commande : 
 ./cs_solver --mpi

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

                                  (R)
                      Code_Saturne

                      Version 6.1-alpha


  Copyright (C) 1998-2019 EDF S.A., France

  révision b610615
  build lun. 22 juil. 2019 09:56:22 CEST
  Version MPI 3.1 (MPICH 3.2)


  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. 29 juil. 2019 21:37:14 CEST
  Processeur :         model name	: Intel(R) Xeon(R) Gold 6140 CPU @ 2.30GHz
  Mémoire :            190315 Mo
  Utilisateur :        aria (Claude Derognat)
  Répertoire :         /tmpdir/aria/THESE_MO/MIGRATION_V6/RANS_D1/RESU/testsc1
  Rangs MPI :          18 (attribut appnum : 0)
  méthode de lecture : MPI-IO collectif (positions explicites)
  méthode d'écriture : MPI-IO collectif (positions explicites)
   pas des rangs E/S :  1

 Lecture des méta-données du fichier: "mesh_input"

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

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


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




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


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

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

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


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

 --- Physics
       NVAR   =              7 (Nb variables                )
       NSCAL  =              1 (Nb scalars                  )
       NSCAUS =              1 (Nb user scalars             )
       NSCAPP =              0 (Nb specific physics scalars )


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


 ** HOMOGENEOUS MIXTURE MODEL VoF           
    ----------------------------------------

       IVOFMT =              0 ( 0  : disabled              )
                               ( >=0: enabled               )


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


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

 --- Per-variable properties

------------------------------------
 Variable          ISTAT      CDTVAR
------------------------------------
 Velocity              1  0.1000E+01
 Pressure              0  0.1000E+01
 k                     1  0.1000E+01
 epsilon               1  0.1000E+01
 scalar1               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      )
                                                             

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


 ** STOKES
    ------

  -- Continuous phase:

       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         )
       THETVI =    0.00000E+00 (theta for total viscosity
                               ((1+theta).new-theta.old
       THETCP =   -0.99900E+03 (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                   )


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


 ** SCALARS
    -------

       ITBRRB =              0 (T or H reconstruction at bdy)

-------------------------------------------------------------
 Variable         Number ISCACP  ITURT     VISLS0      SIGMAS
-------------------------------------------------------------
 scalar1               1      0      0  0.2196E-04  0.7000E+00
-------------------------------------------------------------

------------------------------------
 Variable         Number      RVARFL
------------------------------------
 scalar1               1  0.8000E+00
-------------------------------------------

-------------------------------------------------------
 Variable         Number ICLVFL      SCAMIN      SCAMAX
-------------------------------------------------------
 scalar1               1     -1 -0.1000E+13  0.1000E+13
-------------------------------------------------------

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

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

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

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

       THETSS =                (theta for source terms      )
                               ((1+theta).new-theta.old     )
       THETVS =                (theta for scalar diffusivity
                               ((1+theta).new-theta.old     )


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


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

 --- Restarted calculation
       ISUITE =              0 (1: restarted calculation    )
       ILEAUX =              0 (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.

       NTPABS =              0 (Initial time step)
       NTMABS =             10 (Final time step required)


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


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

 --- Restart file
       NTSUIT =             -1 (Checkpoint frequency )

 --- Probe history files
       NTHIST =              1 (Output frequency     )
       FRHIST =     -.10000E+01 (Output frequency (s) )
         --           --                --

 --- run_solver.log files
       NTLIST =              1 (Output frequency     )

         --           --                --

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


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


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

       IALE   =              0 (1: activated,2: CDO         )
       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: separate_meshes
      dépendence en temps: maillage fixe
      sorties: tous les 1 pas de temps et à la fin du calcul

  -5: nom: 
      répertoire: monitoring
      format: time_plot
      options: 
      dépendence en temps: maillage fixe
      sorties: tous les 1 pas de temps

  -6: nom: 
      répertoire: profiles
      format: plot
      options: 
      dépendence en temps: maillage fixe
      sorties: à la fin du calcul

  -7: nom: histograms
      répertoire: histograms
      format: histogram
      options: txt
      dépendence en temps: maillage fixe
      sorties: à la fin du calcul


 Lecture du fichier :  mesh_input
 Fin de la lecture :  mesh_input
 Pas de fichier "partition_input/domain_number_18" disponible;

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

 Partitionnement par courbe fractale : Morton (dans boîte englobante).
  Nombre de cellules par domaine (histogramme) :
    [     137777 ;     137778 ] =         18

 Partitionnement terminé (7.56 s)


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

  Type de périodicité : translation
  Matrice de transformation :             1            0            0          120
                                          0            1            0            0
                                          0            0            1            0

  Critère de sélection : "east,west"

  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 :       2480000
     Nombre de faces internes : 7373200
     Nombre de faces de bord :  133600
     Nombre de sommets :        2547261

   Nombre global de faces frontières sélectionnées pour le recollement :      40000

  Sélection d'éléments effectuée.
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

        345 |    0.100000 |  0.0000000000e+00   1.7000000000e+02   0.0000000000e+00 | ORI
      31897 |    0.100000 |  0.0000000000e+00   0.0000000000e+00   6.5000000000e+01 | ORI
  Détermination des intersections possibles entre faces :

    répartition de l'arbre de boîtes englobantes : 3D

  Nombre global d'intersections détectées :        657809
    Intersections sommet-sommet :           657809
    Autres intersections :                       0

  L'opération de recollement est conforme.

  Intersections d'arêtes et création de sommets terminées.

  Pré-fusion pour 46986 couples globaux d'éléments.

  Pas besoin de fusionner des sommets.

  Edge removed for 0 faces (global).
  Join mesh cleaning done.

  Edge removed for 0 faces (global).
  Join mesh cleaning done.

  Fusion de sommets et mise à jour du maillage terminées.

  Nombre global de faces après subdivision :      60000

  Global configuration after the joining operation:
     Global number of border faces to add:          0

  Nettoyage du maillage pour des faces dégénérées.
    Nombre global de faces intérieures nettoyées :        0
    Nombre global de faces de bord nettoyées :            0

  Après recollement
     Nombre de cellules :       2480000
     Nombre de faces internes : 7413200
     Nombre de faces de bord :  93600
     Nombre de sommets :        2547261


  Recollement  1 terminé (0.62 s).

  Fin des étapes de recollement :

    Temps écoulé :                   0.621


 ----------------------------------------------------------
 Composition des périodicités

 Construction du halo avec voisinage étendu
 ==========================================

 Création de l'interface entre faces
 Définition des sommets périodiques
 Création de l'interface entre sommets
 Création des halos
 Définition des halos
    Définition du halo local
    Création du halo distant
    Mise à jour de la connectivité faces -> cellules
 Définition des structures pour le voisinage étendu

 Histogramme de la distribution du nombre de cellules sur les rangs :

    valeur minimale =           137777
    valeur maximale =           137778

      1 : [     137777 ;     137778 ] =         18

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

 Histogramme de la distribution du nombre de cellules
 standard + halo sur les rangs :

    valeur minimale =           152846
    valeur maximale =           159049

      1 : [     152846 ;     154086 [ =          4
      2 : [     154086 ;     155327 [ =          1
      3 : [     155327 ;     156567 [ =          1
      4 : [     156567 ;     157808 [ =          8
      5 : [     157808 ;     159049 ] =          4

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

 Histogramme de la distribution des cellules fantômes sur les rangs :

    valeur minimale =            15068
    valeur maximale =            21272

      1 : [      15068 ;      16308 [ =          4
      2 : [      16308 ;      17549 [ =          1
      3 : [      17549 ;      18790 [ =          1
      4 : [      18790 ;      20031 [ =          8
      5 : [      20031 ;      21272 ] =          4

 Histogramme de la distribution des cellules fantômes
 dans le voisinage standard sur les rangs :

    valeur minimale =            14634
    valeur maximale =            20340

      1 : [      14634 ;      15775 [ =          4
      2 : [      15775 ;      16916 [ =          1
      3 : [      16916 ;      18057 [ =          1
      4 : [      18057 ;      19198 [ =          8
      5 : [      19198 ;      20340 ] =          4

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

 Histogramme de la distribution du nombre de faces interne sur les rangs :

    valeur minimale =           416731
    valeur maximale =           421308

      1 : [     416731 ;     417646 [ =          2
      2 : [     417646 ;     418561 [ =          3
      3 : [     418561 ;     419477 [ =          2
      4 : [     419477 ;     420392 [ =          0
      5 : [     420392 ;     421308 ] =         11

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

 Histogramme de la distribution du nombre de faces de bord sur les rangs :

    valeur minimale =             3425
    valeur maximale =             8802

      1 : [       3425 ;       4500 [ =          6
      2 : [       4500 ;       5575 [ =          6
      3 : [       5575 ;       6651 [ =          2
      4 : [       6651 ;       7726 [ =          2
      5 : [       7726 ;       8802 ] =          2

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

 Histogramme du nombre de faces internes par cellule :

    valeur minimale =                3
    valeur maximale =                6

      1 : [          3 ;          4 [ =          4
      2 : [          4 ;          5 [ =       1348
      3 : [          5 ;          6 ] =    2478648

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

 Histogramme de la distribution du nombre de domaines voisins sur les rangs :

    valeur minimale =               12
    valeur maximale =               17

      1 : [         12 ;         13 [ =          1
      2 : [         13 ;         14 [ =          6
      3 : [         14 ;         15 [ =          5
      4 : [         15 ;         16 [ =          4
      5 : [         16 ;         17 ] =          2

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

 Définition globale du nombre d'éléments (cellules, sommets, faces...)
 Synchronisation des familles des cellules

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

 Renumérotation du maillage:

   renumérotation des cellules :
     pré-numérotation                              pas de renumérotation
     cellules adjacentes aux halos en dernier :    non
     numérotation :                                pas de renumérotation

   renumérotation des faces internes :
     pré-ordonnancement par cellules adjacentes :  id le plus bas en premier
     faces adjacentes aux halos en dernier :       non
     numérotation :                                cellules adjacentes

   renumérotation des faces de bord :
     numérotation :                                cellules adjacentes

   renumérotation des sommets :
     numérotation :                                pas de renumérotation

 Numérotation pour cellules :

 type : défaut

 Numérotation pour faces intérieures :

 type : défaut

 Numérotation pour faces de bord :

 type : défaut

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

 Histogramme de la largeur de bande de matrice maillage volumique sur les rangs :

    valeur minimale =           143186
    valeur maximale =           157518

      1 : [     143186 ;     146052 [ =          1
      2 : [     146052 ;     148918 [ =          3
      3 : [     148918 ;     151785 [ =          5
      4 : [     151785 ;     154651 [ =          8
      5 : [     154651 ;     157518 ] =          1

 Histogramme du profil/lignes de matrice maillage volumique sur les rangs :

    valeur minimale =             9289
    valeur maximale =            14099

      1 : [       9289 ;      10251 [ =          3
      2 : [      10251 ;      11213 [ =          1
      3 : [      11213 ;      12175 [ =          4
      4 : [      12175 ;      13137 [ =          4
      5 : [      13137 ;      14099 ] =          6

 Coordonnées du maillage         minimale    et maximale
                       X : -1.4210855e-14  1.2000000e+02
                       Y :  0.0000000e+00  2.4000000e+02
                       Z :  0.0000000e+00  1.0000000e+02
 Maillage
     Nombre de cellules :       2480000
     Nombre de faces internes : 7413200
     Nombre de faces de bord :  93600
     Nombre de sommets :        2547261

 Faces périodiques (qui sont aussi des faces intérieures) :
     Périodicité  1 :         20000 couples de faces

 Groupes :
    "7"
       cellules :               2480000
       faces intérieures :        40000
       faces de bord :            93600
    "Group_bound"
       faces intérieures :        40000
       faces de bord :            93600
    "east"
       faces intérieures :        20000
    "ground"
       faces de bord :             8800
    "input"
       faces de bord :            10000
    "obstacles"
       faces de bord :            36000
    "outlet"
       faces de bord :            10000
    "top"
       faces de bord :            28800
    "west"
       faces intérieures :        20000

 --- Information sur les volumes
       Volume de controle minimal =  1.0000000e+00
       Volume de controle maximal =  1.0000000e+00
       Volume total du domaine    =  2.4800000e+06

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

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

 Computing geometric quantities (0.275 s)

 --- Information on volume zones
  Volume zone "cells"
    id              = 0
    Number of cells = 2480000
    Volume          =  2.4800000e+06
    Fluid volume    =  2.4800000e+06
    Surface         = -1 (not computed)
    Fluid surface   = -1 (not computed)
  Volume zone "all_cells"
    id              = 1
    Number of cells = 2480000
    Volume          =  2.4800000e+06
    Fluid volume    =  2.4800000e+06
    Surface         = -1 (not computed)
    Fluid surface   = -1 (not computed)

 --- Information on boundary zones
  Boundary zone "boundary_faces"
    id              = 0
    Number of faces = 93600
    Surface         =  9.3600000e+04
    Fluid surface   =  9.3600000e+04
    Perimeter       = -1 (not computed)
    Fluid perimeter = -1 (not computed)
  Boundary zone "BC_4"
    id              = 1
    Number of faces = 8800
    Surface         =  8.8000000e+03
    Fluid surface   =  8.8000000e+03
    Perimeter       = -1 (not computed)
    Fluid perimeter = -1 (not computed)
  Boundary zone "BC_5"
    id              = 2
    Number of faces = 10000
    Surface         =  1.0000000e+04
    Fluid surface   =  1.0000000e+04
    Perimeter       = -1 (not computed)
    Fluid perimeter = -1 (not computed)
  Boundary zone "BC_6"
    id              = 3
    Number of faces = 36000
    Surface         =  3.6000000e+04
    Fluid surface   =  3.6000000e+04
    Perimeter       = -1 (not computed)
    Fluid perimeter = -1 (not computed)
  Boundary zone "BC_7"
    id              = 4
    Number of faces = 10000
    Surface         =  1.0000000e+04
    Fluid surface   =  1.0000000e+04
    Perimeter       = -1 (not computed)
    Fluid perimeter = -1 (not computed)
  Boundary zone "BC_8"
    id              = 5
    Number of faces = 28800
    Surface         =  2.8800000e+04
    Fluid surface   =  2.8800000e+04
    Perimeter       = -1 (not computed)
    Fluid perimeter = -1 (not computed)

 Sondes : "probes":
   distance maximale entre centres cellules et coordonnées demandées : 7.500e-01

 Limitation du voisinage étendu par non-orthogonalité
 ----------------------------------------------------

 Taille de la connectivité cellules-cellules complète :     48858136
 Taille de la connectivité cellules-cellules filtrée :             0
 48858136 connexions supprimées, soit un ratio de    0 % utilisées
                                                             
       ALMAX  =    0.13536E+03 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.


MASS SOURCE TERMS TREATMENT ACTIVATED 
                 ON A TOTAL OF       2400 CELLS

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

 Reading dimensions for meteo profiles
 ------------------------------------------------------------- 


 Reading meteo profiles data
 
 ===================================================
 printing meteo profiles
 year, quant-day, hour, minute, second:
 2016    9  17   8      0.00
 tmmet(itp):
  0.000E+00
 zdmet, umet, vmet, ekmet, epmet:
     2.00    1.50    0.00 0.214E+00 0.398E-01
     4.00    1.50    0.00 0.214E+00 0.398E-01
     6.00    1.50    0.00 0.214E+00 0.398E-01
     8.00    1.50    0.00 0.214E+00 0.398E-01
    10.00    1.50    0.00 0.214E+00 0.398E-01
    12.00    1.50    0.00 0.214E+00 0.398E-01
    14.00    1.50    0.00 0.214E+00 0.398E-01
    16.00    1.50    0.00 0.214E+00 0.398E-01
    18.00    1.50    0.00 0.214E+00 0.398E-01
    20.00    1.50    0.00 0.214E+00 0.398E-01
    22.00    1.85    0.00 0.214E+00 0.199E-01
    24.00    2.28    0.00 0.214E+00 0.994E-02
    26.00    2.53    0.00 0.214E+00 0.663E-02
    28.00    2.71    0.00 0.214E+00 0.497E-02
    30.00    2.85    0.00 0.214E+00 0.398E-02
    32.00    2.96    0.00 0.214E+00 0.331E-02
    34.00    3.06    0.00 0.214E+00 0.284E-02
    36.00    3.14    0.00 0.214E+00 0.248E-02
    38.00    3.21    0.00 0.214E+00 0.221E-02
    40.00    3.28    0.00 0.214E+00 0.199E-02
    42.00    3.34    0.00 0.214E+00 0.181E-02
    44.00    3.39    0.00 0.214E+00 0.166E-02
    46.00    3.44    0.00 0.214E+00 0.153E-02
    48.00    3.48    0.00 0.214E+00 0.142E-02
    50.00    3.53    0.00 0.214E+00 0.133E-02
    52.00    3.57    0.00 0.214E+00 0.124E-02
    54.00    3.60    0.00 0.214E+00 0.117E-02
    56.00    3.64    0.00 0.214E+00 0.110E-02
    58.00    3.67    0.00 0.214E+00 0.105E-02
    60.00    3.71    0.00 0.214E+00 0.994E-03
    62.00    3.74    0.00 0.214E+00 0.947E-03
    63.00    3.75    0.00 0.214E+00 0.924E-03
    64.00    3.76    0.00 0.214E+00 0.903E-03
    65.00    3.78    0.00 0.214E+00 0.883E-03
    66.00    3.79    0.00 0.214E+00 0.864E-03
    67.00    3.80    0.00 0.214E+00 0.846E-03
    68.00    3.82    0.00 0.214E+00 0.828E-03
    69.00    3.83    0.00 0.214E+00 0.811E-03
    70.00    3.84    0.00 0.214E+00 0.795E-03
    71.00    3.86    0.00 0.214E+00 0.779E-03
    72.00    3.87    0.00 0.214E+00 0.764E-03
    73.00    3.88    0.00 0.214E+00 0.750E-03
    74.00    3.89    0.00 0.214E+00 0.736E-03
    75.00    3.90    0.00 0.214E+00 0.723E-03
    76.00    3.91    0.00 0.214E+00 0.710E-03
    77.00    3.92    0.00 0.214E+00 0.697E-03
    78.00    3.93    0.00 0.214E+00 0.685E-03
    79.00    3.95    0.00 0.214E+00 0.674E-03
    80.00    3.96    0.00 0.214E+00 0.663E-03
    81.00    3.97    0.00 0.214E+00 0.652E-03
    82.00    3.98    0.00 0.214E+00 0.641E-03
    83.00    3.99    0.00 0.214E+00 0.631E-03
    84.00    4.00    0.00 0.214E+00 0.621E-03
    85.00    4.01    0.00 0.214E+00 0.612E-03
    86.00    4.01    0.00 0.214E+00 0.602E-03
    87.00    4.02    0.00 0.214E+00 0.593E-03
    88.00    4.03    0.00 0.214E+00 0.585E-03
    89.00    4.04    0.00 0.214E+00 0.576E-03
    90.00    4.05    0.00 0.214E+00 0.568E-03
    91.00    4.06    0.00 0.214E+00 0.560E-03
    92.00    4.07    0.00 0.214E+00 0.552E-03
    93.00    4.08    0.00 0.214E+00 0.545E-03
    94.00    4.09    0.00 0.214E+00 0.537E-03
    95.00    4.09    0.00 0.214E+00 0.530E-03
    96.00    4.10    0.00 0.214E+00 0.523E-03
    97.00    4.11    0.00 0.214E+00 0.516E-03
    98.00    4.12    0.00 0.214E+00 0.510E-03
    99.00    4.13    0.00 0.214E+00 0.503E-03
   100.00    4.13    0.00 0.214E+00 0.497E-03
   101.00    4.14    0.00 0.214E+00 0.491E-03
   102.00    4.15    0.00 0.214E+00 0.485E-03
 ===================================================
 WARNING : option  constant density                 
 WARNING : thermal profile will be ignored          
 ===================================================
 ztmet,ttmet,tpmet,rmet,phmet,qvmet:
     2.00   15.13  288.28  1.2087  100000.000 0.000E+00
     4.00   15.11  288.26  1.2087  100000.000 0.000E+00
     6.00   15.09  288.24  1.2088  100000.000 0.000E+00
     8.00   15.07  288.22  1.2089  100000.000 0.000E+00
    10.00   15.05  288.20  1.2090  100000.000 0.000E+00
    12.00   15.03  288.18  1.2091  100000.000 0.000E+00
    14.00   15.01  288.16  1.2091  100000.000 0.000E+00
    16.00   14.99  288.14  1.2092  100000.000 0.000E+00
    18.00   14.97  288.12  1.2093  100000.000 0.000E+00
    20.00   14.95  288.10  1.2094  100000.000 0.000E+00
    22.00   14.94  288.09  1.2095  100000.000 0.000E+00
    24.00   14.92  288.07  1.2096  100000.000 0.000E+00
    26.00   14.90  288.05  1.2096  100000.000 0.000E+00
    28.00   14.88  288.03  1.2097  100000.000 0.000E+00
    30.00   14.86  288.01  1.2098  100000.000 0.000E+00
    32.00   14.84  287.99  1.2099  100000.000 0.000E+00
    34.00   14.82  287.97  1.2100  100000.000 0.000E+00
    36.00   14.80  287.95  1.2101  100000.000 0.000E+00
    38.00   14.78  287.93  1.2101  100000.000 0.000E+00
    40.00   14.76  287.91  1.2102  100000.000 0.000E+00
    42.00   14.74  287.89  1.2103  100000.000 0.000E+00
    44.00   14.72  287.87  1.2104  100000.000 0.000E+00
    46.00   14.70  287.85  1.2105  100000.000 0.000E+00
    48.00   14.68  287.83  1.2105  100000.000 0.000E+00
    50.00   14.66  287.81  1.2106  100000.000 0.000E+00
    52.00   14.64  287.79  1.2107  100000.000 0.000E+00
    54.00   14.62  287.77  1.2108  100000.000 0.000E+00
    56.00   14.60  287.75  1.2109  100000.000 0.000E+00
    58.00   14.58  287.73  1.2110  100000.000 0.000E+00
    60.00   14.56  287.71  1.2110  100000.000 0.000E+00
    62.00   14.54  287.69  1.2111  100000.000 0.000E+00
    63.00   14.53  287.68  1.2112  100000.000 0.000E+00
    64.00   14.52  287.67  1.2112  100000.000 0.000E+00
    65.00   14.51  287.66  1.2112  100000.000 0.000E+00
    66.00   14.51  287.66  1.2113  100000.000 0.000E+00
    67.00   14.50  287.65  1.2113  100000.000 0.000E+00
    68.00   14.49  287.64  1.2114  100000.000 0.000E+00
    69.00   14.48  287.63  1.2114  100000.000 0.000E+00
    70.00   14.47  287.62  1.2114  100000.000 0.000E+00
    71.00   14.46  287.61  1.2115  100000.000 0.000E+00
    72.00   14.45  287.60  1.2115  100000.000 0.000E+00
    73.00   14.44  287.59  1.2116  100000.000 0.000E+00
    74.00   14.43  287.58  1.2116  100000.000 0.000E+00
    75.00   14.42  287.57  1.2117  100000.000 0.000E+00
    76.00   14.41  287.56  1.2117  100000.000 0.000E+00
    77.00   14.40  287.55  1.2117  100000.000 0.000E+00
    78.00   14.39  287.54  1.2118  100000.000 0.000E+00
    79.00   14.38  287.53  1.2118  100000.000 0.000E+00
    80.00   14.37  287.52  1.2119  100000.000 0.000E+00
    81.00   14.36  287.51  1.2119  100000.000 0.000E+00
    82.00   14.35  287.50  1.2119  100000.000 0.000E+00
    83.00   14.34  287.49  1.2120  100000.000 0.000E+00
    84.00   14.33  287.48  1.2120  100000.000 0.000E+00
    85.00   14.32  287.47  1.2121  100000.000 0.000E+00
    86.00   14.31  287.46  1.2121  100000.000 0.000E+00
    87.00   14.30  287.45  1.2121  100000.000 0.000E+00
    88.00   14.29  287.44  1.2122  100000.000 0.000E+00
    89.00   14.28  287.43  1.2122  100000.000 0.000E+00
    90.00   14.27  287.42  1.2123  100000.000 0.000E+00
    91.00   14.26  287.41  1.2123  100000.000 0.000E+00
    92.00   14.25  287.40  1.2124  100000.000 0.000E+00
    93.00   14.24  287.39  1.2124  100000.000 0.000E+00
    94.00   14.23  287.38  1.2124  100000.000 0.000E+00
    95.00   14.22  287.37  1.2125  100000.000 0.000E+00
    96.00   14.21  287.36  1.2125  100000.000 0.000E+00
    97.00   14.20  287.35  1.2126  100000.000 0.000E+00
    98.00   14.19  287.34  1.2126  100000.000 0.000E+00
    99.00   14.18  287.33  1.2126  100000.000 0.000E+00
   100.00   14.17  287.32  1.2127  100000.000 0.000E+00
   101.00   14.16  287.31  1.2127  100000.000 0.000E+00
   102.00   14.15  287.30  1.2128  100000.000 0.000E+00

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


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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2           0
Smooth wall               5           0
Rough wall                6       44800
Symmetry                  4       48800
Free outlet               3           0
Free inlet               14           0
Convective inlet         16           0
Free surface             15           0
Undefined                 1           0
-------------------------------------------------------------------------


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

   champ        min. init.      max. init.   lim. à min.   lim. à max.
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon
a  scalar1


  ** Valeurs des champs sur cellules
     -------------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]                1.5            4.13          3.3818          3.3818
v  Velocity[Y]                  0               0               0               0
v  Velocity[Z]                  0               0               0               0
v  ǁVelocityǁ                 1.5            4.13          3.3818          3.3818
v  Pressure                     0               0               0               0
v  k                      0.21428         0.21428         0.21428         0.21428
v  epsilon             0.00050006        0.039753       0.0052522       0.0052522
v  scalar1                      0               1        0.064516        0.064516
v  TurbVisc                     0               0               0               0
v  CourantNb                    0               0               0               0
v  FourierNb                    0               0               0               0
v  total_pressure      1.0132e+05      1.0132e+05      1.0132e+05      1.0133e+05



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



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


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




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


 INSTANT    0.100000000E+00   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1200E+01  0.1200E+01
  molecular_viscos  0.1830E-04  0.1830E-04
  turbulent_viscos  0.1247E+00  0.9917E+01
 -----------------------------------------

 --- Diffusivity:
 -----------------------------------------------
 Scalar           Number  Min. value  Max. value
 -----------------------------------------------
 scalar1               1  0.2196E-04  0.2196E-04
 -----------------------------------------------



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5           0         0.000000000E+00
Rough wall                6       44800         0.000000000E+00
Symmetry                  4       48800         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.98983E+00
   Friction velocity        uet   :  0.91005E-13 0.35161E+00
   Friction velocity        uk    :  0.25354E+00 0.25354E+00
   Rough dimensionless dist yplus :  0.50000E+01 0.10000E+03
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



 Temps de calcul limite défini via CS_MAXTIME : 249h:59m:38s

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.65501E+05      16   0.11330E-07   0.52700E+00 0.66389E+00 
c  Velocity[X]                                      0.46191E+00 
c  Velocity[Y]                                      0.14187E-01 
c  Velocity[Z]                                      0.50906E-01 
c  Pressure     0.15932E+03      27   0.99436E-08   0.10000E+01 0.10000E+02 
c  k            0.40546E+04      11   0.45321E-08   0.11912E-04 0.51013E-01 
c  epsilon      0.23160E+03      11   0.22255E-08   0.35421E-05 0.50170E+00 
c  scalar1      0.48000E+04     175   0.10421E-01   0.57093E-02 0.95751E+00 
----------------------------------------------------------------------------
  
  

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

   champ        min. init.      max. init.   lim. à min.   lim. à max.
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon
a  scalar1


  ** Valeurs des champs sur cellules
     -------------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           0.020902          4.1286          3.3453          3.3453
v  Velocity[Y]            -1.6079          1.6079     -2.8247e-09     -2.8247e-09
v  Velocity[Z]            -1.6999          1.6999      1.8682e-08      1.8682e-08
v  ǁVelocityǁ            0.021707          4.1286          3.3491          3.3491
v  Pressure               -163.22          163.22      1.3294e-13      1.8777e-15
v  k                      0.21038         0.21435         0.21395         0.21395
v  epsilon             0.00050272        0.045388       0.0052186       0.0052186
v  scalar1            -3.6539e-05               1        0.064516        0.064516
v  TurbVisc               0.12474          9.9167           4.642           4.642
v  CourantNb                    0               0               0               0
v  FourierNb              0.03119           4.896           2.308           2.308
v  total_pressure      1.0116e+05      1.0149e+05      1.0132e+05      1.0132e+05


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.03119           4.896           2.308           2.308


 INSTANT    0.200000000E+00   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5           0         0.000000000E+00
Rough wall                6       44800         0.554650176E-29
Symmetry                  4       48800         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18383E+01
   Friction velocity        uet   :  0.33102E-03 0.55584E+00
   Friction velocity        uk    :  0.25126E+00 0.25247E+00
   Rough dimensionless dist yplus :  0.50000E+01 0.10000E+03
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.65346E+05      41   0.14990E-03   0.15089E-02 0.35526E-01 
c  Velocity[X]                                      0.13778E-02 
c  Velocity[Y]                                      0.32080E-04 
c  Velocity[Z]                                      0.98942E-04 
c  Pressure     0.59583E+02      24   0.13523E-07   0.10000E+01 0.10000E+02 
c  k            0.40493E+04      13   0.27024E-08   0.12292E-04 0.51888E-01 
c  epsilon      0.23038E+03      11   0.20988E-08   0.26871E-05 0.44009E+00 
c  scalar1      0.47209E+04     133   0.62249E-02   0.16633E-02 0.52158E+00 
----------------------------------------------------------------------------
  
  

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

   champ        min. init.      max. init.   lim. à min.   lim. à max.
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon
a  scalar1


  ** Valeurs des champs sur cellules
     -------------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          0.0060301          4.1256          3.3444          3.3444
v  Velocity[Y]            -1.7416          1.7416      6.9655e-10      6.9655e-10
v  Velocity[Z]            -1.7418          1.8429     -4.7264e-06     -4.7264e-06
v  ǁVelocityǁ           0.0096328          4.1256          3.3483          3.3483
v  Pressure                 -7.31          5.9386     -9.7404e-16      1.1442e-16
v  k                      0.20237         0.23761         0.21366         0.21366
v  epsilon             0.00050473        0.057102       0.0051842       0.0051842
v  scalar1             -2.214e-07               1        0.064516        0.064516
v  TurbVisc               0.10547          9.8618          4.6409          4.6409
v  CourantNb            0.0007962         0.41286          0.3367          0.3367
v  FourierNb               0.0271          4.8867          2.3075          2.3075
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0132e+05


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.027896          5.2991          2.6442          2.6442


 INSTANT    0.300000000E+00   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5           0         0.000000000E+00
Rough wall                6       44800         0.182274825E-29
Symmetry                  4       48800         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.18482E+01
   Friction velocity        uet   :  0.57875E-04 0.56796E+00
   Friction velocity        uk    :  0.24692E+00 0.26699E+00
   Rough dimensionless dist yplus :  0.50000E+01 0.10000E+03
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.65340E+05      41   0.35313E-03   0.70560E-03 0.24296E-01 
c  Velocity[X]                                      0.63108E-03 
c  Velocity[Y]                                      0.16006E-04 
c  Velocity[Z]                                      0.58510E-04 
c  Pressure     0.16425E+02      23   0.50898E-07   0.13009E+01 0.27500E+01 
c  k            0.40438E+04      13   0.38724E-08   0.11342E-04 0.49905E-01 
c  epsilon      0.22856E+03      10   0.44918E-08   0.18810E-05 0.37128E+00 
c  scalar1      0.46786E+04     120   0.46608E-02   0.92774E-03 0.39217E+00 
----------------------------------------------------------------------------
  
  

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

   champ        min. init.      max. init.   lim. à min.   lim. à max.
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon
a  scalar1


  ** Valeurs des champs sur cellules
     -------------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           0.012749           4.123          3.3438          3.3438
v  Velocity[Y]            -1.7814          1.7814      1.2373e-10      1.2373e-10
v  Velocity[Z]            -1.6873          1.8879      2.0841e-06      2.0841e-06
v  ǁVelocityǁ            0.015163           4.123          3.3478          3.3478
v  Pressure               -6.2866          4.9119     -1.5799e-15     -5.7797e-16
v  k                      0.19609          0.2582         0.21338         0.21338
v  epsilon             0.00050636        0.067858       0.0051422       0.0051422
v  scalar1            -3.6079e-09               1        0.064516        0.064516
v  TurbVisc              0.092946          9.8202          4.6399          4.6399
v  CourantNb            0.0006596         0.41256         0.33665         0.33665
v  FourierNb             0.024314          4.8756          2.3071          2.3071
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0132e+05


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.024974          5.2878          2.6437          2.6437


 INSTANT    0.400000000E+00   TIME STEP NUMBER               4
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5           0         0.000000000E+00
Rough wall                6       44800         0.518652934E-29
Symmetry                  4       48800         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.17468E+01
   Friction velocity        uet   :  0.55784E-04 0.54889E+00
   Friction velocity        uk    :  0.24297E+00 0.27832E+00
   Rough dimensionless dist yplus :  0.50000E+01 0.10000E+03
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.65336E+05      41   0.35890E-03   0.42217E-03 0.18794E-01 
c  Velocity[X]                                      0.37247E-03 
c  Velocity[Y]                                      0.11258E-04 
c  Velocity[Z]                                      0.38434E-04 
c  Pressure     0.10067E+02      34   0.54753E-07   0.85418E+00 0.10111E+01 
c  k            0.40384E+04      14   0.24062E-08   0.10689E-04 0.48508E-01 
c  epsilon      0.22649E+03      10   0.43192E-08   0.13758E-05 0.32060E+00 
c  scalar1      0.46464E+04     112   0.34914E-02   0.66939E-03 0.33500E+00 
----------------------------------------------------------------------------
  
  

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

   champ        min. init.      max. init.   lim. à min.   lim. à max.
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon
a  scalar1


  ** Valeurs des champs sur cellules
     -------------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            0.01986          4.1208          3.3433          3.3433
v  Velocity[Y]            -1.7734          1.7734     -4.2981e-11     -4.2981e-11
v  Velocity[Z]            -1.6177          1.8964      9.7058e-06      9.7058e-06
v  ǁVelocityǁ            0.021643          4.1208          3.3473          3.3473
v  Pressure               -5.8663          4.2129     -2.0449e-15      -9.403e-16
v  k                      0.19062         0.27331          0.2131          0.2131
v  epsilon             0.00050774        0.077362       0.0050943       0.0050943
v  scalar1            -1.3523e-10               1        0.064516        0.064516
v  TurbVisc              0.083879          9.7861           4.639           4.639
v  CourantNb           0.00057639          0.4123         0.33661         0.33661
v  FourierNb             0.022244          4.8644          2.3067          2.3067
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0132e+05


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.022821          5.2764          2.6433          2.6433


 INSTANT    0.500000000E+00   TIME STEP NUMBER               5
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5           0         0.000000000E+00
Rough wall                6       44800        -0.141882657E-28
Symmetry                  4       48800         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.16918E+01
   Friction velocity        uet   :  0.14346E-03 0.54274E+00
   Friction velocity        uk    :  0.23914E+00 0.28635E+00
   Rough dimensionless dist yplus :  0.50000E+01 0.10000E+03
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.65333E+05      41   0.40301E-03   0.25860E-03 0.14710E-01 
c  Velocity[X]                                      0.21583E-03 
c  Velocity[Y]                                      0.90253E-05 
c  Velocity[Z]                                      0.33743E-04 
c  Pressure     0.77073E+01      20   0.55455E-07   0.66619E+00 0.90515E+00 
c  k            0.40332E+04      14   0.27048E-08   0.10181E-04 0.47400E-01 
c  epsilon      0.22414E+03      10   0.41750E-08   0.10442E-05 0.28238E+00 
c  scalar1      0.46200E+04     105   0.23097E-02   0.53573E-03 0.30117E+00 
----------------------------------------------------------------------------
  
  

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

   champ        min. init.      max. init.   lim. à min.   lim. à max.
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon
a  scalar1


  ** Valeurs des champs sur cellules
     -------------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           0.025012          4.1188          3.3429          3.3429
v  Velocity[Y]            -1.7598          1.7598      2.2358e-10      2.2358e-10
v  Velocity[Z]            -1.5365          1.8833       1.808e-05       1.808e-05
v  ǁVelocityǁ            0.025841          4.1188           3.347           3.347
v  Pressure               -5.8349          3.7076     -1.8879e-15     -6.9092e-16
v  k                      0.18488          0.2844         0.21282         0.21282
v  epsilon             0.00050895        0.085534        0.005042        0.005042
v  scalar1            -4.8377e-12               1        0.064516        0.064516
v  TurbVisc              0.076952          9.7569          4.6381          4.6381
v  CourantNb           0.00050536         0.41208         0.33657         0.33657
v  FourierNb             0.020628          4.8536          2.3062          2.3062
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0132e+05


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.021134          5.2654          2.6428          2.6428


 INSTANT    0.600000000E+00   TIME STEP NUMBER               6
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5           0         0.000000000E+00
Rough wall                6       44800         0.954266991E-29
Symmetry                  4       48800         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.16335E+01
   Friction velocity        uet   :  0.20631E-03 0.52455E+00
   Friction velocity        uk    :  0.23551E+00 0.29209E+00
   Rough dimensionless dist yplus :  0.50000E+01 0.10000E+03
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.65331E+05      41   0.36706E-03   0.18157E-03 0.12326E-01 
c  Velocity[X]                                      0.14251E-03 
c  Velocity[Y]                                      0.79102E-05 
c  Velocity[Z]                                      0.31156E-04 
c  Pressure     0.56241E+01      27   0.58102E-07   0.50762E+00 0.71860E+00 
c  k            0.40282E+04      14   0.29397E-08   0.97435E-05 0.46424E-01 
c  epsilon      0.22154E+03      10   0.40521E-08   0.83095E-06 0.25499E+00 
c  scalar1      0.45970E+04     104   0.18108E-02   0.45643E-03 0.27922E+00 
----------------------------------------------------------------------------
  
  

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

   champ        min. init.      max. init.   lim. à min.   lim. à max.
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon
a  scalar1


  ** Valeurs des champs sur cellules
     -------------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           0.024382           4.117          3.3425          3.3425
v  Velocity[Y]            -1.7415          1.7415     -5.2356e-10     -5.2356e-10
v  Velocity[Z]            -1.4467          1.8654      2.8314e-05      2.8314e-05
v  ǁVelocityǁ            0.025256           4.117          3.3466          3.3466
v  Pressure               -5.8108          3.2577     -1.3114e-15     -7.3346e-17
v  k                      0.17947         0.29208         0.21254         0.21254
v  epsilon             0.00051003        0.092237       0.0049864       0.0049864
v  scalar1            -1.9585e-13               1        0.064516        0.064516
v  TurbVisc              0.071448           9.731          4.6372          4.6372
v  CourantNb           0.00044038         0.41188         0.33654         0.33654
v  FourierNb             0.019322          4.8433          2.3058          2.3058
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0132e+05


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.019762          5.2549          2.6424          2.6424


 INSTANT    0.700000000E+00   TIME STEP NUMBER               7
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5           0         0.000000000E+00
Rough wall                6       44800         0.808996503E-29
Symmetry                  4       48800         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.15819E+01
   Friction velocity        uet   :  0.24715E-03 0.51828E+00
   Friction velocity        uk    :  0.23204E+00 0.29601E+00
   Rough dimensionless dist yplus :  0.50000E+01 0.10000E+03
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.65328E+05      41   0.38702E-03   0.13411E-03 0.10594E-01 
c  Velocity[X]                                      0.95151E-04 
c  Velocity[Y]                                      0.75493E-05 
c  Velocity[Z]                                      0.31410E-04 
c  Pressure     0.45685E+01      27   0.60934E-07   0.43223E+00 0.74789E+00 
c  k            0.40233E+04      14   0.31342E-08   0.93488E-05 0.45527E-01 
c  epsilon      0.21870E+03      10   0.39461E-08   0.69500E-06 0.23634E+00 
c  scalar1      0.45763E+04      96   0.13921E-02   0.40218E-03 0.26317E+00 
----------------------------------------------------------------------------
  
  

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

   champ        min. init.      max. init.   lim. à min.   lim. à max.
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon
a  scalar1


  ** Valeurs des champs sur cellules
     -------------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          0.0048015          4.1153          3.3421          3.3421
v  Velocity[Y]            -1.7486          1.7486     -7.8063e-10     -7.8063e-10
v  Velocity[Z]            -1.3541          1.8246      3.3919e-05      3.3919e-05
v  ǁVelocityǁ            0.010265          4.1153          3.3463          3.3463
v  Pressure               -5.8429          2.8009     -1.6283e-15     -3.0512e-16
v  k                      0.17401         0.29726         0.21227         0.21227
v  epsilon             0.00051102        0.097659       0.0049283       0.0049283
v  scalar1            -1.8155e-21               1        0.064516        0.064516
v  TurbVisc              0.066942          9.7075          4.6363          4.6363
v  CourantNb           0.00039666          0.4117          0.3365          0.3365
v  FourierNb             0.018236          4.8335          2.3054          2.3054
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0132e+05


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.018632           5.245          2.6419          2.6419


 INSTANT    0.800000000E+00   TIME STEP NUMBER               8
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5           0         0.000000000E+00
Rough wall                6       44800         0.808495761E-29
Symmetry                  4       48800         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.15479E+01
   Friction velocity        uet   :  0.26363E-03 0.50512E+00
   Friction velocity        uk    :  0.22848E+00 0.29863E+00
   Rough dimensionless dist yplus :  0.50000E+01 0.10000E+03
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.65325E+05      41   0.41646E-03   0.99234E-04 0.91132E-02 
c  Velocity[X]                                      0.60089E-04 
c  Velocity[Y]                                      0.75587E-05 
c  Velocity[Z]                                      0.31586E-04 
c  Pressure     0.36605E+01      22   0.63218E-07   0.36005E+00 0.64806E+00 
c  k            0.40186E+04      14   0.33002E-08   0.89553E-05 0.44608E-01 
c  epsilon      0.21566E+03      10   0.38538E-08   0.60830E-06 0.22431E+00 
c  scalar1      0.45574E+04      96   0.15503E-02   0.36359E-03 0.25119E+00 
----------------------------------------------------------------------------
  
  

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

   champ        min. init.      max. init.   lim. à min.   lim. à max.
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon
a  scalar1


  ** Valeurs des champs sur cellules
     -------------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           0.003515          4.1138          3.3418          3.3418
v  Velocity[Y]            -1.7145          1.7144     -4.9712e-09     -4.9712e-09
v  Velocity[Z]            -1.2635          1.7716      3.4963e-05      3.4963e-05
v  ǁVelocityǁ           0.0096341          4.1138           3.346           3.346
v  Pressure               -5.8751          2.3944     -1.1237e-15      2.7872e-16
v  k                      0.16872         0.29991           0.212           0.212
v  epsilon             0.00051192         0.10173       0.0048686       0.0048686
v  scalar1            -4.0919e-23               1        0.064516        0.064516
v  TurbVisc              0.063171           9.686          4.6354          4.6354
v  CourantNb           0.00038683         0.41153         0.33646         0.33646
v  FourierNb             0.017316          4.8243           2.305           2.305
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0132e+05


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.017703          5.2356          2.6415          2.6415


 INSTANT    0.900000000E+00   TIME STEP NUMBER               9
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5           0         0.000000000E+00
Rough wall                6       44800         0.213450816E-29
Symmetry                  4       48800         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.15150E+01
   Friction velocity        uet   :  0.27756E-03 0.50043E+00
   Friction velocity        uk    :  0.22498E+00 0.29996E+00
   Rough dimensionless dist yplus :  0.50000E+01 0.10000E+03
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.65323E+05      41   0.36788E-03   0.82891E-04 0.83294E-02 
c  Velocity[X]                                      0.46170E-04 
c  Velocity[Y]                                      0.72943E-05 
c  Velocity[Z]                                      0.29426E-04 
c  Pressure     0.24424E+01      20   0.64722E-07   0.24620E+00 0.30688E+00 
c  k            0.40140E+04      14   0.34447E-08   0.85669E-05 0.43677E-01 
c  epsilon      0.21245E+03      10   0.37729E-08   0.55294E-06 0.21716E+00 
c  scalar1      0.45399E+04      94   0.13886E-02   0.33286E-03 0.24120E+00 
----------------------------------------------------------------------------
  
  

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

   champ        min. init.      max. init.   lim. à min.   lim. à max.
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon
a  scalar1


  ** Valeurs des champs sur cellules
     -------------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]         -0.0084274          4.1124          3.3416          3.3416
v  Velocity[Y]            -1.6784          1.6784      -9.319e-09      -9.319e-09
v  Velocity[Z]            -1.1775          1.7528      3.4163e-05      3.4163e-05
v  ǁVelocityǁ           0.0087234          4.1124          3.3458          3.3458
v  Pressure               -5.8209          2.2124      -1.464e-15     -3.3739e-17
v  k                      0.16361         0.30102         0.21174         0.21174
v  epsilon             0.00051276         0.10461       0.0048078       0.0048078
v  scalar1            -8.5864e-25               1        0.064516        0.064516
v  TurbVisc              0.059979          9.6659          4.6345          4.6345
v  CourantNb           0.00037306         0.41138         0.33642         0.33642
v  FourierNb             0.016525          4.8155          2.3046          2.3046
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0132e+05


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016898          5.2267           2.641           2.641


 INSTANT    0.100000000E+01   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5           0         0.000000000E+00
Rough wall                6       44800        -0.674980668E-29
Symmetry                  4       48800         0.000000000E+00
Free outlet               3           0         0.000000000E+00
Free inlet               14           0         0.000000000E+00
Convective inlet         16           0         0.000000000E+00
Free surface             15           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR ROUGH WALLS
   --------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.14765E+01
   Friction velocity        uet   :  0.49565E-04 0.49479E+00
   Friction velocity        uk    :  0.22155E+00 0.30051E+00
   Rough dimensionless dist yplus :  0.50000E+01 0.10000E+03
   ------------------------------------------------------   
   Nb of reversal of the velocity at the wall   :          0
------------------------------------------------------------




 Write final restart files
   checkpoint at iteration         10, Physical time    0.10000E+01


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

 Start writing
  Wrote field names and types to checkpoint at iteration 10: 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

   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------
   Variable     Rhs norm      N_iter  Norm. residual   Drift   Time residual
----------------------------------------------------------------------------
c  Velocity     0.65320E+05      41   0.33931E-03   0.72942E-04 0.78138E-02 
c  Velocity[X]                                      0.39367E-04 
c  Velocity[Y]                                      0.70096E-05 
c  Velocity[Z]                                      0.26565E-04 
c  Pressure     0.20789E+01      16   0.92962E-07   0.21182E+00 0.24823E+00 
c  k            0.40097E+04      14   0.35716E-08   0.81840E-05 0.42734E-01 
c  epsilon      0.20912E+03      10   0.37016E-08   0.51699E-06 0.21338E+00 
c  scalar1      0.45235E+04      94   0.17466E-02   0.31002E-03 0.23357E+00 
----------------------------------------------------------------------------
  
  

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

   champ        min. init.      max. init.   lim. à min.   lim. à max.
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon
a  scalar1


  ** Valeurs des champs sur cellules
     -------------------------------

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]          -0.036878           4.111          3.3413          3.3413
v  Velocity[Y]            -1.6377           1.638      1.8568e-12      1.8568e-12
v  Velocity[Z]             -1.115           1.732      3.7952e-05      3.7952e-05
v  ǁVelocityǁ           0.0085664           4.111          3.3455          3.3455
v  Pressure               -5.7927          2.1135     -1.3877e-15      3.2272e-17
v  k                       0.1587         0.30072         0.21149         0.21149
v  epsilon             0.00051355         0.10632       0.0047464       0.0047464
v  scalar1            -1.2684e-26               1        0.064516        0.064516
v  TurbVisc              0.057207          9.6471          4.6336          4.6336
v  CourantNb           0.00034437         0.41124         0.33638         0.33638
v  FourierNb              0.01583          4.8071          2.3042          2.3042
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0132e+05


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.016174          5.2181          2.6405          2.6405



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



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


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





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




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


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

 Destruction des structures et clôture du calcul
