541E-03   0.12814E+00 0.30240E+04 
c  k            0.29651E-02       5   0.32831E-07   0.18020E-01 0.72371E+04 
c  omega        0.10995E+06       5   0.52492E-06   0.28895E+16 0.53736E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0086703          15.661          2.1223         0.46376
v  Velocity[Y]          -0.064968          3.9243         0.20917        0.028781
v  Velocity[Z]         -0.0048238       0.0057646      1.7908e-07      2.4817e-11
v  ǁVelocityǁ          8.9334e-08            15.8          2.1464         0.46614
v  Pressure                -31665      1.2484e+05           28393          -10731
v  k                   1.4984e-11          3.3172        0.025742          0.0235
v  omega                   90.037      7.4668e+07      8.5438e+05           68277
v  TurbVisc            2.9174e-16         0.25608         0.10932         0.21753
v  CourantNb           7.4338e-09          0.3467        0.021341       0.0035978
v  FourierNb            0.0012525           1.472         0.16695        0.044411
v  total_pressure           69660      2.2616e+05      1.2972e+05           90594


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012548          1.4725         0.18829        0.048009


 TIME FOR THE TIME STEP               41:        0.89928E+01

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


 INSTANT    0.210000000E-04   TIME STEP NUMBER              42
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.773090755E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.338505595E-06
Free inlet               13         400         0.157170944E-03
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 0.18493E+01
   Friction velocity        uet   :  0.28491E-03 0.14618E+01
   Friction velocity        uk    :  0.28491E-03 0.19880E+01
   Dimensionless distance   yplus :  0.71165E-03 0.48033E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43660E-01       9   0.47769E-04   0.10754E+01 0.82014E+03 
c  Velocity[X]                                      0.97668E+00 
c  Velocity[Y]                                      0.98732E-01 
c  Velocity[Z]                                      0.26936E-05 
c  Pressure     0.53583E-07    1758   0.10769E-02   0.16246E+00 0.79643E+04 
c  k            0.29651E-02       5   0.95692E-07   0.88826E-01 0.16081E+05 
c  omega        0.10995E+06       5   0.13414E-06   0.20180E+15 0.14205E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0085091          15.525           2.122         0.46392
v  Velocity[Y]          -0.066046          3.9854         0.20916        0.028777
v  Velocity[Z]         -0.0044883       0.0052744      1.6998e-07      5.6921e-11
v  ǁVelocityǁ          1.6798e-07          15.666          2.1462         0.46631
v  Pressure                -31958      1.2383e+05           28601          -10641
v  k                   1.5935e-11          3.3225        0.025725        0.023498
v  omega                   90.295      5.6495e+07      8.5125e+05           68017
v  TurbVisc            3.1103e-16         0.25741         0.10913          0.2175
v  CourantNb           5.1995e-09         0.34605        0.021339        0.003598
v  FourierNb            0.0012525          1.4449         0.16615        0.044288
v  total_pressure           69367      2.2515e+05      1.2993e+05           90684


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012548          1.4453         0.18748        0.047886


 TIME FOR THE TIME STEP               42:        0.87741E+01

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


 INSTANT    0.215000000E-04   TIME STEP NUMBER              43
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.889671523E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.345808874E-06
Free inlet               13         400         0.157163641E-03
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 0.18499E+01
   Friction velocity        uet   :  0.27272E-03 0.14627E+01
   Friction velocity        uk    :  0.27272E-03 0.19885E+01
   Dimensionless distance   yplus :  0.68121E-03 0.48046E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43662E-01      10   0.50151E-04   0.10014E+01 0.79141E+03 
c  Velocity[X]                                      0.91301E+00 
c  Velocity[Y]                                      0.88410E-01 
c  Velocity[Z]                                      0.22633E-05 
c  Pressure     0.19622E-06    1652   0.68032E-03   0.61056E+00 0.29991E+05 
c  k            0.29651E-02       5   0.20523E-07   0.10746E-01 0.55975E+04 
c  omega        0.10995E+06       5   0.17312E-06   0.32811E+15 0.18117E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0086025          15.438          2.1218         0.46408
v  Velocity[Y]          -0.067109          3.9558         0.20915        0.028774
v  Velocity[Z]         -0.0041861       0.0048304      1.6178e-07      9.6299e-11
v  ǁVelocityǁ          6.8856e-08          15.579          2.1459         0.46647
v  Pressure                -31671      1.2387e+05           27724          -11049
v  k                   1.6918e-11          3.3301        0.025714        0.023497
v  omega                   90.539      4.8942e+07      8.4817e+05           67772
v  TurbVisc            3.3077e-16         0.25246         0.10908         0.21748
v  CourantNb           4.7002e-09         0.34372        0.021336       0.0035981
v  FourierNb            0.0012525          1.4381           0.166        0.044228
v  total_pressure           69654      2.2519e+05      1.2905e+05           90276


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012549          1.4387         0.18733        0.047826


 TIME FOR THE TIME STEP               43:        0.81818E+01

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


 INSTANT    0.220000000E-04   TIME STEP NUMBER              44
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.491784724E-23
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.352853396E-06
Free inlet               13         400         0.157156597E-03
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 0.18504E+01
   Friction velocity        uet   :  0.12764E-03 0.14617E+01
   Friction velocity        uk    :  0.12764E-03 0.19876E+01
   Dimensionless distance   yplus :  0.31882E-03 0.48024E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43664E-01       8   0.51529E-04   0.94152E+00 0.76736E+03 
c  Velocity[X]                                      0.86799E+00 
c  Velocity[Y]                                      0.73523E-01 
c  Velocity[Z]                                      0.19108E-05 
c  Pressure     0.36500E-07    1977   0.18835E-02   0.11402E+00 0.23480E+05 
c  k            0.29650E-02       5   0.13706E-07   0.92920E-02 0.52090E+04 
c  omega        0.10994E+06       5   0.88895E-07   0.93585E+14 0.96772E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.018392          15.485          2.1216         0.46425
v  Velocity[Y]          -0.068157          4.0013         0.20914         0.02877
v  Velocity[Z]         -0.0039059       0.0044207      1.5401e-07      1.3344e-10
v  ǁVelocityǁ          7.3146e-08          15.629          2.1457         0.46663
v  Pressure                -31963      1.2273e+05           28229          -10751
v  k                   1.7984e-11          3.3339        0.025702        0.023495
v  omega                    90.82      4.8942e+07      8.4542e+05           67539
v  TurbVisc            3.5117e-16         0.24441         0.10853         0.21741
v  CourantNb           6.3529e-09         0.34283        0.021333       0.0035982
v  FourierNb            0.0012525          1.0313         0.16381        0.043964
v  total_pressure           69362      2.2406e+05      1.2955e+05           90574


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012549          1.0319         0.18515        0.047562


 TIME FOR THE TIME STEP               44:        0.93123E+01

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


 INSTANT    0.225000000E-04   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.698773747E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.360131628E-06
Free inlet               13         400         0.157149318E-03
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 0.18508E+01
   Friction velocity        uet   :  0.14502E-03 0.14591E+01
   Friction velocity        uk    :  0.14502E-03 0.19857E+01
   Dimensionless distance   yplus :  0.36217E-03 0.47977E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43666E-01       8   0.50179E-04   0.90242E+00 0.75125E+03 
c  Velocity[X]                                      0.82814E+00 
c  Velocity[Y]                                      0.74280E-01 
c  Velocity[Z]                                      0.15763E-05 
c  Pressure     0.76099E-07    1773   0.71472E-03   0.24483E+00 0.10610E+05 
c  k            0.29650E-02       5   0.13658E-07   0.90009E-02 0.51307E+04 
c  omega        0.10995E+06       5   0.54810E-07   0.31584E+14 0.56221E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.020162          15.412          2.1214         0.46441
v  Velocity[Y]          -0.069192          3.9667         0.20913        0.028766
v  Velocity[Z]         -0.0036507       0.0040501      1.4666e-07      1.6695e-10
v  ǁVelocityǁ          5.1288e-08          15.553          2.1455          0.4668
v  Pressure                -31667      1.2248e+05           27980          -10877
v  k                   1.9043e-11          3.3377         0.02569        0.023494
v  omega                    91.07      4.8942e+07       8.429e+05           67322
v  TurbVisc            3.7322e-16         0.24691         0.10865         0.21742
v  CourantNb           4.6986e-09         0.34341         0.02133       0.0035983
v  FourierNb            0.0012525          1.0775         0.16414        0.043958
v  total_pressure           69658       2.238e+05       1.293e+05           90448


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001255          1.0781         0.18547        0.047556


 TIME FOR THE TIME STEP               45:        0.86033E+01

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


 INSTANT    0.230000000E-04   TIME STEP NUMBER              46
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.141622368E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.367286456E-06
Free inlet               13         400         0.157142164E-03
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 0.18511E+01
   Friction velocity        uet   :  0.18349E-03 0.14572E+01
   Friction velocity        uk    :  0.18349E-03 0.19842E+01
   Dimensionless distance   yplus :  0.45821E-03 0.47942E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43668E-01       9   0.50267E-04   0.88099E+00 0.74227E+03 
c  Velocity[X]                                      0.79410E+00 
c  Velocity[Y]                                      0.86884E-01 
c  Velocity[Z]                                      0.13257E-05 
c  Pressure     0.14305E-06    2051   0.10669E-02   0.45987E+00 0.29469E+05 
c  k            0.29650E-02       5   0.13002E-07   0.90594E-02 0.51512E+04 
c  omega        0.10994E+06       5   0.28847E-06   0.93153E+15 0.30530E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.025048          15.471          2.1212         0.46458
v  Velocity[Y]          -0.070212          3.9999         0.20912        0.028761
v  Velocity[Z]          -0.003426       0.0037052      1.3976e-07      2.0044e-10
v  ǁVelocityǁ          4.3094e-08          15.617          2.1453         0.46697
v  Pressure                -31964      1.2445e+05           28768          -10471
v  k                    2.015e-11           3.338        0.025677        0.023493
v  omega                   91.324      5.4115e+07      8.4133e+05           67126
v  TurbVisc            3.9517e-16          0.2471         0.10855          0.2174
v  CourantNb           4.4002e-09           0.343        0.021327       0.0035985
v  FourierNb            0.0012525          1.0184         0.16368        0.043867
v  total_pressure           69361      2.2577e+05      1.3009e+05           90854


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001255           1.019           0.185        0.047465


 TIME FOR THE TIME STEP               46:        0.95461E+01

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


 INSTANT    0.235000000E-04   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.541480184E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.374716051E-06
Free inlet               13         400         0.157134734E-03
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 0.18512E+01
   Friction velocity        uet   :  0.12039E-03 0.14546E+01
   Friction velocity        uk    :  0.12039E-03 0.19824E+01
   Dimensionless distance   yplus :  0.30064E-03 0.47898E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43670E-01       8   0.50986E-04   0.83475E+00 0.72252E+03 
c  Velocity[X]                                      0.75792E+00 
c  Velocity[Y]                                      0.76824E-01 
c  Velocity[Z]                                      0.10969E-05 
c  Pressure     0.43774E-07    1969   0.15402E-02   0.14382E+00 0.15222E+05 
c  k            0.29650E-02       5   0.14668E-07   0.92075E-02 0.51971E+04 
c  omega        0.10995E+06       5   0.39973E-07   0.13996E+14 0.37424E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.017921          15.527           2.121         0.46474
v  Velocity[Y]          -0.071218          3.9614          0.2091        0.028757
v  Velocity[Z]         -0.0032159       0.0033908      1.3331e-07      2.3279e-10
v  ǁVelocityǁ          8.7919e-08          15.671          2.1451         0.46713
v  Pressure                -31663      1.2351e+05           28490          -10642
v  k                   2.1257e-11          3.3385        0.025663        0.023491
v  omega                   91.527      5.0242e+07       8.391e+05           66931
v  TurbVisc            4.1812e-16         0.24626         0.10849         0.21738
v  CourantNb           4.1044e-09         0.34441        0.021326       0.0035986
v  FourierNb            0.0012525          1.0153         0.16349        0.043813
v  total_pressure           69662      2.2483e+05      1.2982e+05           90683


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012551           1.016         0.18482        0.047412


 TIME FOR THE TIME STEP               47:        0.92342E+01

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


 INSTANT    0.240000000E-04   TIME STEP NUMBER              48
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.257783083E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.381984114E-06
Free inlet               13         400         0.157127466E-03
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 0.18513E+01
   Friction velocity        uet   :  0.18711E-03 0.14527E+01
   Friction velocity        uk    :  0.18711E-03 0.19810E+01
   Dimensionless distance   yplus :  0.46726E-03 0.47865E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43672E-01      10   0.45545E-04   0.81194E+00 0.71257E+03 
c  Velocity[X]                                      0.73409E+00 
c  Velocity[Y]                                      0.77849E-01 
c  Velocity[Z]                                      0.90749E-06 
c  Pressure     0.18455E-06    2002   0.67210E-03   0.61536E+00 0.23561E+05 
c  k            0.29649E-02       5   0.82305E-08   0.75263E-02 0.47023E+04 
c  omega        0.10994E+06       5   0.10073E-07   0.52618E+13 0.22949E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.014989          15.579          2.1208         0.46491
v  Velocity[Y]          -0.072212          3.9273         0.20909        0.028751
v  Velocity[Z]          -0.003023       0.0031065       1.275e-07      2.6873e-10
v  ǁVelocityǁ          1.1062e-07          15.721          2.1449          0.4673
v  Pressure                -31967      1.2376e+05           29155          -10323
v  k                   2.2393e-11          3.3371        0.025649         0.02349
v  omega                   91.729       4.932e+07      8.3702e+05           66742
v  TurbVisc            4.4116e-16         0.24654         0.10851         0.21738
v  CourantNb           4.5437e-09         0.34549        0.021323       0.0035988
v  FourierNb            0.0012525          1.0124         0.16351        0.043763
v  total_pressure           69358      2.2509e+05      1.3048e+05           91002


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012551           1.013         0.18483        0.047361


 TIME FOR THE TIME STEP               48:        0.93554E+01

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


 INSTANT    0.245000000E-04   TIME STEP NUMBER              49
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.335751318E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.389475723E-06
Free inlet               13         400         0.157119974E-03
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 0.18513E+01
   Friction velocity        uet   :  0.20661E-03 0.14515E+01
   Friction velocity        uk    :  0.20661E-03 0.19802E+01
   Dimensionless distance   yplus :  0.51595E-03 0.47845E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43674E-01       8   0.43152E-04   0.75144E+00 0.68550E+03 
c  Velocity[X]                                      0.69372E+00 
c  Velocity[Y]                                      0.57726E-01 
c  Velocity[Z]                                      0.75802E-06 
c  Pressure     0.10667E-06    2122   0.22246E-02   0.36048E+00 0.11652E+05 
c  k            0.29649E-02       5   0.65063E-08   0.70962E-02 0.45694E+04 
c  omega        0.10995E+06       5   0.29836E-07   0.44343E+13 0.21068E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0096376          15.596          2.1206         0.46508
v  Velocity[Y]          -0.073192          3.9059         0.20908        0.028746
v  Velocity[Z]         -0.0028492       0.0028486      1.2209e-07      3.0383e-10
v  ǁVelocityǁ          1.0209e-07          15.737          2.1447         0.46747
v  Pressure                -31659      1.2407e+05           29046          -10404
v  k                   2.3545e-11          3.3348        0.025634        0.023489
v  omega                     91.9      4.9122e+07      8.3505e+05           66565
v  TurbVisc            4.6482e-16         0.24354         0.10791          0.2173
v  CourantNb           4.4544e-09         0.34624        0.021321       0.0035989
v  FourierNb            0.0012525          1.0091         0.16157        0.043534
v  total_pressure           69666      2.2539e+05      1.3037e+05           90921


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012552          1.0097         0.18289        0.047133


 TIME FOR THE TIME STEP               49:        0.97439E+01

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


 INSTANT    0.250000000E-04   TIME STEP NUMBER              50
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.332326273E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.396852217E-06
Free inlet               13         400         0.157112598E-03
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 0.18513E+01
   Friction velocity        uet   :  0.20273E-03 0.14512E+01
   Friction velocity        uk    :  0.20273E-03 0.19801E+01
   Dimensionless distance   yplus :  0.50632E-03 0.47842E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100


 Write intermediate restart files
   checkpoint at iteration         50, Physical time    0.25000E-04


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

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Variables principales écrites dans le fichier de reprise : 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                            
  Coefficients de C.L. écrits dans le fichier de reprise : checkpoint/auxiliary
   End writing the wall distance                        
 End writing


 Time for restart files:    0.32578E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43676E-01       8   0.48220E-04   0.73699E+00 0.67887E+03 
c  Velocity[X]                                      0.67734E+00 
c  Velocity[Y]                                      0.59645E-01 
c  Velocity[Z]                                      0.62640E-06 
c  Pressure     0.15724E-06    2131   0.14939E-02   0.52498E+00 0.75890E+04 
c  k            0.29649E-02       5   0.67196E-08   0.67846E-02 0.44712E+04 
c  omega        0.10994E+06       5   0.77948E-08   0.40573E+13 0.20154E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0091414           15.47          2.1204         0.46525
v  Velocity[Y]          -0.074158            3.95         0.20907         0.02874
v  Velocity[Z]         -0.0026952        0.002619      1.1734e-07      3.4483e-10
v  ǁVelocityǁ          7.1208e-08          15.613          2.1445         0.46764
v  Pressure                -31971      1.2428e+05           29287          -10329
v  k                   2.4732e-11          3.3325         0.02562        0.023488
v  omega                   92.067      4.9083e+07      8.3317e+05           66392
v  TurbVisc            4.8865e-16         0.24353         0.10791          0.2173
v  CourantNb           5.3365e-09         0.34497        0.021319       0.0035991
v  FourierNb            0.0012525          1.0059         0.16145        0.043478
v  total_pressure           69354       2.256e+05      1.3061e+05           90996


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012552          1.0065         0.18277        0.047077


 TIME FOR THE TIME STEP               50:        0.10162E+02

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


 INSTANT    0.255000000E-04   TIME STEP NUMBER              51
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.461476309E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.404308927E-06
Free inlet               13         400         0.157105141E-03
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 0.18514E+01
   Friction velocity        uet   :  0.13917E-03 0.14514E+01
   Friction velocity        uk    :  0.13917E-03 0.19802E+01
   Dimensionless distance   yplus :  0.34755E-03 0.47846E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43678E-01       8   0.50496E-04   0.70775E+00 0.66526E+03 
c  Velocity[X]                                      0.63104E+00 
c  Velocity[Y]                                      0.76715E-01 
c  Velocity[Z]                                      0.52100E-06 
c  Pressure     0.75549E-07    1941   0.16253E-02   0.25895E+00 0.27791E+05 
c  k            0.29649E-02       5   0.71643E-08   0.65110E-02 0.43833E+04 
c  omega        0.10994E+06       5   0.31305E-07   0.37888E+13 0.19476E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0096861          15.387          2.1202         0.46541
v  Velocity[Y]          -0.075112          3.9284         0.20905        0.028735
v  Velocity[Z]         -0.0025589       0.0024131      1.1299e-07       3.856e-10
v  ǁVelocityǁ          8.1853e-08          15.529          2.1443          0.4678
v  Pressure                -31665      1.2368e+05           28713          -10715
v  k                   2.5929e-11          3.3326        0.025605        0.023486
v  omega                   92.223      4.9078e+07      8.3138e+05           66231
v  TurbVisc            5.1318e-16         0.24353          0.1077         0.21727
v  CourantNb           4.5486e-09         0.34304        0.021316       0.0035992
v  FourierNb            0.0012525          1.0027         0.16077        0.043371
v  total_pressure           69660        2.25e+05      1.3004e+05           90610


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012553          1.0034         0.18208         0.04697


 TIME FOR THE TIME STEP               51:        0.91901E+01

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


 INSTANT    0.260000000E-04   TIME STEP NUMBER              52
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.177456091E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.411491002E-06
Free inlet               13         400         0.157097959E-03
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 0.18517E+01
   Friction velocity        uet   :  0.16605E-03 0.14502E+01
   Friction velocity        uk    :  0.16605E-03 0.19794E+01
   Dimensionless distance   yplus :  0.41019E-03 0.47825E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43680E-01       9   0.46231E-04   0.67157E+00 0.64802E+03 
c  Velocity[X]                                      0.60632E+00 
c  Velocity[Y]                                      0.65250E-01 
c  Velocity[Z]                                      0.43289E-06 
c  Pressure     0.10629E-06    2044   0.10392E-02   0.36118E+00 0.22143E+05 
c  k            0.29648E-02       5   0.65677E-08   0.62234E-02 0.42885E+04 
c  omega        0.10994E+06       5   0.82486E-08   0.35056E+13 0.18736E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.010472          15.388            2.12         0.46557
v  Velocity[Y]          -0.076052          3.9707         0.20904        0.028729
v  Velocity[Z]         -0.0024349       0.0022299       1.087e-07      4.1942e-10
v  ǁVelocityǁ          1.1274e-07          15.508          2.1441         0.46797
v  Pressure                -31974      1.2375e+05           28922          -10435
v  k                   2.7164e-11          3.3306         0.02559        0.023485
v  omega                   92.393       4.908e+07      8.2967e+05           66073
v  TurbVisc             5.378e-16          0.2464         0.10806         0.21731
v  CourantNb           2.7196e-09         0.34237        0.021314       0.0035994
v  FourierNb            0.0012525          1.0009         0.16171        0.043433
v  total_pressure           69351      2.2507e+05      1.3025e+05           90890


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012553          1.0016         0.18302        0.047032


 TIME FOR THE TIME STEP               52:        0.94874E+01

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


 INSTANT    0.265000000E-04   TIME STEP NUMBER              53
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.591304891E-24
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.418909047E-06
Free inlet               13         400         0.157090541E-03
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 0.18519E+01
   Friction velocity        uet   :  0.22744E-03 0.14484E+01
   Friction velocity        uk    :  0.22744E-03 0.19781E+01
   Dimensionless distance   yplus :  0.56799E-03 0.47795E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43682E-01       8   0.37832E-04   0.62987E+00 0.62757E+03 
c  Velocity[X]                                      0.57503E+00 
c  Velocity[Y]                                      0.54834E-01 
c  Velocity[Z]                                      0.35746E-06 
c  Pressure     0.47775E-07    1939   0.14113E-02   0.16669E+00 0.18868E+05 
c  k            0.29648E-02       5   0.62401E-08   0.59560E-02 0.41983E+04 
c  omega        0.10994E+06       5   0.32799E-07   0.32996E+13 0.18177E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0093036          15.423          2.1198         0.46574
v  Velocity[Y]          -0.076981          3.9251         0.20903        0.028724
v  Velocity[Z]         -0.0023218       0.0020669      1.0505e-07      4.5933e-10
v  ǁVelocityǁ          7.9408e-08          15.547          2.1439         0.46814
v  Pressure                -31664      1.2363e+05           28663          -10677
v  k                   2.8424e-11          3.3292        0.025576        0.023484
v  omega                   92.548      4.9084e+07      8.2803e+05           65925
v  TurbVisc            5.6293e-16          0.2439         0.10775         0.21727
v  CourantNb           3.0808e-09         0.34231        0.021312       0.0035995
v  FourierNb            0.0012525         0.99633         0.16045        0.043269
v  total_pressure           69661      2.2496e+05      1.2999e+05           90648


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012554         0.99703         0.18176        0.046868


 TIME FOR THE TIME STEP               53:        0.91643E+01

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


 INSTANT    0.270000000E-04   TIME STEP NUMBER              54
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.705462278E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.426119083E-06
Free inlet               13         400         0.157083331E-03
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 0.18520E+01
   Friction velocity        uet   :  0.16534E-03 0.14458E+01
   Friction velocity        uk    :  0.16534E-03 0.19763E+01
   Dimensionless distance   yplus :  0.41291E-03 0.47751E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43683E-01      10   0.39729E-04   0.61926E+00 0.62226E+03 
c  Velocity[X]                                      0.56638E+00 
c  Velocity[Y]                                      0.52880E-01 
c  Velocity[Z]                                      0.30011E-06 
c  Pressure     0.24623E-06    2069   0.10243E-02   0.84252E+00 0.39632E+05 
c  k            0.29648E-02       5   0.52126E-08   0.56867E-02 0.41052E+04 
c  omega        0.10994E+06       5   0.87387E-08   0.30704E+13 0.17536E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0093602          15.458          2.1196         0.46591
v  Velocity[Y]          -0.077896          3.9665         0.20901        0.028717
v  Velocity[Z]         -0.0022577       0.0019196      1.0189e-07      5.0235e-10
v  ǁVelocityǁ          8.5332e-08          15.604          2.1437         0.46831
v  Pressure                -31973      1.2444e+05           29657          -10116
v  k                   2.9718e-11          3.3245        0.025561        0.023482
v  omega                   92.712      4.9088e+07      8.2645e+05           65779
v  TurbVisc            5.8856e-16         0.24606         0.10793         0.21728
v  CourantNb           4.7575e-09         0.34305         0.02131       0.0035997
v  FourierNb            0.0012525         0.99546         0.16118        0.043301
v  total_pressure           69352      2.2576e+05      1.3098e+05           91209


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012554         0.99617         0.18249        0.046901


 TIME FOR THE TIME STEP               54:        0.95861E+01

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


 INSTANT    0.275000000E-04   TIME STEP NUMBER              55
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.128949703E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.433697725E-06
Free inlet               13         400         0.157075752E-03
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 0.18521E+01
   Friction velocity        uet   :  0.19356E-03 0.14437E+01
   Friction velocity        uk    :  0.19356E-03 0.19749E+01
   Dimensionless distance   yplus :  0.48340E-03 0.47718E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43685E-01       8   0.54965E-04   0.59057E+00 0.60767E+03 
c  Velocity[X]                                      0.53173E+00 
c  Velocity[Y]                                      0.58838E-01 
c  Velocity[Z]                                      0.24970E-06 
c  Pressure     0.92626E-07    2165   0.30801E-02   0.32486E+00 0.23193E+05 
c  k            0.29647E-02       5   0.53927E-08   0.54381E-02 0.40172E+04 
c  omega        0.10994E+06       5   0.34356E-07   0.29129E+13 0.17080E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0096929          15.509          2.1194         0.46607
v  Velocity[Y]            -0.0788          3.9191         0.20899         0.02871
v  Velocity[Z]         -0.0021981       0.0017888      9.8905e-08      5.4214e-10
v  ǁVelocityǁ          5.9044e-08          15.654          2.1435         0.46847
v  Pressure                -31660      1.2484e+05           29319          -10381
v  k                   3.1019e-11          3.3217        0.025546        0.023481
v  omega                   92.845      4.9091e+07      8.2494e+05           65643
v  TurbVisc            6.1469e-16         0.24353          0.1072         0.21719
v  CourantNb           3.5767e-09         0.34411        0.021308       0.0035999
v  FourierNb            0.0012525         0.98993         0.15891        0.043032
v  total_pressure           69665      2.2616e+05      1.3064e+05           90944


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012555         0.99064         0.18022        0.046631


 TIME FOR THE TIME STEP               55:        0.99131E+01

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


 INSTANT    0.280000000E-04   TIME STEP NUMBER              56
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.977236346E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.441039946E-06
Free inlet               13         400         0.157068410E-03
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 0.18522E+01
   Friction velocity        uet   :  0.12607E-03 0.14420E+01
   Friction velocity        uk    :  0.12607E-03 0.19738E+01
   Dimensionless distance   yplus :  0.31483E-03 0.47690E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43687E-01       8   0.55728E-04   0.61135E+00 0.61826E+03 
c  Velocity[X]                                      0.54636E+00 
c  Velocity[Y]                                      0.64992E-01 
c  Velocity[Z]                                      0.20503E-06 
c  Pressure     0.34206E-06    2214   0.14870E-02   0.12133E+01 0.38151E+05 
c  k            0.29647E-02       5   0.50468E-08   0.52088E-02 0.39343E+04 
c  omega        0.10994E+06       5   0.92611E-08   0.27248E+13 0.16521E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0096282          15.412          2.1192         0.46624
v  Velocity[Y]          -0.079692          3.9056         0.20897        0.028703
v  Velocity[Z]         -0.0021004       0.0017304      9.5943e-08      5.7405e-10
v  ǁVelocityǁ          1.1077e-07          15.556          2.1433         0.46865
v  Pressure                -31972      1.2579e+05           30403           -9844
v  k                   3.2366e-11          3.3167        0.025531         0.02348
v  omega                   92.983      4.9094e+07      8.2349e+05           65508
v  TurbVisc            6.4131e-16         0.24352         0.10726         0.21719
v  CourantNb           4.7752e-09         0.34509        0.021306          0.0036
v  FourierNb            0.0012525         0.99096         0.15893        0.042994
v  total_pressure           69353      2.2712e+05      1.3173e+05           91481


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012555         0.99169         0.18023        0.046594


 TIME FOR THE TIME STEP               56:        0.10075E+02

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


 INSTANT    0.285000000E-04   TIME STEP NUMBER              57
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.131799598E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.448725705E-06
Free inlet               13         400         0.157060724E-03
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 0.18522E+01
   Friction velocity        uet   :  0.20712E-03 0.14428E+01
   Friction velocity        uk    :  0.20712E-03 0.19745E+01
   Dimensionless distance   yplus :  0.51726E-03 0.47706E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43689E-01       8   0.50325E-04   0.56545E+00 0.59459E+03 
c  Velocity[X]                                      0.50145E+00 
c  Velocity[Y]                                      0.64002E-01 
c  Velocity[Z]                                      0.17243E-06 
c  Pressure     0.12838E-06    2231   0.44133E-02   0.45157E+00 0.29506E+05 
c  k            0.29647E-02       5   0.52872E-08   0.50102E-02 0.38611E+04 
c  omega        0.10994E+06       5   0.35979E-07   0.26059E+13 0.16156E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.010036          15.434          2.1191         0.46641
v  Velocity[Y]          -0.080572          3.9572         0.20895        0.028696
v  Velocity[Z]         -0.0020128       0.0016759      9.3347e-08      6.0687e-10
v  ǁVelocityǁ          4.9838e-08          15.553          2.1432         0.46881
v  Pressure                -31658      1.2614e+05           29858          -10200
v  k                   3.3718e-11          3.3126        0.025516        0.023479
v  omega                   93.097      4.9098e+07       8.221e+05           65382
v  TurbVisc            6.6841e-16         0.24352         0.10676         0.21712
v  CourantNb           4.5606e-09         0.34347        0.021305       0.0036002
v  FourierNb            0.0012525         0.98729         0.15762        0.042819
v  total_pressure           69667      2.2747e+05      1.3118e+05           91125


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012556         0.98804         0.17892        0.046419


 TIME FOR THE TIME STEP               57:        0.10106E+02

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


 INSTANT    0.290000000E-04   TIME STEP NUMBER              58
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.215583947E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.456122085E-06
Free inlet               13         400         0.157053328E-03
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 0.18521E+01
   Friction velocity        uet   :  0.68826E-04 0.14427E+01
   Friction velocity        uk    :  0.68826E-04 0.19745E+01
   Dimensionless distance   yplus :  0.17188E-03 0.47707E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43690E-01       8   0.47929E-04   0.54889E+00 0.58582E+03 
c  Velocity[X]                                      0.49173E+00 
c  Velocity[Y]                                      0.57160E-01 
c  Velocity[Z]                                      0.14431E-06 
c  Pressure     0.10231E-06    2105   0.17670E-02   0.36754E+00 0.72457E+04 
c  k            0.29647E-02       5   0.50996E-08   0.48136E-02 0.37870E+04 
c  omega        0.10994E+06       5   0.98159E-08   0.24500E+13 0.15667E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0096581          15.467          2.1189         0.46658
v  Velocity[Y]          -0.081441          3.9085         0.20894        0.028688
v  Velocity[Z]         -0.0019373       0.0016366      9.0804e-08       6.365e-10
v  ǁVelocityǁ          1.1648e-07          15.586           2.143         0.46898
v  Pressure                -31983       1.258e+05           29662          -10310
v  k                   3.5147e-11          3.3108        0.025501        0.023478
v  omega                   93.217      4.9101e+07      8.2076e+05           65257
v  TurbVisc            6.9599e-16         0.24351         0.10686         0.21713
v  CourantNb           4.8875e-09         0.34389        0.021303       0.0036004
v  FourierNb            0.0012525         0.99008         0.15777        0.042797
v  total_pressure           69342      2.2713e+05      1.3099e+05           91015


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012556         0.99084         0.17907        0.046397


 TIME FOR THE TIME STEP               58:        0.97063E+01

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


 INSTANT    0.295000000E-04   TIME STEP NUMBER              59
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.267961282E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.463516018E-06
Free inlet               13         400         0.157045934E-03
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 0.18521E+01
   Friction velocity        uet   :  0.21119E-03 0.14417E+01
   Friction velocity        uk    :  0.21119E-03 0.19738E+01
   Dimensionless distance   yplus :  0.52743E-03 0.47691E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43692E-01       8   0.51391E-04   0.55328E+00 0.58815E+03 
c  Velocity[X]                                      0.50120E+00 
c  Velocity[Y]                                      0.52080E-01 
c  Velocity[Z]                                      0.12094E-06 
c  Pressure     0.19996E-06    2177   0.15039E-02   0.70402E+00 0.15611E+05 
c  k            0.29646E-02       5   0.47163E-08   0.46156E-02 0.37107E+04 
c  omega        0.10993E+06       5   0.18545E-08   0.17060E+13 0.13074E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.00952            15.5          2.1187         0.46674
v  Velocity[Y]          -0.082298          3.9423         0.20892         0.02868
v  Velocity[Z]         -0.0018726       0.0016032      8.8311e-08        6.62e-10
v  ǁVelocityǁ          5.9331e-08          15.644          2.1428         0.46915
v  Pressure                -31983      1.2631e+05           30136          -10081
v  k                   3.6598e-11          3.3064        0.025486        0.023476
v  omega                   93.339      4.9104e+07      8.1947e+05           65139
v  TurbVisc            7.2403e-16         0.24556         0.10693         0.21713
v  CourantNb           4.5366e-09         0.34481        0.021301       0.0036005
v  FourierNb            0.0012525         0.98692         0.15777        0.042766
v  total_pressure           69342      2.2764e+05      1.3146e+05           91244


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012556         0.98769         0.17908        0.046367


 TIME FOR THE TIME STEP               59:        0.99383E+01

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


 INSTANT    0.300000000E-04   TIME STEP NUMBER              60
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.443898721E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.471018230E-06
Free inlet               13         400         0.157038432E-03
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 0.18520E+01
   Friction velocity        uet   :  0.12725E-03 0.14416E+01
   Friction velocity        uk    :  0.12725E-03 0.19738E+01
   Dimensionless distance   yplus :  0.31781E-03 0.47691E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        802
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43694E-01       8   0.52331E-04   0.55728E+00 0.59026E+03 
c  Velocity[X]                                      0.49557E+00 
c  Velocity[Y]                                      0.61709E-01 
c  Velocity[Z]                                      0.10171E-06 
c  Pressure     0.33132E-07    1864   0.27568E-02   0.11919E+00 0.22726E+05 
c  k            0.29646E-02       5   0.49564E-08   0.13928E-01 0.64502E+04 
c  omega        0.10994E+06       5   0.44270E-07   0.32080E+16 0.56666E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.012125          15.547          2.1186         0.46691
v  Velocity[Y]          -0.083144          3.8879          0.2089        0.028674
v  Velocity[Z]         -0.0018147       0.0015737      8.5863e-08      6.8296e-10
v  ǁVelocityǁ          3.8521e-07          15.689          2.1427         0.46931
v  Pressure                -31657      1.2582e+05           29659          -10386
v  k                   3.8042e-11          3.3042        0.025469        0.023475
v  omega                   93.454      6.7696e+07      8.1938e+05           65053
v  TurbVisc            7.5252e-16         0.24351         0.10666         0.21709
v  CourantNb           4.8681e-09         0.34569          0.0213       0.0036007
v  FourierNb            0.0012525         0.98514         0.15697        0.042645
v  total_pressure           69668      2.2714e+05      1.3098e+05           90939


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012557         0.98592         0.17827        0.046245


 TIME FOR THE TIME STEP               60:        0.89146E+01

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


 INSTANT    0.305000000E-04   TIME STEP NUMBER              61
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.102040483E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.478279217E-06
Free inlet               13         400         0.157031171E-03
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 0.18519E+01
   Friction velocity        uet   :  0.35457E-03 0.14418E+01
   Friction velocity        uk    :  0.35457E-03 0.19740E+01
   Dimensionless distance   yplus :  0.88538E-03 0.47695E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        802
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43695E-01       8   0.51634E-04   0.56655E+00 0.59515E+03 
c  Velocity[X]                                      0.50274E+00 
c  Velocity[Y]                                      0.63810E-01 
c  Velocity[Z]                                      0.85062E-07 
c  Pressure     0.11723E-06    2058   0.15202E-02   0.42238E+00 0.12499E+05 
c  k            0.29646E-02       5   0.58837E-08   0.10743E+00 0.17927E+05 
c  omega        0.10994E+06       5   0.10367E-07   0.18538E+15 0.13625E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.011594           15.45          2.1184         0.46707
v  Velocity[Y]          -0.083979          3.8684         0.20888        0.028666
v  Velocity[Z]         -0.0017669       0.0015488      8.3777e-08        7.07e-10
v  ǁVelocityǁ          6.3061e-08          15.591          2.1425         0.46948
v  Pressure                -31944      1.2583e+05           29765          -10254
v  k                    3.959e-11          3.3016        0.025448        0.023474
v  omega                   93.577      5.2559e+07      8.1794e+05           64936
v  TurbVisc            7.8146e-16         0.24557         0.10681          0.2171
v  CourantNb           2.9208e-08         0.34542        0.021299       0.0036009
v  FourierNb            0.0012525         0.98296         0.15741        0.042664
v  total_pressure           69381      2.2715e+05      1.3109e+05           91071


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012557         0.98375         0.17871        0.046265


 TIME FOR THE TIME STEP               61:        0.95593E+01

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


 INSTANT    0.310000000E-04   TIME STEP NUMBER              62
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.708693452E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.485695492E-06
Free inlet               13         400         0.157023755E-03
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 0.18517E+01
   Friction velocity        uet   :  0.29419E-03 0.14326E+01
   Friction velocity        uk    :  0.29419E-03 0.19675E+01
   Dimensionless distance   yplus :  0.73457E-03 0.47539E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43697E-01       8   0.53482E-04   0.50582E+00 0.56234E+03 
c  Velocity[X]                                      0.44780E+00 
c  Velocity[Y]                                      0.58019E-01 
c  Velocity[Z]                                      0.72109E-07 
c  Pressure     0.11643E-06    1959   0.12632E-02   0.41584E+00 0.30048E+05 
c  k            0.29646E-02       5   0.66159E-08   0.67123E-02 0.44837E+04 
c  omega        0.10994E+06       5   0.40232E-07   0.36921E+15 0.19232E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0075662          15.378          2.1182         0.46723
v  Velocity[Y]          -0.084803          3.9166         0.20887        0.028659
v  Velocity[Z]         -0.0017314        0.001528      8.1736e-08      7.2816e-10
v  ǁVelocityǁ          1.1965e-07          15.521          2.1423         0.46964
v  Pressure                -31668       1.255e+05           29153          -10678
v  k                   4.1087e-11          3.2969        0.025432        0.023473
v  omega                   93.695      4.9115e+07      8.1641e+05           64823
v  TurbVisc            8.1084e-16         0.24375         0.10677         0.21709
v  CourantNb           5.6059e-09         0.34462        0.021297       0.0036011
v  FourierNb            0.0012525         0.97977         0.15705        0.042593
v  total_pressure           69657      2.2682e+05      1.3048e+05           90647


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012558         0.98057         0.17835        0.046194


 TIME FOR THE TIME STEP               62:        0.92336E+01

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


 INSTANT    0.315000000E-04   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.106835546E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.492809382E-06
Free inlet               13         400         0.157016641E-03
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 0.18516E+01
   Friction velocity        uet   :  0.68734E-04 0.14364E+01
   Friction velocity        uk    :  0.68733E-04 0.19704E+01
   Dimensionless distance   yplus :  0.16970E-03 0.47607E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43699E-01      10   0.52270E-04   0.48581E+00 0.55110E+03 
c  Velocity[X]                                      0.43612E+00 
c  Velocity[Y]                                      0.49695E-01 
c  Velocity[Z]                                      0.61072E-07 
c  Pressure     0.19248E-06    2037   0.10890E-02   0.70291E+00 0.22627E+05 
c  k            0.29645E-02       5   0.65905E-08   0.46440E-02 0.37318E+04 
c  omega        0.10994E+06       5   0.11297E-07   0.10260E+15 0.10140E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0076402          15.406          2.1181         0.46739
v  Velocity[Y]          -0.085617          3.8748         0.20885        0.028652
v  Velocity[Z]         -0.0017066       0.0015123       8.004e-08      7.5267e-10
v  ǁVelocityǁ          6.8764e-08          15.523          2.1421          0.4698
v  Pressure                -31987      1.2437e+05           28308          -10950
v  k                   4.2555e-11          3.2938        0.025417        0.023471
v  omega                   93.832      4.9117e+07       8.151e+05           64714
v  TurbVisc            8.4066e-16         0.24715          0.1071         0.21711
v  CourantNb           3.8714e-09          0.3447        0.021295       0.0036012
v  FourierNb            0.0012525          1.4164          0.1583         0.04267
v  total_pressure           69338      2.2569e+05      1.2963e+05           90375


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012558          1.4172          0.1796        0.046271


 TIME FOR THE TIME STEP               63:        0.94792E+01

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


 INSTANT    0.320000000E-04   TIME STEP NUMBER              64
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.538701374E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.499867508E-06
Free inlet               13         400         0.157009582E-03
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 0.18514E+01
   Friction velocity        uet   :  0.94989E-04 0.14379E+01
   Friction velocity        uk    :  0.94988E-04 0.19714E+01
   Dimensionless distance   yplus :  0.23719E-03 0.47633E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        801
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43700E-01       8   0.54445E-04   0.47383E+00 0.54426E+03 
c  Velocity[X]                                      0.42530E+00 
c  Velocity[Y]                                      0.48527E-01 
c  Velocity[Z]                                      0.52991E-07 
c  Pressure     0.77657E-07    1927   0.18125E-02   0.27819E+00 0.12025E+05 
c  k            0.29645E-02       5   0.59444E-08   0.46887E-02 0.37519E+04 
c  omega        0.10993E+06       5   0.23144E-08   0.31079E+14 0.55808E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.021046          15.428          2.1179         0.46755
v  Velocity[Y]          -0.086426          3.9163         0.20883        0.028644
v  Velocity[Z]          -0.001682       0.0014972      7.8258e-08      7.7007e-10
v  ǁVelocityǁ          3.5818e-08          15.555           2.142         0.46996
v  Pressure                -32013      1.2407e+05           28301          -10815
v  k                   4.4124e-11          3.2898        0.025402         0.02347
v  omega                   93.992      4.9119e+07      8.1391e+05           64612
v  TurbVisc             8.709e-16          0.2435         0.10651         0.21703
v  CourantNb           3.8476e-09         0.34385        0.021293       0.0036014
v  FourierNb            0.0012525         0.97812         0.15621        0.042414
v  total_pressure           69312       2.254e+05      1.2963e+05           90510


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012559         0.97894          0.1775        0.046016


 TIME FOR THE TIME STEP               64:        0.91230E+01

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


 INSTANT    0.325000000E-04   TIME STEP NUMBER              65
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.823787880E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.507021988E-06
Free inlet               13         400         0.157002428E-03
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 0.18512E+01
   Friction velocity        uet   :  0.65450E-04 0.14364E+01
   Friction velocity        uk    :  0.65450E-04 0.19705E+01
   Dimensionless distance   yplus :  0.16344E-03 0.47609E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        802
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43702E-01       8   0.51420E-04   0.48980E+00 0.55335E+03 
c  Velocity[X]                                      0.43229E+00 
c  Velocity[Y]                                      0.57517E-01 
c  Velocity[Z]                                      0.44685E-07 
c  Pressure     0.77782E-07    1867   0.19325E-02   0.28452E+00 0.25736E+04 
c  k            0.29645E-02       5   0.51511E-08   0.49493E-02 0.38570E+04 
c  omega        0.10992E+06       5   0.21746E-08   0.10384E+16 0.32252E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.037752          15.465          2.1177         0.46771
v  Velocity[Y]          -0.087221          3.8602         0.20882        0.028637
v  Velocity[Z]         -0.0016593       0.0014828      7.6663e-08      7.8752e-10
v  ǁVelocityǁ          7.3574e-08          15.607          2.1418         0.47012
v  Pressure                -31837      1.2362e+05           28243          -10828
v  k                   4.5644e-11           3.286        0.025387        0.023469
v  omega                   94.156      4.9822e+07      8.1352e+05           64531
v  TurbVisc            9.0155e-16         0.24556         0.10655         0.21702
v  CourantNb           8.1833e-09         0.34439        0.021291       0.0036016
v  FourierNb            0.0012525          0.9696          0.1562         0.04238
v  total_pressure           69488      2.2495e+05      1.2957e+05           90497


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012559         0.97044         0.17749        0.045982


 TIME FOR THE TIME STEP               65:        0.89074E+01

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


 INSTANT    0.330000000E-04   TIME STEP NUMBER              66
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.590335539E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.514156602E-06
Free inlet               13         400         0.156995293E-03
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 0.18509E+01
   Friction velocity        uet   :  0.13937E-03 0.14362E+01
   Friction velocity        uk    :  0.13937E-03 0.19704E+01
   Dimensionless distance   yplus :  0.34807E-03 0.47608E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        802
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43703E-01       8   0.48973E-04   0.45962E+00 0.53603E+03 
c  Velocity[X]                                      0.40640E+00 
c  Velocity[Y]                                      0.53228E-01 
c  Velocity[Z]                                      0.37453E-07 
c  Pressure     0.58168E-07    2104   0.23170E-02   0.20905E+00 0.23655E+05 
c  k            0.29645E-02       5   0.56361E-08   0.56776E-02 0.41335E+04 
c  omega        0.10994E+06       5   0.50673E-07   0.80084E+13 0.28323E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.045768          15.368          2.1176         0.46787
v  Velocity[Y]          -0.088003          3.8898          0.2088         0.02863
v  Velocity[Z]         -0.0016359       0.0014689      7.5211e-08      8.0465e-10
v  ǁVelocityǁ          5.0849e-08          15.511          2.1417         0.47028
v  Pressure                -31646      1.2389e+05           29011          -10488
v  k                   4.7184e-11          3.2805        0.025371        0.023468
v  omega                   94.322      4.9125e+07      8.1248e+05           64440
v  TurbVisc            9.3261e-16         0.24572         0.10627         0.21697
v  CourantNb           4.4134e-09         0.34301         0.02129       0.0036017
v  FourierNb            0.0012525         0.96331         0.15549        0.042276
v  total_pressure           69679      2.2522e+05      1.3034e+05           90837


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001256         0.96416         0.17678        0.045878


 TIME FOR THE TIME STEP               66:        0.97318E+01

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


 INSTANT    0.335000000E-04   TIME STEP NUMBER              67
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.659644227E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.521419528E-06
Free inlet               13         400         0.156988030E-03
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 0.18507E+01
   Friction velocity        uet   :  0.16877E-03 0.14361E+01
   Friction velocity        uk    :  0.16877E-03 0.19705E+01
   Dimensionless distance   yplus :  0.41736E-03 0.47609E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        802
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43705E-01       9   0.48516E-04   0.44007E+00 0.52450E+03 
c  Velocity[X]                                      0.39049E+00 
c  Velocity[Y]                                      0.49586E-01 
c  Velocity[Z]                                      0.31274E-07 
c  Pressure     0.15252E-06    1907   0.10097E-02   0.56072E+00 0.26059E+05 
c  k            0.29645E-02       5   0.59671E-08   0.38522E-02 0.34067E+04 
c  omega        0.10994E+06       4   0.86618E-08   0.20275E+13 0.14252E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.044733          15.312          2.1174         0.46803
v  Velocity[Y]          -0.088774          3.8539         0.20879        0.028621
v  Velocity[Z]         -0.0016141       0.0014569      7.3756e-08      8.1798e-10
v  ǁVelocityǁ          6.6773e-08          15.448          2.1415         0.47044
v  Pressure                -32327      1.2346e+05           28349          -10911
v  k                   4.8743e-11          3.2768        0.025357        0.023467
v  omega                   94.464      4.9127e+07       8.115e+05           64348
v  TurbVisc            9.6408e-16         0.24764         0.10638         0.21696
v  CourantNb           7.9218e-09         0.34162        0.021288       0.0036019
v  FourierNb            0.0012525          1.4215          0.1561        0.042297
v  total_pressure           68998      2.2478e+05      1.2967e+05           90414


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001256          1.4225         0.17739        0.045898


 TIME FOR THE TIME STEP               67:        0.90493E+01

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


 INSTANT    0.340000000E-04   TIME STEP NUMBER              68
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.138113313E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.528550696E-06
Free inlet               13         400         0.156980899E-03
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 0.18504E+01
   Friction velocity        uet   :  0.13809E-03 0.14347E+01
   Friction velocity        uk    :  0.13809E-03 0.19696E+01
   Dimensionless distance   yplus :  0.34095E-03 0.47588E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        804
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43706E-01       8   0.52808E-04   0.44618E+00 0.52812E+03 
c  Velocity[X]                                      0.38518E+00 
c  Velocity[Y]                                      0.61003E-01 
c  Velocity[Z]                                      0.28540E-07 
c  Pressure     0.64255E-07    2037   0.17151E-02   0.23333E+00 0.26226E+05 
c  k            0.29644E-02       5   0.28818E-07   0.19265E-01 0.76230E+04 
c  omega        0.10993E+06       5   0.44262E-06   0.48763E+16 0.69846E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.056448          15.357          2.1173         0.46819
v  Velocity[Y]          -0.089534          3.8998         0.20877        0.028612
v  Velocity[Z]          -0.001592        0.001445      7.2458e-08      8.3246e-10
v  ǁVelocityǁ          1.5642e-07          15.475          2.1414         0.47061
v  Pressure                -31875      1.2573e+05           28945          -10512
v  k                   5.0321e-11          3.2714        0.025338        0.023466
v  omega                    94.62      7.0029e+07      8.1274e+05           64303
v  TurbVisc            9.9593e-16         0.24366         0.10594         0.21689
v  CourantNb           4.6644e-09         0.34162        0.021287       0.0036021
v  FourierNb            0.0012525         0.95686         0.15475        0.042126
v  total_pressure           69450      2.2705e+05      1.3027e+05           90813


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012561         0.95772         0.17603        0.045729


 TIME FOR THE TIME STEP               68:        0.95030E+01

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


 INSTANT    0.345000000E-04   TIME STEP NUMBER              69
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.707077865E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.535870110E-06
Free inlet               13         400         0.156973580E-03
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 0.18502E+01
   Friction velocity        uet   :  0.25083E-03 0.14325E+01
   Friction velocity        uk    :  0.25083E-03 0.19681E+01
   Dimensionless distance   yplus :  0.62006E-03 0.47552E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        804
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43708E-01       9   0.58454E-04   0.43130E+00 0.51924E+03 
c  Velocity[X]                                      0.36783E+00 
c  Velocity[Y]                                      0.63466E-01 
c  Velocity[Z]                                      0.22478E-07 
c  Pressure     0.89046E-07    1910   0.10454E-02   0.31751E+00 0.16762E+05 
c  k            0.29644E-02       5   0.69355E-07   0.85986E-01 0.16114E+05 
c  omega        0.10995E+06       5   0.11529E-06   0.23407E+15 0.15306E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.050468          15.395          2.1171         0.46835
v  Velocity[Y]          -0.090284           3.916         0.20875        0.028605
v  Velocity[Z]         -0.0015727       0.0014354      7.1274e-08      8.4634e-10
v  ǁVelocityǁ          4.6279e-08          15.513          2.1412         0.47077
v  Pressure                -31650       1.241e+05           28559          -10720
v  k                   5.1918e-11          3.2665        0.025315        0.023464
v  omega                   94.745      5.4894e+07      8.1141e+05           64214
v  TurbVisc            1.0282e-15         0.24721         0.10615         0.21689
v  CourantNb           5.8868e-09         0.34198        0.021286       0.0036023
v  FourierNb            0.0012525          1.4442         0.15579        0.042202
v  total_pressure           69675      2.2543e+05      1.2988e+05           90605


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012561          1.4451         0.17708        0.045804


 TIME FOR THE TIME STEP               69:        0.90724E+01

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


 INSTANT    0.350000000E-04   TIME STEP NUMBER              70
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.193547339E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.543000508E-06
Free inlet               13         400         0.156966450E-03
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 0.18499E+01
   Friction velocity        uet   :  0.23329E-03 0.14294E+01
   Friction velocity        uk    :  0.23329E-03 0.19660E+01
   Dimensionless distance   yplus :  0.57697E-03 0.47501E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        803
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43709E-01       8   0.49741E-04   0.42743E+00 0.51690E+03 
c  Velocity[X]                                      0.36443E+00 
c  Velocity[Y]                                      0.62994E-01 
c  Velocity[Z]                                      0.18919E-07 
c  Pressure     0.45355E-07    1822   0.13051E-02   0.16574E+00 0.12209E+05 
c  k            0.29644E-02       5   0.19781E-07   0.63622E-02 0.43857E+04 
c  omega        0.10994E+06       5   0.10267E-06   0.34031E+15 0.18461E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.055499          15.314           2.117         0.46851
v  Velocity[Y]          -0.091023          3.8688         0.20873        0.028596
v  Velocity[Z]         -0.0015581       0.0014295       7.033e-08       8.627e-10
v  ǁVelocityǁ          5.7076e-08          15.441          2.1411         0.47093
v  Pressure                -32348      1.2511e+05           28755          -10643
v  k                   5.3532e-11          3.2607        0.025298        0.023463
v  omega                   94.882       5.034e+07       8.101e+05           64121
v  TurbVisc            1.0608e-15         0.24587         0.10578         0.21683
v  CourantNb           5.1029e-09         0.34328        0.021285       0.0036025
v  FourierNb            0.0012525         0.95281         0.15448        0.042044
v  total_pressure           68977      2.2643e+05      1.3008e+05           90682


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012562         0.95369         0.17576        0.045647


 TIME FOR THE TIME STEP               70:        0.87952E+01

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


 INSTANT    0.355000000E-04   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.483125177E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.550307959E-06
Free inlet               13         400         0.156959142E-03
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 0.18496E+01
   Friction velocity        uet   :  0.15750E-03 0.14283E+01
   Friction velocity        uk    :  0.15750E-03 0.19653E+01
   Dimensionless distance   yplus :  0.38921E-03 0.47485E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        804
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43711E-01       8   0.50157E-04   0.40780E+00 0.50489E+03 
c  Velocity[X]                                      0.35421E+00 
c  Velocity[Y]                                      0.53593E-01 
c  Velocity[Z]                                      0.18535E-07 
c  Pressure     0.42505E-07    1762   0.86787E-03   0.15424E+00 0.48344E+04 
c  k            0.29644E-02       5   0.10266E-07   0.47909E-02 0.38079E+04 
c  omega        0.10993E+06       5   0.85749E-07   0.15955E+15 0.12639E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.053118          15.362          2.1168         0.46867
v  Velocity[Y]          -0.091753          3.9168         0.20871        0.028587
v  Velocity[Z]         -0.0015418       0.0014229      6.9379e-08      8.7707e-10
v  ǁVelocityǁ          5.1948e-08          15.482          2.1409          0.4711
v  Pressure                -31885       1.251e+05           28861          -10590
v  k                   5.5164e-11          3.2534        0.025283        0.023462
v  omega                   95.002      4.9324e+07       8.095e+05           64047
v  TurbVisc            1.0938e-15         0.24769         0.10587         0.21682
v  CourantNb           5.2672e-09         0.34171        0.021283       0.0036026
v  FourierNb            0.0012525          1.4542         0.15512        0.042074
v  total_pressure           69440      2.2642e+05      1.3019e+05           90735


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012562          1.4552          0.1764        0.045676


 TIME FOR THE TIME STEP               71:        0.88116E+01

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


 INSTANT    0.360000000E-04   TIME STEP NUMBER              72
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.402604314E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.557575407E-06
Free inlet               13         400         0.156951875E-03
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 0.18493E+01
   Friction velocity        uet   :  0.26226E-03 0.14265E+01
   Friction velocity        uk    :  0.26226E-03 0.19642E+01
   Dimensionless distance   yplus :  0.64811E-03 0.47458E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        804
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43713E-01       8   0.50217E-04   0.40048E+00 0.50033E+03 
c  Velocity[X]                                      0.35469E+00 
c  Velocity[Y]                                      0.45790E-01 
c  Velocity[Z]                                      0.15178E-07 
c  Pressure     0.49425E-07    1728   0.84223E-03   0.18316E+00 0.72189E+04 
c  k            0.29643E-02       5   0.73629E-08   0.35681E-02 0.32879E+04 
c  omega        0.10994E+06       4   0.55662E-07   0.38244E+13 0.19568E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.053063            15.4          2.1167         0.46883
v  Velocity[Y]          -0.092474          3.8624         0.20869         0.02858
v  Velocity[Z]         -0.0015317       0.0014203       6.836e-08      8.8646e-10
v  ǁVelocityǁ          4.0082e-08          15.519          2.1408         0.47126
v  Pressure                -31647      1.2367e+05           28640          -10635
v  k                   5.6814e-11          3.2488        0.025268        0.023461
v  omega                   95.116      4.9315e+07      8.0871e+05           63974
v  TurbVisc            1.1271e-15          0.2461         0.10574         0.21678
v  CourantNb           2.5233e-09         0.34182        0.021282       0.0036028
v  FourierNb            0.0012525          1.4408         0.15475        0.042001
v  total_pressure           69678        2.25e+05      1.2996e+05           90690


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012563          1.4417         0.17603        0.045604


 TIME FOR THE TIME STEP               72:        0.91644E+01

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


 INSTANT    0.365000000E-04   TIME STEP NUMBER              73
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.140478532E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.564765135E-06
Free inlet               13         400         0.156944685E-03
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 0.18489E+01
   Friction velocity        uet   :  0.11677E-03 0.14239E+01
   Friction velocity        uk    :  0.11677E-03 0.19624E+01
   Dimensionless distance   yplus :  0.28857E-03 0.47415E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        804
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43714E-01      10   0.53274E-04   0.41122E+00 0.50699E+03 
c  Velocity[X]                                      0.36425E+00 
c  Velocity[Y]                                      0.46969E-01 
c  Velocity[Z]                                      0.13587E-07 
c  Pressure     0.17401E-06    2043   0.83801E-03   0.62783E+00 0.27563E+05 
c  k            0.29643E-02       5   0.67695E-08   0.31082E-02 0.30702E+04 
c  omega        0.10994E+06       4   0.93869E-08   0.15777E+13 0.12569E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.054835           15.43          2.1165           0.469
v  Velocity[Y]          -0.093185          3.9035         0.20867        0.028569
v  Velocity[Z]         -0.0015205       0.0014173      6.7358e-08      8.9358e-10
v  ǁVelocityǁ          5.2976e-08          15.549          2.1407         0.47143
v  Pressure                -32367       1.241e+05           29468          -10309
v  k                   5.8481e-11          3.2422        0.025254         0.02346
v  omega                   95.234      4.9316e+07      8.0792e+05           63898
v  TurbVisc            1.1608e-15         0.24728         0.10557         0.21674
v  CourantNb           4.2012e-09         0.34278        0.021281        0.003603
v  FourierNb            0.0012525          1.4696         0.15415        0.041906
v  total_pressure           68958      2.2542e+05      1.3079e+05           91016


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012563          1.4705         0.17543        0.045509


 TIME FOR THE TIME STEP               73:        0.10014E+02

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


 INSTANT    0.370000000E-04   TIME STEP NUMBER              74
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.377595025E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.572250810E-06
Free inlet               13         400         0.156937199E-03
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 0.18486E+01
   Friction velocity        uet   :  0.25237E-03 0.14121E+01
   Friction velocity        uk    :  0.25237E-03 0.19540E+01
   Dimensionless distance   yplus :  0.63007E-03 0.47213E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        804
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43716E-01       7   0.47828E-04   0.40689E+00 0.50431E+03 
c  Velocity[X]                                      0.35543E+00 
c  Velocity[Y]                                      0.51459E-01 
c  Velocity[Z]                                      0.12121E-07 
c  Pressure     0.43300E-07    1916   0.21137E-02   0.16030E+00 0.21850E+05 
c  k            0.29643E-02       5   0.65695E-08   0.29055E-02 0.29700E+04 
c  omega        0.10993E+06       4   0.25176E-08   0.68970E+12 0.83105E+03 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.049611          15.444          2.1164         0.46916
v  Velocity[Y]          -0.093887          3.8599         0.20865        0.028559
v  Velocity[Z]         -0.0015106       0.0014177      6.6434e-08      9.0001e-10
v  ǁVelocityǁ          4.4419e-07          15.561          2.1405         0.47159
v  Pressure                -31893      1.2403e+05           29072          -10584
v  k                   6.0164e-11          3.2351        0.025241        0.023459
v  omega                   95.324      4.9317e+07      8.0715e+05           63825
v  TurbVisc            1.1949e-15         0.24362         0.10508         0.21666
v  CourantNb            2.379e-09         0.34325         0.02128       0.0036032
v  FourierNb            0.0012525          0.9447         0.15229        0.041697
v  total_pressure           69432      2.2536e+05       1.304e+05           90741


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012564         0.94563         0.17357          0.0453


 TIME FOR THE TIME STEP               74:        0.92685E+01

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


 INSTANT    0.375000000E-04   TIME STEP NUMBER              75
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.722813684E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.579493599E-06
Free inlet               13         400         0.156929956E-03
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 0.18483E+01
   Friction velocity        uet   :  0.41689E-03 0.14150E+01
   Friction velocity        uk    :  0.41689E-03 0.19563E+01
   Dimensionless distance   yplus :  0.10408E-02 0.47267E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        804
   Total number of wall faces                   :       1140
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         75, Physical time    0.37500E-04


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

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Variables principales écrites dans le fichier de reprise : 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                            
  Coefficients de C.L. écrits dans le fichier de reprise : checkpoint/auxiliary
   End writing the wall distance                        
 End writing


 Time for restart files:    0.58710E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43717E-01       9   0.54499E-04   0.39329E+00 0.49581E+03 
c  Velocity[X]                                      0.34786E+00 
c  Velocity[Y]                                      0.45429E-01 
c  Velocity[Z]                                      0.10396E-07 
c  Pressure     0.13130E-06    2019   0.11276E-02   0.47657E+00 0.22911E+05 
c  k            0.29643E-02       5   0.69637E-08   0.27606E-02 0.28964E+04 
c  omega        0.10994E+06       4   0.57796E-07   0.18582E+13 0.13640E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.046424          15.454          2.1162         0.46933
v  Velocity[Y]          -0.094571          3.8811         0.20863        0.028552
v  Velocity[Z]         -0.0015014       0.0014181      6.5501e-08      9.0332e-10
v  ǁVelocityǁ          4.4762e-07          15.599          2.1404         0.47175
v  Pressure                -31639      1.2414e+05           29437          -10226
v  k                   6.1864e-11          3.2265        0.025227        0.023458
v  omega                   95.423      4.9319e+07       8.064e+05           63758
v  TurbVisc            1.2293e-15         0.24497         0.10518         0.21665
v  CourantNb           1.9944e-08          0.3435        0.021278       0.0036034
v  FourierNb            0.0012525         0.94638         0.15277        0.041701
v  total_pressure           69686      2.2547e+05      1.3076e+05           91099


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012564         0.94734         0.17405        0.045304


 TIME FOR THE TIME STEP               75:        0.98842E+01

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


 INSTANT    0.380000000E-04   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.766434536E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.586898723E-06
Free inlet               13         400         0.156922551E-03
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 0.18479E+01
   Friction velocity        uet   :  0.23298E-03 0.14173E+01
   Friction velocity        uk    :  0.23298E-03 0.19581E+01
   Dimensionless distance   yplus :  0.57620E-03 0.47312E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        804
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43719E-01       8   0.52141E-04   0.39183E+00 0.49488E+03 
c  Velocity[X]                                      0.34411E+00 
c  Velocity[Y]                                      0.47718E-01 
c  Velocity[Z]                                      0.93051E-08 
c  Pressure     0.77770E-07    1997   0.17835E-02   0.28696E+00 0.33834E+05 
c  k            0.29642E-02       5   0.44537E-08   0.26052E-02 0.28150E+04 
c  omega        0.10994E+06       4   0.94372E-08   0.13959E+13 0.11823E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.038626          15.358          2.1161         0.46949
v  Velocity[Y]          -0.095245          3.8345         0.20861        0.028541
v  Velocity[Z]         -0.0014949       0.0014189      6.4792e-08      9.0987e-10
v  ǁVelocityǁ          2.1371e-07          15.502          2.1402         0.47191
v  Pressure                -32402      1.2372e+05           28859          -10772
v  k                    6.358e-11          3.2238        0.025214        0.023457
v  omega                    95.51      4.9321e+07      8.0567e+05           63688
v  TurbVisc             1.264e-15         0.24359         0.10492         0.21659
v  CourantNb           1.0174e-08         0.34264        0.021277       0.0036036
v  FourierNb            0.0012525         0.94457         0.15181        0.041573
v  total_pressure           68923      2.2505e+05      1.3018e+05           90553


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012565         0.94552         0.17309        0.045177


 TIME FOR THE TIME STEP               76:        0.93075E+01

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


 INSTANT    0.385000000E-04   TIME STEP NUMBER              77
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.325379249E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.594092058E-06
Free inlet               13         400         0.156915358E-03
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 0.18476E+01
   Friction velocity        uet   :  0.24587E-03 0.14080E+01
   Friction velocity        uk    :  0.24587E-03 0.19515E+01
   Dimensionless distance   yplus :  0.60792E-03 0.47151E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        804
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43720E-01       9   0.43956E-04   0.37321E+00 0.48298E+03 
c  Velocity[X]                                      0.33334E+00 
c  Velocity[Y]                                      0.39871E-01 
c  Velocity[Z]                                      0.85252E-08 
c  Pressure     0.74264E-07    1913   0.12255E-02   0.27077E+00 0.22215E+05 
c  k            0.29642E-02       5   0.55584E-08   0.25283E-02 0.27745E+04 
c  omega        0.10993E+06       4   0.23961E-08   0.56823E+12 0.75436E+03 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.036756          15.303           2.116         0.46965
v  Velocity[Y]          -0.095909          3.8854          0.2086        0.028532
v  Velocity[Z]         -0.0014881       0.0014181      6.4098e-08      9.1585e-10
v  ǁVelocityǁ          1.6686e-07          15.433          2.1401         0.47208
v  Pressure                -31892      1.2363e+05           29117          -10436
v  k                   6.5311e-11          3.2176        0.025201        0.023456
v  omega                   95.613      4.9322e+07      8.0496e+05           63621
v  TurbVisc            1.2991e-15         0.24512         0.10519         0.21659
v  CourantNb           9.8057e-09         0.34111        0.021275       0.0036037
v  FourierNb            0.0012525          1.2376         0.15301        0.041653
v  total_pressure           69433      2.2496e+05      1.3044e+05           90889


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012565          1.2385         0.17429        0.045256


 TIME FOR THE TIME STEP               77:        0.90243E+01

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


 INSTANT    0.390000000E-04   TIME STEP NUMBER              78
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.456371054E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.601446157E-06
Free inlet               13         400         0.156908004E-03
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 0.18472E+01
   Friction velocity        uet   :  0.31627E-03 0.14129E+01
   Friction velocity        uk    :  0.31627E-03 0.19552E+01
   Dimensionless distance   yplus :  0.78183E-03 0.47240E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        804
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43721E-01       8   0.50231E-04   0.34519E+00 0.46449E+03 
c  Velocity[X]                                      0.30662E+00 
c  Velocity[Y]                                      0.38568E-01 
c  Velocity[Z]                                      0.76640E-08 
c  Pressure     0.11190E-06    1937   0.10437E-02   0.41749E+00 0.24802E+05 
c  k            0.29642E-02       5   0.45607E-08   0.24309E-02 0.27218E+04 
c  omega        0.10994E+06       4   0.60802E-07   0.18263E+13 0.13523E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.03288          15.345          2.1158         0.46981
v  Velocity[Y]          -0.096565          3.8389         0.20858        0.028524
v  Velocity[Z]         -0.0014809       0.0014163      6.3569e-08      9.2265e-10
v  ǁVelocityǁ          9.4174e-08          15.463          2.1399         0.47224
v  Pressure                -31649      1.2316e+05           28579          -10764
v  k                   6.7058e-11          3.2136        0.025188        0.023455
v  omega                   95.707      4.9323e+07      8.0428e+05           63559
v  TurbVisc            1.3345e-15         0.24363         0.10491         0.21654
v  CourantNb           1.1539e-08         0.34091        0.021273       0.0036039
v  FourierNb            0.0012525         0.94382         0.15186        0.041503
v  total_pressure           69676      2.2448e+05       1.299e+05           90561


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012565         0.94481         0.17313        0.045107


 TIME FOR THE TIME STEP               78:        0.90474E+01

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


 INSTANT    0.395000000E-04   TIME STEP NUMBER              79
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.817487090E-23
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.608534913E-06
Free inlet               13         400         0.156900915E-03
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 0.18469E+01
   Friction velocity        uet   :  0.19106E-03 0.14153E+01
   Friction velocity        uk    :  0.19106E-03 0.19570E+01
   Dimensionless distance   yplus :  0.47250E-03 0.47284E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        804
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43723E-01       9   0.48552E-04   0.34797E+00 0.46636E+03 
c  Velocity[X]                                      0.31215E+00 
c  Velocity[Y]                                      0.35820E-01 
c  Velocity[Z]                                      0.74034E-08 
c  Pressure     0.11554E-06    2045   0.13322E-02   0.42438E+00 0.28241E+05 
c  k            0.29642E-02       5   0.43302E-08   0.23455E-02 0.26748E+04 
c  omega        0.10994E+06       4   0.96613E-08   0.13504E+13 0.11630E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.033599          15.369          2.1157         0.46997
v  Velocity[Y]          -0.097212          3.8646         0.20856        0.028513
v  Velocity[Z]         -0.0014777       0.0014158      6.3029e-08      9.2797e-10
v  ǁVelocityǁ          2.6067e-07          15.488          2.1398          0.4724
v  Pressure                -32417      1.2349e+05           29209          -10429
v  k                   6.8819e-11          3.2093        0.025175        0.023454
v  omega                   95.824      4.9325e+07       8.036e+05           63494
v  TurbVisc            1.3701e-15         0.24667           0.105         0.21652
v  CourantNb           1.0831e-08         0.34114        0.021272       0.0036041
v  FourierNb            0.0012525          1.4704         0.15233        0.041499
v  total_pressure           68908      2.2482e+05      1.3053e+05           90896


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012566          1.4714          0.1736        0.045103


 TIME FOR THE TIME STEP               79:        0.94775E+01

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


 INSTANT    0.400000000E-04   TIME STEP NUMBER              80
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.822010734E-23
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.615961941E-06
Free inlet               13         400         0.156893488E-03
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 0.18465E+01
   Friction velocity        uet   :  0.31717E-03 0.14156E+01
   Friction velocity        uk    :  0.31717E-03 0.19573E+01
   Dimensionless distance   yplus :  0.78438E-03 0.47293E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        805
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43724E-01       8   0.51204E-04   0.33439E+00 0.45716E+03 
c  Velocity[X]                                      0.29995E+00 
c  Velocity[Y]                                      0.34439E-01 
c  Velocity[Z]                                      0.87098E-08 
c  Pressure     0.35547E-07    1926   0.14883E-02   0.13283E+00 0.17356E+05 
c  k            0.29642E-02       5   0.45409E-08   0.11896E-01 0.60267E+04 
c  omega        0.10993E+06       5   0.14897E-07   0.32950E+16 0.57420E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.030609          15.278          2.1155         0.47013
v  Velocity[Y]          -0.097851          3.8193         0.20854        0.028503
v  Velocity[Z]         -0.0014735       0.0014141       6.265e-08      9.3443e-10
v  ǁVelocityǁ          9.0939e-08          15.417          2.1396         0.47256
v  Pressure                -31905      1.2349e+05           28924          -10631
v  k                   7.0596e-11          3.2057        0.025161        0.023453
v  omega                   95.898       6.776e+07      8.0406e+05           63459
v  TurbVisc            1.4061e-15         0.24455         0.10476         0.21647
v  CourantNb           1.0497e-08         0.34207        0.021271       0.0036043
v  FourierNb            0.0012525         0.94273         0.15136        0.041386
v  total_pressure           69420      2.2481e+05      1.3025e+05           90694


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012566         0.94372         0.17263         0.04499


 TIME FOR THE TIME STEP               80:        0.90780E+01

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


 INSTANT    0.405000000E-04   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.312260681E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.623183774E-06
Free inlet               13         400         0.156886266E-03
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 0.18462E+01
   Friction velocity        uet   :  0.74893E-04 0.14166E+01
   Friction velocity        uk    :  0.74893E-04 0.19581E+01
   Dimensionless distance   yplus :  0.18701E-03 0.47312E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        805
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43726E-01      10   0.54255E-04   0.34736E+00 0.46594E+03 
c  Velocity[X]                                      0.30291E+00 
c  Velocity[Y]                                      0.44448E-01 
c  Velocity[Z]                                      0.74803E-08 
c  Pressure     0.12469E-06    1932   0.13124E-02   0.45873E+00 0.23967E+05 
c  k            0.29641E-02       5   0.45573E-08   0.10585E+00 0.17987E+05 
c  omega        0.10995E+06       5   0.63809E-07   0.19053E+15 0.13809E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.028936          15.322          2.1154          0.4703
v  Velocity[Y]          -0.098481          3.8695         0.20852        0.028495
v  Velocity[Z]         -0.0014667       0.0014105      6.2265e-08      9.3848e-10
v  ǁVelocityǁ          1.6407e-07           15.44          2.1395         0.47273
v  Pressure                -31638      1.2386e+05           29430          -10249
v  k                   7.2386e-11          3.2009        0.025142        0.023452
v  omega                   95.978      5.2593e+07      8.0316e+05           63397
v  TurbVisc            1.4424e-15         0.24498         0.10496         0.21646
v  CourantNb           9.6328e-09         0.34039        0.021269       0.0036044
v  FourierNb            0.0012525          1.3505         0.15228        0.041433
v  total_pressure           69687      2.2518e+05      1.3075e+05           91076


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012567          1.3515         0.17355        0.045037


 TIME FOR THE TIME STEP               81:        0.90504E+01

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


 INSTANT    0.410000000E-04   TIME STEP NUMBER              82
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.120878229E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.630567479E-06
Free inlet               13         400         0.156878883E-03
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 0.18458E+01
   Friction velocity        uet   :  0.25035E-03 0.14166E+01
   Friction velocity        uk    :  0.25035E-03 0.19582E+01
   Dimensionless distance   yplus :  0.61854E-03 0.47314E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        804
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43727E-01       7   0.59496E-04   0.35431E+00 0.47058E+03 
c  Velocity[X]                                      0.29786E+00 
c  Velocity[Y]                                      0.56451E-01 
c  Velocity[Z]                                      0.68992E-08 
c  Pressure     0.47732E-07    1920   0.17981E-02   0.17401E+00 0.27729E+05 
c  k            0.29641E-02       5   0.37196E-08   0.40483E-02 0.35191E+04 
c  omega        0.10995E+06       5   0.98656E-08   0.37791E+15 0.19453E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.023653          15.358          2.1153         0.47046
v  Velocity[Y]          -0.099103          3.8923          0.2085        0.028483
v  Velocity[Z]         -0.0014591        0.001406      6.1921e-08       9.421e-10
v  ǁVelocityǁ          3.0895e-07          15.475          2.1394         0.47289
v  Pressure                -32449      1.2374e+05           29029          -10700
v  k                   7.4191e-11          3.1982        0.025129        0.023451
v  omega                   96.041      4.9328e+07      8.0216e+05           63328
v  TurbVisc             1.479e-15         0.24356         0.10455         0.21639
v  CourantNb             9.84e-09         0.34065        0.021267       0.0036046
v  FourierNb            0.0012525         0.94173         0.15061        0.041234
v  total_pressure           68876      2.2507e+05      1.3035e+05           90625


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012567         0.94274         0.17188        0.044838


 TIME FOR THE TIME STEP               82:        0.90062E+01

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


 INSTANT    0.415000000E-04   TIME STEP NUMBER              83
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.119068772E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.637801894E-06
Free inlet               13         400         0.156871648E-03
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 0.18454E+01
   Friction velocity        uet   :  0.34334E-03 0.14150E+01
   Friction velocity        uk    :  0.34334E-03 0.19572E+01
   Dimensionless distance   yplus :  0.84846E-03 0.47288E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        804
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43729E-01       9   0.59490E-04   0.37795E+00 0.48602E+03 
c  Velocity[X]                                      0.31633E+00 
c  Velocity[Y]                                      0.61615E-01 
c  Velocity[Z]                                      0.74590E-08 
c  Pressure     0.67583E-07    1962   0.13225E-02   0.25095E+00 0.17385E+05 
c  k            0.29641E-02       5   0.30470E-08   0.23476E-02 0.26810E+04 
c  omega        0.10993E+06       5   0.22086E-08   0.10362E+15 0.10187E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.021841          15.381          2.1152         0.47062
v  Velocity[Y]          -0.099716          3.8202         0.20848        0.028473
v  Velocity[Z]         -0.0014519       0.0014011      6.1563e-08      9.4542e-10
v  ǁVelocityǁ          1.3069e-07          15.525          2.1392         0.47305
v  Pressure                -31905      1.2376e+05           29141          -10441
v  k                   7.6009e-11          3.1958        0.025117         0.02345
v  omega                    96.12      4.9329e+07      8.0136e+05           63266
v  TurbVisc            1.5159e-15         0.24467         0.10477         0.21638
v  CourantNb           1.4441e-08         0.34204        0.021266       0.0036048
v  FourierNb            0.0012525          0.9412          0.1515        0.041281
v  total_pressure           69420      2.2509e+05      1.3047e+05           90884


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012568         0.94223         0.17276        0.044886


 TIME FOR THE TIME STEP               83:        0.91629E+01

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


 INSTANT    0.420000000E-04   TIME STEP NUMBER              84
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.425610275E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.645146872E-06
Free inlet               13         400         0.156864303E-03
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 0.18450E+01
   Friction velocity        uet   :  0.18078E-03 0.14036E+01
   Friction velocity        uk    :  0.18078E-03 0.19489E+01
   Dimensionless distance   yplus :  0.45142E-03 0.47089E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        804
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43730E-01       8   0.52100E-04   0.33100E+00 0.45483E+03 
c  Velocity[X]                                      0.28477E+00 
c  Velocity[Y]                                      0.46227E-01 
c  Velocity[Z]                                      0.57027E-08 
c  Pressure     0.11813E-06    2035   0.12099E-02   0.43153E+00 0.10870E+05 
c  k            0.29641E-02       5   0.54311E-08   0.27314E-02 0.28930E+04 
c  omega        0.10995E+06       4   0.66819E-07   0.32435E+14 0.56994E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.020974          15.327           2.115         0.47078
v  Velocity[Y]           -0.10031          3.8565         0.20846        0.028464
v  Velocity[Z]         -0.0014442       0.0013955      6.1136e-08      9.4533e-10
v  ǁVelocityǁ            3.09e-07          15.449          2.1391         0.47321
v  Pressure                -31639      1.2422e+05           29502          -10292
v  k                    7.784e-11          3.1888        0.025106        0.023449
v  omega                   96.188      4.9329e+07      8.0066e+05           63212
v  TurbVisc             1.553e-15         0.24447         0.10462         0.21634
v  CourantNb           9.2433e-09         0.34196        0.021265        0.003605
v  FourierNb            0.0012525         0.94067         0.15079        0.041178
v  total_pressure           69686      2.2554e+05      1.3083e+05           91033


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012568         0.94171         0.17205        0.044783


 TIME FOR THE TIME STEP               84:        0.93818E+01

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


 INSTANT    0.425000000E-04   TIME STEP NUMBER              85
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.109924549E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.652481621E-06
Free inlet               13         400         0.156856968E-03
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 0.18447E+01
   Friction velocity        uet   :  0.36281E-03 0.14076E+01
   Friction velocity        uk    :  0.36281E-03 0.19520E+01
   Dimensionless distance   yplus :  0.89666E-03 0.47164E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        805
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43732E-01       8   0.59208E-04   0.32404E+00 0.45001E+03 
c  Velocity[X]                                      0.27848E+00 
c  Velocity[Y]                                      0.45561E-01 
c  Velocity[Z]                                      0.42154E-08 
c  Pressure     0.72894E-07    1915   0.12135E-02   0.27311E+00 0.24655E+05 
c  k            0.29641E-02       5   0.47231E-08   0.32272E-02 0.31460E+04 
c  omega        0.10994E+06       5   0.10080E-07   0.10643E+16 0.32642E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.01411          15.358          2.1149         0.47094
v  Velocity[Y]           -0.10089          3.8039         0.20844        0.028452
v  Velocity[Z]         -0.0014377       0.0013899      6.0945e-08      9.5037e-10
v  ǁVelocityǁ          1.0461e-07          15.475           2.139         0.47337
v  Pressure                -32472      1.2378e+05           29051          -10707
v  k                   7.9685e-11           3.184        0.025094        0.023448
v  omega                   96.254      4.9838e+07      8.0073e+05           63171
v  TurbVisc            1.5905e-15         0.24354         0.10444         0.21629
v  CourantNb           1.2665e-08         0.34258        0.021263       0.0036052
v  FourierNb            0.0012525         0.94013         0.15021        0.041084
v  total_pressure           68853      2.2511e+05      1.3038e+05           90618


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012569         0.94118         0.17147        0.044689


 TIME FOR THE TIME STEP               85:        0.89816E+01

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


 INSTANT    0.430000000E-04   TIME STEP NUMBER              86
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.543321953E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.659711458E-06
Free inlet               13         400         0.156849739E-03
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 0.18445E+01
   Friction velocity        uet   :  0.19464E-03 0.14098E+01
   Friction velocity        uk    :  0.19464E-03 0.19537E+01
   Dimensionless distance   yplus :  0.48099E-03 0.47204E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        805
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43733E-01      10   0.56331E-04   0.33945E+00 0.46059E+03 
c  Velocity[X]                                      0.29133E+00 
c  Velocity[Y]                                      0.48120E-01 
c  Velocity[Z]                                      0.39137E-08 
c  Pressure     0.79943E-07    1977   0.10733E-02   0.29516E+00 0.19253E+05 
c  k            0.29640E-02       5   0.41664E-08   0.38695E-02 0.34463E+04 
c  omega        0.10993E+06       4   0.24093E-08   0.63776E+13 0.25270E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.013923          15.342          2.1148          0.4711
v  Velocity[Y]           -0.10146          3.8289         0.20843        0.028442
v  Velocity[Z]         -0.0014325       0.0013861      6.1039e-08      9.6121e-10
v  ǁVelocityǁ          1.4719e-07          15.485          2.1388         0.47354
v  Pressure                -31910      1.2391e+05           29236          -10410
v  k                   8.1542e-11          3.1794        0.025081        0.023447
v  omega                   96.333      4.9331e+07      8.0013e+05           63117
v  TurbVisc            1.6281e-15         0.24483         0.10474          0.2163
v  CourantNb           1.1923e-08         0.34218        0.021262       0.0036053
v  FourierNb            0.0012525          1.3923         0.15141        0.041167
v  total_pressure           69415      2.2523e+05      1.3056e+05           90915


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012569          1.3934         0.17267        0.044772


 TIME FOR THE TIME STEP               86:        0.92341E+01

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


 INSTANT    0.435000000E-04   TIME STEP NUMBER              87
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.442993992E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.667066194E-06
Free inlet               13         400         0.156842384E-03
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 0.18443E+01
   Friction velocity        uet   :  0.22558E-03 0.14099E+01
   Friction velocity        uk    :  0.22558E-03 0.19539E+01
   Dimensionless distance   yplus :  0.56326E-03 0.47209E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        806
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43735E-01       8   0.50374E-04   0.33892E+00 0.46022E+03 
c  Velocity[X]                                      0.29155E+00 
c  Velocity[Y]                                      0.47364E-01 
c  Velocity[Z]                                      0.41405E-08 
c  Pressure     0.72947E-07    1868   0.10217E-02   0.26445E+00 0.18924E+05 
c  k            0.29640E-02       5   0.32108E-07   0.89443E-02 0.52418E+04 
c  omega        0.10995E+06       5   0.51582E-06   0.24411E+16 0.49418E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0094162          15.314          2.1147         0.47126
v  Velocity[Y]           -0.10203          3.8432         0.20841        0.028433
v  Velocity[Z]          -0.001429       0.0013856      6.1751e-08      9.8496e-10
v  ǁVelocityǁ           1.922e-07          15.431          2.1387          0.4737
v  Pressure                -31645      1.2372e+05           28890          -10642
v  k                   8.3412e-11          3.1766        0.025068        0.023446
v  omega                   96.402      6.9887e+07      8.0075e+05           63088
v  TurbVisc            1.6661e-15         0.24355         0.10444         0.21624
v  CourantNb           9.4645e-09           0.342        0.021261       0.0036055
v  FourierNb            0.0012525         0.93776         0.15008        0.041008
v  total_pressure           69680      2.2504e+05      1.3021e+05           90683


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001257         0.93884         0.17134        0.044613


 TIME FOR THE TIME STEP               87:        0.89610E+01

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


 INSTANT    0.440000000E-04   TIME STEP NUMBER              88
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.156860586E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.674201381E-06
Free inlet               13         400         0.156835249E-03
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 0.18441E+01
   Friction velocity        uet   :  0.31687E-03 0.13989E+01
   Friction velocity        uk    :  0.31687E-03 0.19459E+01
   Dimensionless distance   yplus :  0.78311E-03 0.47016E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        807
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43736E-01       8   0.53788E-04   0.31598E+00 0.44437E+03 
c  Velocity[X]                                      0.27544E+00 
c  Velocity[Y]                                      0.40533E-01 
c  Velocity[Z]                                      0.38568E-08 
c  Pressure     0.67480E-07    1913   0.87542E-03   0.24483E+00 0.11357E+05 
c  k            0.29640E-02       5   0.77585E-07   0.52707E-01 0.12730E+05 
c  omega        0.10995E+06       5   0.12028E-06   0.35144E+16 0.59278E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0086398          15.356          2.1145         0.47142
v  Velocity[Y]           -0.10259          3.8544         0.20839        0.028421
v  Velocity[Z]         -0.0014276       0.0013862      6.2518e-08      1.0093e-09
v  ǁVelocityǁ          1.8113e-07          15.473          2.1386         0.47386
v  Pressure                -32495      1.2327e+05           28631          -10773
v  k                   8.5294e-11          3.1715        0.025049        0.023445
v  omega                   96.491      6.7793e+07       8.011e+05           63059
v  TurbVisc            1.7043e-15         0.24541         0.10472         0.21624
v  CourantNb           1.0527e-08         0.34223        0.021259       0.0036057
v  FourierNb            0.0012525          1.4362         0.15124        0.041078
v  total_pressure           68830       2.246e+05      1.2996e+05           90552


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.001257          1.4373          0.1725        0.044684


 TIME FOR THE TIME STEP               88:        0.89866E+01

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


 INSTANT    0.445000000E-04   TIME STEP NUMBER              89
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.149344875E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.681431324E-06
Free inlet               13         400         0.156828019E-03
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 0.18439E+01
   Friction velocity        uet   :  0.29574E-03 0.14025E+01
   Friction velocity        uk    :  0.29574E-03 0.19487E+01
   Dimensionless distance   yplus :  0.73090E-03 0.47083E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        806
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43737E-01       9   0.54426E-04   0.33959E+00 0.46067E+03 
c  Velocity[X]                                      0.29756E+00 
c  Velocity[Y]                                      0.42025E-01 
c  Velocity[Z]                                      0.37079E-08 
c  Pressure     0.98278E-07    1871   0.71140E-03   0.35812E+00 0.99135E+04 
c  k            0.29640E-02       5   0.11395E-07   0.10840E+00 0.18265E+05 
c  omega        0.10994E+06       5   0.17769E-06   0.49256E+15 0.22200E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.012588          15.384          2.1144         0.47158
v  Velocity[Y]           -0.10314          3.8605         0.20837         0.02841
v  Velocity[Z]         -0.0014285       0.0013885      6.3131e-08      1.0297e-09
v  ǁVelocityǁ           8.846e-08          15.501          2.1384         0.47402
v  Pressure                -31924      1.2274e+05           28306          -10857
v  k                   8.7187e-11          3.1667        0.025031        0.023444
v  omega                    96.59      5.2607e+07      7.9997e+05           62998
v  TurbVisc            1.7427e-15         0.24558         0.10458          0.2162
v  CourantNb           9.9037e-09         0.34206        0.021258       0.0036059
v  FourierNb            0.0012525          1.3822         0.15055        0.040973
v  total_pressure           69401      2.2407e+05      1.2963e+05           90468


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012571           1.383          0.1718        0.044579


 TIME FOR THE TIME STEP               89:        0.89095E+01

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


 INSTANT    0.450000000E-04   TIME STEP NUMBER              90
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.919301391E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.688554189E-06
Free inlet               13         400         0.156820896E-03
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 0.18437E+01
   Friction velocity        uet   :  0.15979E-03 0.14030E+01
   Friction velocity        uk    :  0.15979E-03 0.19491E+01
   Dimensionless distance   yplus :  0.39900E-03 0.47095E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        805
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43739E-01       8   0.47549E-04   0.33619E+00 0.45836E+03 
c  Velocity[X]                                      0.29266E+00 
c  Velocity[Y]                                      0.43528E-01 
c  Velocity[Z]                                      0.35903E-08 
c  Pressure     0.34916E-07    1951   0.19907E-02   0.13112E+00 0.17930E+05 
c  k            0.29639E-02       5   0.10378E-07   0.41841E-02 0.35899E+04 
c  omega        0.10995E+06       5   0.11719E-06   0.46814E+15 0.21646E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.01544          15.385          2.1143         0.47174
v  Velocity[Y]           -0.10368           3.786         0.20835        0.028402
v  Velocity[Z]          -0.001429        0.001391      6.3649e-08      1.0479e-09
v  ǁVelocityǁ          2.9371e-07          15.529          2.1383         0.47418
v  Pressure                -31642      1.2283e+05           28702          -10581
v  k                   8.9093e-11          3.1626        0.025018        0.023443
v  omega                   96.693      4.9334e+07      7.9889e+05           62942
v  TurbVisc            1.7814e-15         0.24436         0.10436         0.21615
v  CourantNb           9.2479e-09         0.34292        0.021257       0.0036061
v  FourierNb            0.0012525         0.93757         0.14963        0.040853
v  total_pressure           69683      2.2415e+05      1.3003e+05           90744


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012571         0.93836         0.17089        0.044459


 TIME FOR THE TIME STEP               90:        0.91617E+01

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


 INSTANT    0.455000000E-04   TIME STEP NUMBER              91
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.120836224E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.695769530E-06
Free inlet               13         400         0.156813680E-03
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 0.18435E+01
   Friction velocity        uet   :  0.21624E-03 0.14042E+01
   Friction velocity        uk    :  0.21624E-03 0.19501E+01
   Dimensionless distance   yplus :  0.53427E-03 0.47119E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        806
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43740E-01       9   0.44362E-04   0.32001E+00 0.44720E+03 
c  Velocity[X]                                      0.28000E+00 
c  Velocity[Y]                                      0.40011E-01 
c  Velocity[Z]                                      0.35169E-08 
c  Pressure     0.82073E-07    1828   0.91510E-03   0.30180E+00 0.13381E+05 
c  k            0.29639E-02       5   0.12169E-07   0.30169E-02 0.30495E+04 
c  omega        0.10995E+06       5   0.22604E-06   0.59490E+15 0.24401E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.017839          15.286          2.1142          0.4719
v  Velocity[Y]           -0.10422           3.823         0.20833        0.028388
v  Velocity[Z]         -0.0014312       0.0013945      6.4357e-08      1.0692e-09
v  ǁVelocityǁ          1.5309e-07           15.43          2.1382         0.47434
v  Pressure                -32516      1.2347e+05           29062          -10539
v  k                   9.1009e-11          3.1586        0.025007        0.023443
v  omega                   96.775      4.9449e+07      7.9872e+05           62897
v  TurbVisc            1.8204e-15         0.24465         0.10437         0.21612
v  CourantNb           9.5808e-09         0.34166        0.021256       0.0036063
v  FourierNb            0.0012525          1.0789         0.14996        0.040855
v  total_pressure           68809       2.248e+05      1.3039e+05           90786


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012572          1.0797         0.17121        0.044462


 TIME FOR THE TIME STEP               91:        0.87269E+01

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


 INSTANT    0.460000000E-04   TIME STEP NUMBER              92
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.128665359E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.703137670E-06
Free inlet               13         400         0.156806312E-03
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 0.18432E+01
   Friction velocity        uet   :  0.29400E-03 0.13944E+01
   Friction velocity        uk    :  0.29400E-03 0.19430E+01
   Dimensionless distance   yplus :  0.72640E-03 0.46947E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        806
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43742E-01       8   0.48628E-04   0.29506E+00 0.42940E+03 
c  Velocity[X]                                      0.25165E+00 
c  Velocity[Y]                                      0.43411E-01 
c  Velocity[Z]                                      0.36364E-08 
c  Pressure     0.72298E-07    1896   0.98266E-03   0.27286E+00 0.16361E+05 
c  k            0.29639E-02       5   0.96467E-08   0.29542E-02 0.30188E+04 
c  omega        0.10993E+06       4   0.53330E-08   0.31860E+14 0.56472E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015639          15.213          2.1141         0.47206
v  Velocity[Y]           -0.10475          3.7698         0.20831        0.028377
v  Velocity[Z]         -0.0014287        0.001396      6.5313e-08      1.0956e-09
v  ǁVelocityǁ          1.9864e-07          15.356          2.1381          0.4745
v  Pressure                -31929      1.2327e+05           28696          -10738
v  k                   9.2936e-11          3.1538        0.024995        0.023442
v  omega                   96.825      4.9336e+07      7.9812e+05           62848
v  TurbVisc            1.8595e-15         0.24432         0.10438          0.2161
v  CourantNb           8.3501e-09         0.33989        0.021255       0.0036065
v  FourierNb            0.0012525         0.94033         0.14994        0.040828
v  total_pressure           69396       2.246e+05      1.3002e+05           90587


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012572         0.94115         0.17119        0.044435


 TIME FOR THE TIME STEP               92:        0.88818E+01

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


 INSTANT    0.465000000E-04   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.347706663E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.710312618E-06
Free inlet               13         400         0.156799137E-03
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 0.18430E+01
   Friction velocity        uet   :  0.28452E-03 0.13989E+01
   Friction velocity        uk    :  0.28452E-03 0.19465E+01
   Dimensionless distance   yplus :  0.70297E-03 0.47030E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        806
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43743E-01       9   0.44346E-04   0.28869E+00 0.42474E+03 
c  Velocity[X]                                      0.24788E+00 
c  Velocity[Y]                                      0.40813E-01 
c  Velocity[Z]                                      0.36103E-08 
c  Pressure     0.42447E-07    1766   0.10521E-02   0.15805E+00 0.16568E+05 
c  k            0.29639E-02       5   0.66363E-08   0.27601E-02 0.29190E+04 
c  omega        0.10995E+06       4   0.75997E-07   0.12263E+14 0.35034E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.016439          15.192           2.114         0.47222
v  Velocity[Y]           -0.10527          3.8087         0.20829        0.028369
v  Velocity[Z]         -0.0014238       0.0013959      6.6242e-08      1.1208e-09
v  ǁVelocityǁ          7.9049e-08          15.309           2.138         0.47466
v  Pressure                -31639      1.2322e+05           28846          -10482
v  k                   9.4874e-11          3.1479        0.024985        0.023441
v  omega                   96.901      4.9337e+07      7.9759e+05           62806
v  TurbVisc            1.8989e-15         0.24532         0.10433         0.21606
v  CourantNb           8.2515e-09         0.33849        0.021253       0.0036066
v  FourierNb            0.0012525          1.4646         0.14988        0.040778
v  total_pressure           69686      2.2455e+05      1.3017e+05           90843


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012573          1.4657         0.17113        0.044385


 TIME FOR THE TIME STEP               93:        0.85138E+01

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


 INSTANT    0.470000000E-04   TIME STEP NUMBER              94
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.667754474E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.717579443E-06
Free inlet               13         400         0.156791871E-03
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 0.18428E+01
   Friction velocity        uet   :  0.15579E-03 0.14004E+01
   Friction velocity        uk    :  0.15579E-03 0.19477E+01
   Dimensionless distance   yplus :  0.38898E-03 0.47059E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        807
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43745E-01       8   0.42014E-04   0.27707E+00 0.41610E+03 
c  Velocity[X]                                      0.23661E+00 
c  Velocity[Y]                                      0.40462E-01 
c  Velocity[Z]                                      0.33431E-08 
c  Pressure     0.36818E-07    1739   0.85908E-03   0.13588E+00 0.17402E+05 
c  k            0.29639E-02       5   0.53581E-08   0.31770E-02 0.31329E+04 
c  omega        0.10995E+06       5   0.10871E-07   0.15686E+16 0.39614E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.016254          15.241          2.1138         0.47238
v  Velocity[Y]           -0.10579          3.8401         0.20827        0.028356
v  Velocity[Z]         -0.0014178        0.001395       6.711e-08      1.1445e-09
v  ǁVelocityǁ          2.1328e-07           15.36          2.1378         0.47482
v  Pressure                -32543      1.2308e+05           28684          -10769
v  k                   9.6823e-11          3.1439        0.024973         0.02344
v  omega                   96.956      5.3525e+07       7.979e+05           62779
v  TurbVisc            1.9385e-15         0.24448         0.10431         0.21603
v  CourantNb           7.6714e-09         0.33872        0.021252       0.0036068
v  FourierNb            0.0012525          1.3776         0.14989        0.040757
v  total_pressure           68782      2.2441e+05      1.3001e+05           90556


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012573          1.3788         0.17114        0.044364


 TIME FOR THE TIME STEP               94:        0.84011E+01

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


 INSTANT    0.475000000E-04   TIME STEP NUMBER              95
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.630305164E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.724817859E-06
Free inlet               13         400         0.156784632E-03
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 0.18426E+01
   Friction velocity        uet   :  0.28567E-03 0.14002E+01
   Friction velocity        uk    :  0.28567E-03 0.19476E+01
   Dimensionless distance   yplus :  0.70595E-03 0.47058E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        807
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43746E-01       9   0.46552E-04   0.26700E+00 0.40847E+03 
c  Velocity[X]                                      0.23070E+00 
c  Velocity[Y]                                      0.36300E-01 
c  Velocity[Z]                                      0.29071E-08 
c  Pressure     0.28545E-07    1707   0.67799E-03   0.10510E+00 0.11181E+05 
c  k            0.29638E-02       5   0.47580E-08   0.57749E-02 0.42254E+04 
c  omega        0.10993E+06       4   0.27135E-08   0.24760E+14 0.49773E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.01658          15.282          2.1137         0.47254
v  Velocity[Y]            -0.1063          3.8633         0.20825        0.028344
v  Velocity[Z]         -0.0014136       0.0013949      6.8122e-08      1.1713e-09
v  ǁVelocityǁ          1.6149e-07          15.402          2.1377         0.47498
v  Pressure                -31930      1.2312e+05           28797          -10590
v  k                   9.8782e-11          3.1404        0.024962        0.023439
v  omega                   97.029      4.9339e+07      7.9737e+05           62734
v  TurbVisc            1.9783e-15         0.24513         0.10422           0.216
v  CourantNb           7.5943e-09         0.33891        0.021251        0.003607
v  FourierNb            0.0012525          1.4637         0.14965        0.040692
v  total_pressure           69395      2.2445e+05      1.3012e+05           90735


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012574           1.465          0.1709        0.044299


 TIME FOR THE TIME STEP               95:        0.84183E+01

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


 INSTANT    0.480000000E-04   TIME STEP NUMBER              96
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.127308266E-23
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.732097849E-06
Free inlet               13         400         0.156777352E-03
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 0.18424E+01
   Friction velocity        uet   :  0.25950E-03 0.13993E+01
   Friction velocity        uk    :  0.25950E-03 0.19470E+01
   Dimensionless distance   yplus :  0.64149E-03 0.47043E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        807
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43747E-01       9   0.45766E-04   0.28783E+00 0.42410E+03 
c  Velocity[X]                                      0.26022E+00 
c  Velocity[Y]                                      0.27613E-01 
c  Velocity[Z]                                      0.24249E-08 
c  Pressure     0.38079E-07    1824   0.59841E-03   0.14076E+00 0.63319E+04 
c  k            0.29638E-02       5   0.42325E-08   0.18649E-02 0.24020E+04 
c  omega        0.10995E+06       4   0.79102E-07   0.36531E+13 0.19118E+04 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.016461          15.313          2.1136          0.4727
v  Velocity[Y]            -0.1068          3.8575         0.20823        0.028335
v  Velocity[Z]          -0.001413       0.0013971      6.9324e-08       1.202e-09
v  ǁVelocityǁ          7.1476e-08          15.431          2.1376         0.47515
v  Pressure                -31639      1.2323e+05           28903          -10496
v  k                   1.0075e-10          3.1359        0.024951        0.023438
v  omega                   97.087       4.934e+07      7.9691e+05           62695
v  TurbVisc            2.0183e-15          0.2445         0.10416         0.21596
v  CourantNb           7.1805e-09         0.33915         0.02125       0.0036072
v  FourierNb            0.0012525          1.4038          0.1495        0.040654
v  total_pressure           69686      2.2455e+05      1.3023e+05           90829


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012574          1.4051         0.17075        0.044261


 TIME FOR THE TIME STEP               96:        0.87752E+01

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


 INSTANT    0.485000000E-04   TIME STEP NUMBER              97
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.311969876E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.739345156E-06
Free inlet               13         400         0.156770105E-03
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 0.18421E+01
   Friction velocity        uet   :  0.17519E-03 0.13973E+01
   Friction velocity        uk    :  0.17519E-03 0.19457E+01
   Dimensionless distance   yplus :  0.43308E-03 0.47012E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        808
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43749E-01       9   0.53863E-04   0.32019E+00 0.44731E+03 
c  Velocity[X]                                      0.28215E+00 
c  Velocity[Y]                                      0.38042E-01 
c  Velocity[Z]                                      0.31959E-08 
c  Pressure     0.88343E-07    1973   0.10568E-02   0.33287E+00 0.11037E+05 
c  k            0.29638E-02       5   0.37990E-08   0.11566E-01 0.59841E+04 
c  omega        0.10995E+06       5   0.11003E-07   0.34695E+16 0.58891E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015612          15.312          2.1135         0.47287
v  Velocity[Y]           -0.10729          3.7889          0.2082        0.028321
v  Velocity[Z]         -0.0014149       0.0014009      7.0517e-08      1.2336e-09
v  ǁVelocityǁ          4.7086e-08          15.457          2.1375         0.47531
v  Pressure                -32562      1.2352e+05           29145          -10505
v  k                   1.0273e-10          3.1319        0.024939        0.023437
v  omega                   97.143      6.7833e+07      7.9762e+05           62680
v  TurbVisc            2.0585e-15         0.24431         0.10408         0.21593
v  CourantNb           6.9647e-09         0.33991        0.021249       0.0036074
v  FourierNb            0.0012525          1.2666          0.1492        0.040597
v  total_pressure           68763      2.2485e+05      1.3047e+05           90820


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012575          1.2677         0.17045        0.044204


 TIME FOR THE TIME STEP               97:        0.92161E+01

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


 INSTANT    0.490000000E-04   TIME STEP NUMBER              98
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140        -0.654959024E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.746734742E-06
Free inlet               13         400         0.156762715E-03
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 0.18419E+01
   Friction velocity        uet   :  0.12673E-03 0.13860E+01
   Friction velocity        uk    :  0.12673E-03 0.19375E+01
   Dimensionless distance   yplus :  0.31319E-03 0.46813E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        808
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43750E-01       9   0.53391E-04   0.29175E+00 0.42697E+03 
c  Velocity[X]                                      0.24994E+00 
c  Velocity[Y]                                      0.41805E-01 
c  Velocity[Z]                                      0.20653E-08 
c  Pressure     0.21071E-06    2148   0.14571E-02   0.78182E+00 0.24048E+05 
c  k            0.29638E-02       5   0.63588E-08   0.10975E+00 0.18442E+05 
c  omega        0.10994E+06       5   0.14293E-07   0.20136E+15 0.14191E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.015566          15.236          2.1134         0.47303
v  Velocity[Y]           -0.10778          3.8195         0.20818        0.028309
v  Velocity[Z]         -0.0014145       0.0014034      7.1752e-08      1.2661e-09
v  ǁVelocityǁ          7.6999e-08          15.381          2.1374         0.47548
v  Pressure                -31931      1.2441e+05           29834          -10134
v  k                   1.0472e-10          3.1239        0.024922        0.023436
v  omega                   97.187      5.2626e+07      7.9691e+05           62634
v  TurbVisc             2.099e-15         0.24361         0.10372         0.21587
v  CourantNb           7.0086e-09         0.33967        0.021248       0.0036076
v  FourierNb            0.0012525         0.92263         0.14774        0.040427
v  total_pressure           69394      2.2573e+05      1.3116e+05           91191


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012575         0.92383         0.16899        0.044035


 TIME FOR THE TIME STEP               98:        0.98127E+01

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


 INSTANT    0.495000000E-04   TIME STEP NUMBER              99
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.667883721E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.754236064E-06
Free inlet               13         400         0.156755214E-03
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 0.18417E+01
   Friction velocity        uet   :  0.16633E-03 0.13912E+01
   Friction velocity        uk    :  0.16633E-03 0.19415E+01
   Dimensionless distance   yplus :  0.41104E-03 0.46911E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        807
   Total number of wall faces                   :       1140
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43752E-01       7   0.53398E-04   0.27142E+00 0.41183E+03 
c  Velocity[X]                                      0.23257E+00 
c  Velocity[Y]                                      0.38843E-01 
c  Velocity[Z]                                      0.16300E-08 
c  Pressure     0.38983E-07    1898   0.25301E-02   0.14381E+00 0.26207E+05 
c  k            0.29638E-02       5   0.40127E-08   0.33604E-02 0.32280E+04 
c  omega        0.10995E+06       5   0.82427E-07   0.39819E+15 0.19958E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.010445          15.233          2.1133         0.47319
v  Velocity[Y]           -0.10826          3.8432         0.20816        0.028299
v  Velocity[Z]         -0.0014209       0.0014042      7.2767e-08      1.2927e-09
v  ǁVelocityǁ          8.0504e-08          15.351          2.1373         0.47564
v  Pressure                -31640      1.2429e+05           29417          -10463
v  k                   1.0671e-10          3.1192        0.024912        0.023436
v  omega                   97.204      4.9342e+07      7.9612e+05           62589
v  TurbVisc            2.1396e-15          0.2436         0.10323         0.21578
v  CourantNb           6.9366e-09          0.3392        0.021247       0.0036078
v  FourierNb            0.0012525         0.92306          0.1464        0.040263
v  total_pressure           69685      2.2561e+05      1.3074e+05           90862


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012576         0.92428         0.16764        0.043871


 TIME FOR THE TIME STEP               99:        0.89438E+01

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


 INSTANT    0.500000000E-04   TIME STEP NUMBER             100
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.157509450E-03
Smooth wall               5        1140         0.379372171E-22
Rough wall                6           0         0.000000000E+00
Symmetry                  4      114000         0.000000000E+00
Free outlet               3         100         0.761441570E-06
Free inlet               13         400         0.156748009E-03
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 0.18414E+01
   Friction velocity        uet   :  0.27914E-03 0.13934E+01
   Friction velocity        uk    :  0.27914E-03 0.19433E+01
   Dimensionless distance   yplus :  0.68981E-03 0.46952E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        807
   Total number of wall faces                   :       1140
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        100


 Write final restart files
   checkpoint at iteration        100, Physical time    0.50000E-04


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

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Variables principales écrites dans le fichier de reprise : 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                            
  Coefficients de C.L. écrits dans le fichier de reprise : checkpoint/auxiliary
   End writing the wall distance                        
 End writing


 Time for restart files:    0.33844E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.43753E-01       8   0.52878E-04   0.28464E+00 0.42174E+03 
c  Velocity[X]                                      0.24086E+00 
c  Velocity[Y]                                      0.43779E-01 
c  Velocity[Z]                                      0.18749E-08 
c  Pressure     0.71267E-07    1819   0.12009E-02   0.26280E+00 0.11731E+05 
c  k            0.29637E-02       5   0.25869E-08   0.16384E-02 0.22547E+04 
c  omega        0.10995E+06       4   0.11273E-07   0.10991E+15 0.10487E+05 
-----------------------------------------------------------------------------
  
  

  ** "Clippings" des champs calculés
     -------------------------------

   champ      min. init.      max. init.   lim. à min.   lim. à max.
-  -----  --------------  --------------  ------------  ------------
a  k    
a  omega


  ** Champs calculés sur cellules
     ----------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0090066          15.276          2.1132         0.47335
v  Velocity[Y]           -0.10872           3.845         0.20814        0.028285
v  Velocity[Z]         -0.0014278       0.0014043      7.3522e-08       1.313e-09
v  ǁVelocityǁ          7.3914e-08          15.394          2.1372          0.4758
v  Pressure                -32585      1.2419e+05           29423          -10466
v  k                   1.0872e-10          3.1169        0.024902        0.023435
v  omega                   97.236      4.9343e+07      7.9552e+05           62544
v  TurbVisc            2.1804e-15         0.24419         0.10356          0.2158
v  CourantNb           9.3242e-09          0.3398        0.021246        0.003608
v  FourierNb            0.0012525         0.93043         0.14735        0.040333
v  total_pressure           68740      2.2551e+05      1.3075e+05           90859


  ** Valeurs calculées sur cellules
     ------------------------------

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0012576         0.93166         0.16859        0.043941


 TIME FOR THE TIME STEP              100:        0.90222E+01

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.90512E-03
      -----------------------                                



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




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


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

 Destruction des structures et clôture du calcul


Bilan des temps de calcul :

  Temps CPU utilisateur :      947.216 s
  Temps CPU système :            9.988 s

  Temps écoulé :               958.714 s
  Temps CPU / écoulé             0.998

Bilan de l'occupation mémoire :

  Consommation mémoire totale mesurée :           204.750 Mio
  Mémoire dynamique instrumentée théorique :      109.253 Mio
