commande : 
 /home/friess/Code_Saturne/ETUDES/testdebug/minirans/RESU/20131117-1625/cs_solver --mpi

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

                                  (R)
                      Code_Saturne

                      Version 3.0.1


  Copyright (C) 1998-2013 EDF S.A., France

  build jeu. 14 nov. 2013 18:32:36 CET
  Version MPI 2.1 (Open MPI 1.4.1)


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

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

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


Configuration locale du cas :

  Date :               dim. 17 nov. 2013 16:25:51 CET
  Système :            Linux 2.6.32-45-generic
  Machine :            friess-HP
  Processeur :         model name	: Intel(R) Xeon(R) CPU E5-1603 0 @ 2.80GHz
  Mémoire :            7930 Mo
  Utilisateur :        friess (Christophe Friess)
  Répertoire :         /home/friess/Code_Saturne/ETUDES/testdebug/minirans/RESU/20131117-1625
  Rangs MPI :          2 (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
                   =======================


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



@
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@
@ @@ ATTENTION : ENTREE DES DONNEES
@    =========
@    REFERENCE VELOCITY  UREF WAS NOT DEFINED
@    or is ill defined  (NEGATIVE value ? ).
@   It IS EQUAL  -0.10000E+14
@
@  calculation can only run if turbulence is defined
@  via a restart file or the interface or the
@  cs_user_initialization subroutine.
@
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@


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


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

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

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


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

 --- Geometry
       NPRFML =              1 (Nb max. family properties   )
       NFML   =              2 (Nb families                 )

 --- Physics
       NVAR   =             12 (Nb variables                )
       NSCAL  =              0 (Nb scalars                  )
       NSCAUS =              0 (Nb user scalars             )
       NSCAPP =              0 (Nb specific physics scalars )
       NPROCE =              6 (Nb cell properties          )
       NPROFA =              1 (Nb internal face properties )
       NPROFB =              2 (Nb boundary face properties )


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


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

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

       OMEGAX =    0.00000E+00 (Rotation vector x component )
       OMEGAY =    0.00000E+00 (Rotation vector y component )
       OMEGAZ =    0.00000E+00 (Rotation vector z component )
       ICORIO =          0 (Coriolis source terms       )

  -- Continuous phase:

       RO0    =    0.11786E+01 (Reference density           )
       VISCL0 =    0.18334E-04 (Ref. molecular dyn. visc.   )
       CP0    =    0.10172E+04 (Ref. specific heat          )
       ICP    =              0 (> 0: variable CP (usphyv)   )
       P0     =    0.10132E+06 (Ref. total pressure         )
       PRED0  =    0.00000E+00 (Ref. reduced pressure       )
       T0     =    0.29315E+03 (Ref. temperature            )

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

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

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


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

 --- Continuous phase:

   - Commons
       ITURB  =             32 (Turbulence model            )
       IDEUCH =              0 (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)     )
       ISCALT =             -1 (Temperature salar number    )

   - Rij-epsilon EBRSM     (ITURB = 32)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =   -0.10000E+14 (Characteristic velocity     )
       IRIJNU =              0 (Matrix stabilization        )
       IRIJRB =              0 (Reconstruct at boundaries   )
       IGRARI =              1 (Account for gravity         )
       ICLSYR =              1 (Symmetry implicitation      )
       ICLPTR =              0 (Wall implicitation          )

 --- 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))

   - EBRSM Rij-epsilon     (ITURB = 32)
       CEBMS1 =    0.17000E+01 (Cs1 coeff.                  )
       CEBMR1 =    0.90000E+00 (Cr1 coeff.                  )
       CEBMR2 =    0.80000E+00 (Cr2 coeff.                  )
       CEBMR3 =    0.65000E+00 (Cr3 coeff.                  )
       CEBMR4 =    0.62500E+00 (Cr4 coeff.                  )
       CEBMR5 =    0.20000E+00 (Cr5 coeff.                  )
       CSEBM  =    0.21000E+00 (Rij Cs diffusion coeff.     )
       CEBMR6 =    0.60000E+00 (Gravity term coeff.         )
       CEBME2 =    0.18300E+01 (Coef Ceps2                  )
       Ce1    =    0.14400E+01 (Coef Ceps1                  )
       SIGEBM =    0.11500E+01 (Coef sigma_eps              )
       XA1    =    0.10000E+00 (Coef A1                     )
       SIGMAK =    0.10000E+01 (Coef sigma_k                )
       XCETA  =    0.80000E+02 (Coef Ceta                   )
       XCT    =    0.60000E+01 (Coef CT                     )


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


 ** 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  =    0.10000E-03 (Minimum time step           )
       DTMAX  =    0.10000E+01 (Maximum time step           )
       DTREF  =    0.10000E-02 (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
------------------------------------
 Pressure              0  0.1000E+01
 VelocityX             1  0.1000E+01
 VelocityY             1  0.1000E+01
 VelocityZ             1  0.1000E+01
 R11                   1  0.1000E+01
 R22                   1  0.1000E+01
 R33                   1  0.1000E+01
 R12                   1  0.1000E+01
 R13                   1  0.1000E+01
 R23                   1  0.1000E+01
 Turb Dissipation      1  0.1000E+01
 Alphap                0  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
---------------------------------------------------------------------
 Pressure              0      1      1      1      0 0.00E+00 0.10E+01
 VelocityX             1      1      1      1      0 0.10E+01 0.10E+01
 VelocityY             1      1      1      1      0 0.10E+01 0.10E+01
 VelocityZ             1      1      1      1      0 0.10E+01 0.10E+01
 R11                   1      1      1      1      0 0.00E+00 0.10E+01
 R22                   1      1      1      1      0 0.00E+00 0.10E+01
 R33                   1      1      1      1      0 0.00E+00 0.10E+01
 R12                   1      1      1      1      0 0.00E+00 0.10E+01
 R13                   1      1      1      1      0 0.00E+00 0.10E+01
 R23                   1      1      1      1      0 0.00E+00 0.10E+01
 Turb Dissipation      1      1      1      1      0 0.00E+00 0.10E+01
 Alphap                0      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
    ------
       IVELCO =              0 (0: segregated solving of the
                                   velocity components during
                                   the prediction step
                                1: coupled solving of the
                                   velocity components       )
       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
-------------------------------------------------------------------
 Pressure            100      2  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityX           100      1  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityY           100      1  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityZ           100      1  0.1000E-04  0.1000E-06  0.0000E+00
 R11                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 R22                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 R33                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 R12                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 R13                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 R23                 100      1  0.1000E-04  0.1000E-06  0.0000E+00
 Turb Dissipation    100      1  0.1000E-04  0.1000E-06  0.0000E+00
 Alphap              100      1  0.1000E-04  0.1000E-06  0.0000E+00
-----------------------------------------------------------

-------------------------------------------
 Variable         IRCFLU IMLIGR      CLIMGR
-------------------------------------------
 Pressure              1     -1  0.1500E+01
 VelocityX             1     -1  0.1500E+01
 VelocityY             1     -1  0.1500E+01
 VelocityZ             1     -1  0.1500E+01
 R11                   1     -1  0.1500E+01
 R22                   1     -1  0.1500E+01
 R33                   1     -1  0.1500E+01
 R12                   1     -1  0.1500E+01
 R13                   1     -1  0.1500E+01
 R23                   1     -1  0.1500E+01
 Turb Dissipation      1     -1  0.1500E+01
 Alphap                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                )


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


 ** CALCULATION OF TEMPORAL MEANS (MOMENTS)
    ---------------------------------------

       NBMOMT =              0 (Number of moments           )

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


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

--------------------------------------------------
 Variable         IRESOL NITMAX      EPSILO IDIRCL
--------------------------------------------------
 Pressure             -1  10000  0.1000E-07      1
 VelocityX            -1  10000  0.1000E-07      1
 VelocityY            -1  10000  0.1000E-07      1
 VelocityZ            -1  10000  0.1000E-07      1
 R11                  -1  10000  0.1000E-07      1
 R22                  -1  10000  0.1000E-07      1
 R33                  -1  10000  0.1000E-07      1
 R12                  -1  10000  0.1000E-07      1
 R13                  -1  10000  0.1000E-07      1
 R23                  -1  10000  0.1000E-07      1
 Turb Dissipation     -1  10000  0.1000E-07      1
 Alphap               -1  10000  0.1000E-07      0
-----------------------------------

       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    )


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


 ** MULTIGRID
    ---------

       NCEGRM =             30 (Max nb cells coarsest grid  )
       NGRMAX =             25 (Max number of levels        )
--------------------------------------
 Variable           IMGR NCYMAX NITMGF
--------------------------------------                       
 Pressure              1    100     10
 VelocityX             0    100     10
 VelocityY             0    100     10
 VelocityZ             0    100     10
 R11                   0    100     10
 R22                   0    100     10
 R33                   0    100     10
 R12                   0    100     10
 R13                   0    100     10
 R23                   0    100     10
 Turb Dissipation      0    100     10
 Alphap                0    100     10
------------------------------

       IMGR   =  0 ou 1        (1: multigrid activated      )
       NCYMAX =                (Max number  of cycles       )
       NITMGF =                (Max nb iter on coarsest grid)


  Paramètres multigrille de regroupement de rangs:
    nombre moyen limite de cellules grossières: 300
    nombre total limite de cellules grossières: 500
    nombre limite de rangs actifs:              1
    nombre de rangs par regroupement:           1

  Type d'agglomération multigrille : algébrique, faces ordonnées par critère

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


 ** 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 =             10 (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

       Number Name
         2 Pressure        
         3 VelocityX       
         4 VelocityY       
         5 VelocityZ       
         6 R11             
         7 R22             
         8 R33             
         9 R12             
        10 R13             
        11 R23             
        12 Turb Dissipation
        13 Alphap          
        14 Density         
         --           --

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

       Number Name                  Nb. probes (-1: all)
         2 Pressure                      -1
         3 VelocityX                     -1
         4 VelocityY                     -1
         5 VelocityZ                     -1
         6 R11                           -1
         7 R22                           -1
         8 R33                           -1
         9 R12                           -1
        10 R13                           -1
        11 R23                           -1
        12 Turb Dissipation              -1
        13 Alphap                        -1
         --           --                --

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

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

         2 Pressure                       0
         3 VelocityX                      0
         4 VelocityY                      0
         5 VelocityZ                      0
         6 R11                            0
         7 R22                            0
         8 R33                            0
         9 R12                            0
        10 R13                            0
        11 R23                            0
        12 Turb Dissipation               0
        13 Alphap                         0
         --           --                --

 --- Additional post-processing variables (ipstdv)
       ipstfo =              0 (Force exerted  at boundary)
       ipstyp =              0 (Yplus          at boundary)
       ipstft =              0 (Thermal flow   at boundary)
       ipsttb =              0 (Temperature    at boundary)
       ipstnu =              0 (Nusselt        at boundary)


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


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

       IALE   =              0 (1: activated                )
       NALINF =              0 (Fluid initialization
                                                  iterations)


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


 Lecture du fichier :  mesh_input
 Fin de la lecture :  mesh_input
 Pas de fichier "partition_input/domain_number_2" disponible;

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

 Partitionnement par courbe fractale : Morton (dans boîte englobante).
  Nombre de cellules par domaine (histogramme) :
    [        200 ;        200 ] =          2

 Écriture du fichier : partition_output/domain_number_2
 Fin de l'écriture :  partition_output/domain_number_2

 Partitionnement terminé (0.343 s)


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

  -1: nom: results
      répertoire: postprocessing
      format: EnSight Gold
      options: 
      dépendence en temps: maillage fixe
      sorties: à la fin du calcul


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

 Construction du halo avec voisinage standard
 ============================================

 Création de l'interface entre faces
 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

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

    valeur minimale =              200
    valeur maximale =              200

      1 : [        200 ;        200 ] =          2

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

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

    valeur minimale =              201
    valeur maximale =              201

      1 : [        201 ;        201 ] =          2

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

 Histogramme de la distribution des cellules fantômes sur les rangs :

    valeur minimale =                1
    valeur maximale =                1

      1 : [          1 ;          1 ] =          2

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

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

    valeur minimale =              200
    valeur maximale =              200

      1 : [        200 ;        200 ] =          2

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

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

    valeur minimale =              801
    valeur maximale =              801

      1 : [        801 ;        801 ] =          2

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

 Histogramme du nombre de faces internes par cellule :

    valeur minimale =                1
    valeur maximale =                2

      1 : [          1 ;          2 ] =        400

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

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

    valeur minimale =                1
    valeur maximale =                1

      1 : [          1 ;          1 ] =          2

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

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

 Renumérotation du maillage:

Vérification de la renumérotation de maillage pour les threads
--------------------------------------------------------------

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

    valeur minimale =                1
    valeur maximale =              200

      1 : [          1 ;         40 [ =          1
      2 : [         40 ;         80 [ =          0
      3 : [         80 ;        120 [ =          0
      4 : [        120 ;        160 [ =          0
      5 : [        160 ;        200 ] =          1

 Histogramme du profil/lignes de matrice maillage volumiqueur les rangs :

    valeur minimale =                1
    valeur maximale =                1

      1 : [          1 ;          1 ] =          2

 Coordonnées du maillage         minimale    et maximale
                       X :  0.0000000e+00  2.0000000e-01
                       Y :  0.0000000e+00  1.0000000e+00
                       Z :  0.0000000e+00  2.0000000e-01
 Maillage
     Nombre de cellules :       400
     Nombre de faces internes : 399
     Nombre de faces de bord :  1602
     Nombre de sommets :        1604

 Groupes :
    "7"
       cellules :                   400

 --- Information sur les volumes
       Volume de controle minimal =  5.7828197e-08
       Volume de controle maximal =  9.5243653e-04
       Volume total du domaine    =  4.0000000e-02

  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 %

 Calcul des grandeurs géométriques (0.158 s)
                                                             
       ALMAX  =    0.34236E+00 (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
 -----------------------------------------                   
  Pressure          0.0000E+00  0.0000E+00
  VelocityX         0.2126E+02  0.2126E+02
  VelocityY         0.0000E+00  0.0000E+00
  VelocityZ         0.1000E+01  0.1000E+01
  R11               0.2511E+01  0.2511E+01
  R22               0.2511E+01  0.2511E+01
  R33               0.2511E+01  0.2511E+01
  R12               0.0000E+00  0.0000E+00
  R13               0.0000E+00  0.0000E+00
  R23               0.0000E+00  0.0000E+00
  Turb Dissipation  0.9437E+04  0.9437E+04
  Alphap            0.1000E+01  0.1000E+01
 ---------------------------------

  Local Time Step   0.1000E-02  0.1000E-02
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.100000000E-02   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  Density           0.1179E+01  0.1179E+01
  Laminar Viscosit  0.1833E-04  0.1833E-04
  Turb Viscosity    0.1595E-03  0.1595E-03
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2           0
Smooth wall               5         401
Rough wall                6           0
Symmetry                  4        1201
Free outlet               3           0
Undefined                 1           0
-------------------------------------------------------------------------



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         401         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        1201         0.000000000E+00
Free outlet               3           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   :  0.82943E+00 0.21401E+02
   Friction velocity        uk    :  0.82943E+00 0.21401E+02
   Dimensionless distance   yplus :  0.99451E+00 0.53321E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :        401
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54869E-02     232   0.85461E-08   0.10000E+01 
c  VelocityX    0.11069E+03    3811   0.99536E-08   0.28176E+02 
c  VelocityY    0.11838E+00    4344   0.99648E-08   0.49343E-05 
c  VelocityZ    0.52066E+01    3811   0.99537E-08   0.62338E-01 
c  R11          0.36005E+02   10000   0.33501E-04   0.14296E+04 
c  R22          0.36005E+02   10000   0.33501E-04   0.14296E+04 
c  R33          0.36003E+02   10000   0.33504E-04   0.14335E+04 
c  R12          0.25168E+01    4307   0.99427E-08   0.16643E-02 
c  R13          0.17475E-06    4643   0.99658E-08   0.78431E-13 
c  R23          0.11838E+00    4307   0.99428E-08   0.39032E-05 
c  Turb Dissipa 0.29044E+10    5672   0.99826E-08   0.47397E+16 
c  Alphap       0.73431E+05      97   0.61034E-08   0.12261E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.21254E-02   0.14945E-01         --         -- 
v  VelocityX    0.12319E+00   0.21260E+02         --         -- 
v  VelocityY   -0.44516E-04   0.58340E-01         --         -- 
v  VelocityZ    0.57946E-02   0.10000E+01         --         -- 
v  R11          0.18200E-01   0.24794E+01          0          0 
v  R22          0.17983E-01   0.24794E+01          0          0 
v  R33          0.14720E-02   0.14245E+01          0          0 
v  R12         -0.19142E-14   0.16090E+00          4          0 
v  R13         -0.66745E-07   0.12501E-07          0          0 
v  R23         -0.90982E-11   0.78840E-02          1          0 
v  Turb Dissipa 0.16897E+04   0.22340E+09          0          0 
v  Alphap       0.29466E-02   0.10000E+01          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  R11          0.18200E-01   0.24794E+01          0          0 
a  R22          0.17983E-01   0.24794E+01          0          0 
a  R33          0.14720E-02   0.14245E+01          0          0 
a  R12         -0.19142E-14   0.16970E+00          4          0 
a  R13         -0.66745E-07   0.12501E-07          0          0 
a  R23         -0.90982E-11   0.79821E-02          1          0 
a  Turb Dissipa 0.16897E+04   0.22340E+09          0          0 
a  Alphap       0.29466E-02   0.10000E+01          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.10000E+00  0.48809E+00  0.10000E+00  
Courant max  0.00000E+00  0.10000E+00  0.48809E+00  0.10000E+00  
Fourier min  0.53865E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Fourier max  0.13093E+06  0.10000E+00  0.10000E+01  0.10000E+00  
Cou_Fou min  0.53865E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Cou_Fou max  0.13093E+06  0.10000E+00  0.10000E+01  0.10000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                1:        0.16423E+02

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


 INSTANT    0.200000000E-02   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         401         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        1201         0.000000000E+00
Free outlet               3           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   :  0.91473E-02 0.16291E+01
   Friction velocity        uk    :  0.91473E-02 0.16291E+01
   Dimensionless distance   yplus :  0.75704E-01 0.53321E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :        401
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.58183E-01     234   0.66023E-08   0.10000E+01 
c  VelocityX    0.11069E+03    3182   0.99698E-08   0.39534E+01 
c  VelocityY    0.20044E-01    5971   0.38152E-06   0.32360E-04 
c  VelocityZ    0.52066E+01    3184   0.99673E-08   0.87872E-02 
c  R11          0.54411E+03   10000   0.12322E-05   0.21260E+03 
c  R22          0.10699E+03   10000   0.62664E-05   0.21267E+03 
c  R33          0.24046E+03   10000   0.27883E-05   0.21051E+03 
c  R12          0.13841E+00    1627   0.99699E-08   0.16451E-02 
c  R13          0.92723E-03      52   0.88516E-08   0.79065E-12 
c  R23          0.83330E-02    1487   0.99822E-08   0.38489E-05 
c  Turb Dissipa 0.11817E+07   10000   0.18430E-05   0.47276E+16 
c  Alphap       0.31408E+05      49   0.87629E-08   0.94868E-01 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.11092E+01   0.43131E-01         --         -- 
v  VelocityX    0.65332E-01   0.21260E+02         --         -- 
v  VelocityY   -0.64506E-02   0.39781E-02         --         -- 
v  VelocityZ    0.30800E-02   0.10000E+01         --         -- 
v  R11          0.22659E-01   0.90872E+00          0          0 
v  R22          0.79874E-07   0.90872E+00          0          0 
v  R33          0.87195E-02   0.90872E+00          0          0 
v  R12         -0.58775E-15   0.90973E-03          0          0 
v  R13         -0.75745E-07   0.23664E-05          0          0 
v  R23         -0.35709E-05   0.55654E-04          0          0 
v  Turb Dissipa 0.65802E+03   0.94364E+06          0          0 
v  Alphap       0.36065E-01   0.10000E+01          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  R11          0.22659E-01   0.90872E+00          0          0 
a  R22          0.79874E-07   0.90872E+00          0          0 
a  R33          0.87195E-02   0.90872E+00          0          0 
a  R12         -0.58775E-15   0.90973E-03          0          0 
a  R13         -0.75745E-07   0.23664E-05          0          0 
a  R23         -0.35709E-05   0.55654E-04          0          0 
a  Turb Dissipa 0.65802E+03   0.94364E+06          0          0 
a  Alphap       0.36065E-01   0.10000E+01          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.10000E+00  0.10000E+01  0.10000E+00  
Courant max  0.57068E-03  0.10000E+00  0.29767E-04  0.10000E+00  
Fourier min  0.79531E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Fourier max  0.11695E+06  0.10000E+00  0.22047E-05  0.10000E+00  
Cou_Fou min  0.79544E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Cou_Fou max  0.11695E+06  0.10000E+00  0.22047E-05  0.10000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                2:        0.13180E+02

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


 INSTANT    0.300000000E-02   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         401         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        1201         0.000000000E+00
Free outlet               3           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   :  0.48748E-02 0.11864E+01
   Friction velocity        uk    :  0.48748E-02 0.11864E+01
   Dimensionless distance   yplus :  0.55130E-01 0.53321E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :        401
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.20018E-01     260   0.51998E-08   0.37854E+00 
c  VelocityX    0.11069E+03    2860   0.99179E-08   0.14682E+01 
c  VelocityY    0.95103E-02    4233   0.12820E-04   0.13058E-03 
c  VelocityZ    0.52066E+01    2855   0.99387E-08   0.32420E-02 
c  R11          0.62315E+01   10000   0.95010E-04   0.55016E+02 
c  R22          0.60592E+01   10000   0.97698E-04   0.55173E+02 
c  R33          0.61397E+01   10000   0.96430E-04   0.55019E+02 
c  R12          0.51178E-01    1917   0.99705E-08   0.74354E-03 
c  R13          0.10385E-04     120   0.88739E-08   0.20728E-10 
c  R23          0.81768E-02    1159   0.99814E-08   0.35290E-04 
c  Turb Dissipa 0.94778E+06   10000   0.11008E-05   0.59208E+10 
c  Alphap       0.19392E+05      90   0.91111E-08   0.37093E-01 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.18979E+00   0.75402E+00         --         -- 
v  VelocityX    0.45342E-01   0.21260E+02         --         -- 
v  VelocityY   -0.51644E-02   0.87250E-02         --         -- 
v  VelocityZ    0.21296E-02   0.10000E+01         --         -- 
v  R11          0.18875E-01   0.72894E+00          0          0 
v  R22          0.11116E-08   0.68882E+00          0          0 
v  R33          0.72596E-02   0.70751E+00          0          0 
v  R12         -0.23611E-13   0.49182E-01          0          0 
v  R13         -0.83042E-06   0.14054E-04          0          0 
v  R23         -0.74283E-02   0.30881E-01          0          0 
v  Turb Dissipa 0.33961E+03   0.89569E+06          0          0 
v  Alphap       0.64310E-02   0.10000E+01          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  R11          0.18875E-01   0.72894E+00          0          0 
a  R22          0.11116E-08   0.68882E+00          0          0 
a  R33          0.72596E-02   0.70751E+00          0          0 
a  R12         -0.23611E-13   0.49182E-01          0          0 
a  R13         -0.83042E-06   0.14054E-04          0          0 
a  R23         -0.74283E-02   0.30881E-01          0          0 
a  Turb Dissipa 0.33961E+03   0.89569E+06          0          0 
a  Alphap       0.64310E-02   0.10000E+01          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.10000E+00  0.72285E-06  0.10000E+00  
Courant max  0.12221E-01  0.10000E+00  0.99997E+00  0.10000E+00  
Fourier min  0.86117E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Fourier max  0.15286E+06  0.10000E+00  0.22047E-05  0.10000E+00  
Cou_Fou min  0.86407E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Cou_Fou max  0.15286E+06  0.10000E+00  0.22047E-05  0.10000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                3:        0.12670E+02

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


 INSTANT    0.400000000E-02   TIME STEP NUMBER               4
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         401         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        1201         0.000000000E+00
Free outlet               3           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   :  0.35796E-02 0.98833E+00
   Friction velocity        uk    :  0.35796E-02 0.98833E+00
   Dimensionless distance   yplus :  0.45928E-01 0.53321E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :        401
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.20252E-01     250   0.99452E-08   0.55124E+00 
c  VelocityX    0.11069E+03    2652   0.99098E-08   0.89522E+00 
c  VelocityY    0.66919E-02    5899   0.54877E-04   0.11194E-04 
c  VelocityZ    0.52065E+01    2640   0.46535E-07   0.20992E-02 
c  R11          0.42905E+01   10000   0.10595E-03   0.19527E+02 
c  R22          0.40631E+01   10000   0.11196E-03   0.19560E+02 
c  R33          0.41001E+01   10000   0.11087E-03   0.19530E+02 
c  R12          0.12293E-01    1186   0.99515E-08   0.30353E-02 
c  R13          0.62000E-03     162   0.87593E-08   0.91995E-05 
c  R23          0.58722E-03    1176   0.99720E-08   0.33121E-04 
c  Turb Dissipa 0.78940E+06   10000   0.70489E-06   0.39713E+09 
c  Alphap       0.13930E+05      90   0.86595E-08   0.23853E-01 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.83224E-01   0.10381E+01         --         -- 
v  VelocityX    0.39098E-01   0.21260E+02         --         -- 
v  VelocityY   -0.33951E-02   0.75223E-02         --         -- 
v  VelocityZ    0.18458E-02   0.10000E+01         --         -- 
v  R11          0.15724E-01   0.70636E+00          0          0 
v  R22          0.45578E-09   0.55177E+00          0          0 
v  R33          0.60449E-02   0.59221E+00          0          0 
v  R12         -0.76072E-13   0.14164E+00          0          0 
v  R13         -0.27717E-03   0.58800E-02          0          0 
v  R23         -0.11115E-04   0.67020E-02          0          0 
v  Turb Dissipa 0.18712E+03   0.74298E+06          0          0 
v  Alphap       0.54439E-02   0.10000E+01          1          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  R11          0.15724E-01   0.70636E+00          0          0 
a  R22          0.45578E-09   0.55177E+00          0          0 
a  R33          0.60449E-02   0.59221E+00          0          0 
a  R12         -0.76072E-13   0.14164E+00          0          0 
a  R13         -0.27717E-03   0.58800E-02          0          0 
a  R23         -0.11115E-04   0.67020E-02          0          0 
a  Turb Dissipa 0.18712E+03   0.74298E+06          0          0 
a  Alphap       0.54439E-02   0.10000E+01          1          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.10000E+00  0.10000E+01  0.10000E+00  
Courant max  0.45236E-01  0.10000E+00  0.29767E-04  0.10000E+00  
Fourier min  0.87867E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Fourier max  0.16766E+06  0.10000E+00  0.22047E-05  0.10000E+00  
Cou_Fou min  0.88939E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Cou_Fou max  0.16766E+06  0.10000E+00  0.22047E-05  0.10000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                4:        0.12769E+02

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


 INSTANT    0.500000000E-02   TIME STEP NUMBER               5
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         401         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        1201         0.000000000E+00
Free outlet               3           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   :  0.31606E-02 0.91777E+00
   Friction velocity        uk    :  0.31606E-02 0.91777E+00
   Dimensionless distance   yplus :  0.42649E-01 0.53321E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :        401
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.12246E-01     233   0.81128E-08   0.42673E+00 
c  VelocityX    0.11069E+03    2469   0.99560E-08   0.60789E+00 
c  VelocityY    0.38911E-02    5993   0.67310E-04   0.54229E-04 
c  VelocityZ    0.52065E+01    2470   0.42041E-07   0.14106E-02 
c  R11          0.31987E+01   10000   0.10874E-03   0.84415E+01 
c  R22          0.30049E+01   10000   0.11580E-03   0.84261E+01 
c  R33          0.30373E+01   10000   0.11452E-03   0.84238E+01 
c  R12          0.52498E-02    2347   0.99750E-08   0.97395E-03 
c  R13          0.13297E-02     156   0.94224E-08   0.73005E-04 
c  R23          0.25758E-03    1980   0.99757E-08   0.33845E-05 
c  Turb Dissipa 0.65752E+06   10000   0.49604E-06   0.11215E+09 
c  Alphap       0.10791E+05      89   0.93088E-08   0.29544E-02 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.21013E+00   0.92303E+00         --         -- 
v  VelocityX    0.35264E-01   0.21260E+02         --         -- 
v  VelocityY   -0.33127E-02   0.52367E-02         --         -- 
v  VelocityZ    0.16674E-02   0.10001E+01         --         -- 
v  R11          0.13098E-01   0.92550E+00          0          0 
v  R22          0.32025E-09   0.45686E+00          0          0 
v  R33          0.50335E-02   0.49171E+00          0          0 
v  R12         -0.24200E-11   0.93127E-01          0          0 
v  R13         -0.88289E-07   0.22314E-01          0          0 
v  R23         -0.35482E-04   0.44478E-02          0          0 
v  Turb Dissipa 0.10548E+03   0.62060E+06          0          0 
v  Alphap       0.51306E-02   0.10000E+01          1          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  R11          0.13098E-01   0.92550E+00          0          0 
a  R22          0.32025E-09   0.45686E+00          0          0 
a  R33          0.50335E-02   0.49171E+00          0          0 
a  R12         -0.24200E-11   0.93127E-01          0          0 
a  R13         -0.88289E-07   0.22314E-01          0          0 
a  R23         -0.35482E-04   0.44478E-02          0          0 
a  Turb Dissipa 0.10548E+03   0.62060E+06          0          0 
a  Alphap       0.51306E-02   0.10000E+01          1          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.10000E+00  0.10000E+01  0.10000E+00  
Courant max  0.42855E-01  0.10000E+00  0.29767E-04  0.10000E+00  
Fourier min  0.87958E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Fourier max  0.17500E+06  0.10000E+00  0.22047E-05  0.10000E+00  
Cou_Fou min  0.88973E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Cou_Fou max  0.17500E+06  0.10000E+00  0.22047E-05  0.10000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                5:        0.13141E+02

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


 INSTANT    0.600000000E-02   TIME STEP NUMBER               6
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         401         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        1201         0.000000000E+00
Free outlet               3           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   :  0.28988E-02 0.87160E+00
   Friction velocity        uk    :  0.28988E-02 0.87160E+00
   Dimensionless distance   yplus :  0.40503E-01 0.53321E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :        401
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.73322E-02     260   0.56003E-08   0.31625E+00 
c  VelocityX    0.11069E+03    2463   0.99394E-08   0.43100E+00 
c  VelocityY    0.25638E-02    5937   0.72810E-05   0.22822E-04 
c  VelocityZ    0.52065E+01    2474   0.99534E-08   0.96344E-03 
c  R11          0.25440E+01   10000   0.10605E-03   0.41482E+01 
c  R22          0.23581E+01   10000   0.11435E-03   0.41477E+01 
c  R33          0.23898E+01   10000   0.11289E-03   0.41482E+01 
c  R12          0.53822E-02     868   0.99656E-08   0.10866E-03 
c  R13          0.16986E-02     189   0.94626E-08   0.53118E-05 
c  R23          0.24702E-03     882   0.99285E-08   0.41556E-06 
c  Turb Dissipa 0.54766E+06   10000   0.37338E-06   0.95987E+08 
c  Alphap       0.87648E+04      97   0.89970E-08   0.18834E-03 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.16461E+00   0.68790E+00         --         -- 
v  VelocityX    0.31827E-01   0.21260E+02         --         -- 
v  VelocityY   -0.28617E-02   0.37068E-02         --         -- 
v  VelocityZ    0.15019E-02   0.10001E+01         --         -- 
v  R11          0.10911E-01   0.88253E+00          0          0 
v  R22          0.24376E-09   0.38730E+00          0          0 
v  R33          0.41914E-02   0.41142E+00          0          0 
v  R12         -0.18296E-11   0.76832E-01          0          0 
v  R13         -0.85267E-07   0.23118E-01          0          0 
v  R23         -0.27873E-04   0.32268E-02          0          0 
v  Turb Dissipa 0.66802E+02   0.51787E+06          0          0 
v  Alphap       0.49797E-02   0.10000E+01          1          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  R11          0.10911E-01   0.88253E+00          0          0 
a  R22          0.24376E-09   0.38730E+00          0          0 
a  R33          0.41914E-02   0.41142E+00          0          0 
a  R12         -0.18296E-11   0.76832E-01          0          0 
a  R13         -0.85267E-07   0.23118E-01          0          0 
a  R23         -0.27873E-04   0.32268E-02          0          0 
a  Turb Dissipa 0.66802E+02   0.51787E+06          0          0 
a  Alphap       0.49797E-02   0.10000E+01          1          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.10000E+00  0.10000E+01  0.10000E+00  
Courant max  0.47280E-02  0.10000E+00  0.29767E-04  0.10000E+00  
Fourier min  0.87395E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Fourier max  0.17891E+06  0.10000E+00  0.22047E-05  0.10000E+00  
Cou_Fou min  0.87507E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Cou_Fou max  0.17891E+06  0.10000E+00  0.22047E-05  0.10000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                6:        0.12611E+02

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


 INSTANT    0.700000000E-02   TIME STEP NUMBER               7
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         401         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        1201         0.000000000E+00
Free outlet               3           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   :  0.26609E-02 0.82941E+00
   Friction velocity        uk    :  0.26609E-02 0.82941E+00
   Dimensionless distance   yplus :  0.38479E-01 0.53321E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :        401
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57515E-02     250   0.67718E-08   0.29799E+00 
c  VelocityX    0.11069E+03    2381   0.99004E-08   0.34022E+00 
c  VelocityY    0.22641E-02    5856   0.24526E-04   0.14912E-05 
c  VelocityZ    0.52065E+01    2392   0.99409E-08   0.74661E-03 
c  R11          0.20905E+01   10000   0.10178E-03   0.22494E+01 
c  R22          0.19258E+01   10000   0.11038E-03   0.22491E+01 
c  R33          0.19542E+01   10000   0.10889E-03   0.22494E+01 
c  R12          0.47526E-02     929   0.99667E-08   0.31238E-04 
c  R13          0.14661E-02     218   0.91412E-08   0.27469E-05 
c  R23          0.23364E-03    1003   0.99494E-08   0.20956E-06 
c  Turb Dissipa 0.45616E+06   10000   0.29600E-06   0.65674E+08 
c  Alphap       0.73541E+04      99   0.70918E-08   0.58474E-03 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.79109E-01   0.49469E+00         --         -- 
v  VelocityX    0.29201E-01   0.21260E+02         --         -- 
v  VelocityY   -0.27077E-02   0.25511E-02         --         -- 
v  VelocityZ    0.13740E-02   0.10000E+01         --         -- 
v  R11          0.90891E-02   0.86802E+00          0          0 
v  R22          0.17097E-09   0.33429E+00          0          0 
v  R33          0.34902E-02   0.35124E+00          0          0 
v  R12         -0.28890E-11   0.79315E-01          0          0 
v  R13         -0.82042E-07   0.24326E-01          0          0 
v  R23         -0.40380E-04   0.39824E-02          0          0 
v  Turb Dissipa 0.48787E+02   0.43218E+06          0          0 
v  Alphap       0.47037E-02   0.10000E+01          2          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  R11          0.90891E-02   0.86802E+00          0          0 
a  R22          0.17097E-09   0.33429E+00          0          0 
a  R33          0.34902E-02   0.35124E+00          0          0 
a  R12         -0.28890E-11   0.79315E-01          0          0 
a  R13         -0.82042E-07   0.24326E-01          0          0 
a  R23         -0.40380E-04   0.39824E-02          0          0 
a  Turb Dissipa 0.48787E+02   0.43218E+06          0          0 
a  Alphap       0.47037E-02   0.10000E+01          2          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.10000E+00  0.72285E-06  0.10000E+00  
Courant max  0.20034E-01  0.10000E+00  0.99997E+00  0.10000E+00  
Fourier min  0.86564E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Fourier max  0.18098E+06  0.10000E+00  0.22047E-05  0.10000E+00  
Cou_Fou min  0.87039E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Cou_Fou max  0.18098E+06  0.10000E+00  0.22047E-05  0.10000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                7:        0.12555E+02

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


 INSTANT    0.800000000E-02   TIME STEP NUMBER               8
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         401         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        1201         0.000000000E+00
Free outlet               3           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   :  0.24767E-02 0.82941E+00
   Friction velocity        uk    :  0.24767E-02 0.82941E+00
   Dimensionless distance   yplus :  0.36858E-01 0.53320E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :        401
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.40697E-02     250   0.65591E-08   0.24432E+00 
c  VelocityX    0.11069E+03    2297   0.99006E-08   0.27445E+00 
c  VelocityY    0.15099E-02    5888   0.24549E-04   0.34654E-05 
c  VelocityZ    0.52065E+01    2301   0.99333E-08   0.60433E-03 
c  R11          0.17624E+01   10000   0.96783E-04   0.13135E+01 
c  R22          0.16184E+01   10000   0.10532E-03   0.13125E+01 
c  R33          0.16436E+01   10000   0.10378E-03   0.13127E+01 
c  R12          0.44927E-02    1307   0.99790E-08   0.37183E-04 
c  R13          0.14991E-02     232   0.90611E-08   0.41082E-05 
c  R23          0.22771E-03     870   0.99340E-08   0.10702E-06 
c  Turb Dissipa 0.37995E+06   10000   0.24451E-06   0.48162E+08 
c  Alphap       0.63187E+04      98   0.88629E-08   0.18154E-03 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.38821E-01   0.38130E+00         --         -- 
v  VelocityX    0.27201E-01   0.21260E+02         --         -- 
v  VelocityY   -0.25542E-02   0.19527E-02         --         -- 
v  VelocityZ    0.12779E-02   0.10000E+01         --         -- 
v  R11          0.75712E-02   0.88476E+00          0          0 
v  R22          0.12450E-09   0.29267E+00          0          0 
v  R33          0.29064E-02   0.31081E+00          0          0 
v  R12         -0.49483E-11   0.82253E-01          0          0 
v  R13         -0.79344E-07   0.26737E-01          0          0 
v  R23         -0.53165E-04   0.40939E-02          0          0 
v  Turb Dissipa 0.39066E+02   0.36062E+06          0          0 
v  Alphap       0.44982E-02   0.10000E+01          1          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  R11          0.75712E-02   0.88476E+00          0          0 
a  R22          0.12450E-09   0.29267E+00          0          0 
a  R33          0.29064E-02   0.31081E+00          0          0 
a  R12         -0.49483E-11   0.82253E-01          0          0 
a  R13         -0.79344E-07   0.26737E-01          0          0 
a  R23         -0.53165E-04   0.40939E-02          0          0 
a  Turb Dissipa 0.39066E+02   0.36062E+06          0          0 
a  Alphap       0.44982E-02   0.10000E+01          1          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.10000E+00  0.72285E-06  0.10000E+00  
Courant max  0.20667E-01  0.10000E+00  0.99997E+00  0.10000E+00  
Fourier min  0.85632E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Fourier max  0.18198E+06  0.10000E+00  0.22047E-05  0.10000E+00  
Cou_Fou min  0.86122E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Cou_Fou max  0.18198E+06  0.10000E+00  0.22047E-05  0.10000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                8:        0.12598E+02

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


 INSTANT    0.900000000E-02   TIME STEP NUMBER               9
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2           0         0.000000000E+00
Smooth wall               5         401         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        1201         0.000000000E+00
Free outlet               3           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   :  0.23349E-02 0.82941E+00
   Friction velocity        uk    :  0.23349E-02 0.82941E+00
   Dimensionless distance   yplus :  0.35573E-01 0.53320E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :        401
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.31320E-02     231   0.69408E-08   0.21195E+00 
c  VelocityX    0.11069E+03    2229   0.99178E-08   0.22593E+00 
c  VelocityY    0.10904E-02    5896   0.12831E-04   0.20727E-05 
c  VelocityZ    0.52065E+01    2227   0.99231E-08   0.49896E-03 
c  R11          0.15130E+01   10000   0.91744E-04   0.81257E+00 
c  R22          0.13898E+01   10000   0.99852E-04   0.81144E+00 
c  R33          0.14116E+01   10000   0.98333E-04   0.81162E+00 
c  R12          0.46387E-02    1554   0.99785E-08   0.42553E-04 
c  R13          0.15922E-02     234   0.91537E-08   0.29278E-05 
c  R23          0.23804E-03    1291   0.99853E-08   0.13121E-06 
c  Turb Dissipa 0.31647E+06   10000   0.20882E-06   0.34787E+08 
c  Alphap       0.55282E+04      97   0.90286E-08   0.34540E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.38506E-01   0.32745E+00         --         -- 
v  VelocityX    0.25601E-01   0.21260E+02         --         -- 
v  VelocityY   -0.24355E-02   0.17503E-02         --         -- 
v  VelocityZ    0.12026E-02   0.10000E+01         --         -- 
v  R11          0.63067E-02   0.90097E+00          0          0 
v  R22          0.91083E-10   0.25925E+00          0          0 
v  R33          0.24202E-02   0.28623E+00          0          0 
v  R12         -0.32249E-11   0.85691E-01          0          0 
v  R13         -0.76905E-07   0.28904E-01          0          0 
v  R23         -0.65607E-04   0.40417E-02          0          0 
v  Turb Dissipa 0.32596E+02   0.30088E+06          0          0 
v  Alphap       0.43081E-02   0.10000E+01          2          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  R11          0.63067E-02   0.90097E+00          0          0 
a  R22          0.91083E-10   0.25925E+00          0          0 
a  R33          0.24202E-02   0.28623E+00          0          0 
a  R12         -0.32249E-11   0.85691E-01          0          0 
a  R13         -0.76905E-07   0.28904E-01          0          0 
a  R23         -0.65607E-04   0.40417E-02          0          0 
a  Turb Dissipa 0.32596E+02   0.30088E+06          0          0 
a  Alphap       0.43081E-02   0.10000E+01          2          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.10000E+00  0.72285E-06  0.10000E+00  
Courant max  0.11174E-01  0.10000E+00  0.99997E+00  0.10000E+00  
Fourier min  0.84676E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Fourier max  0.18234E+06  0.10000E+00  0.22047E-05  0.10000E+00  
Cou_Fou min  0.84941E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Cou_Fou max  0.18234E+06  0.10000E+00  0.22047E-05  0.10000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                9:        0.12699E+02

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


 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         401         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4        1201         0.000000000E+00
Free outlet               3           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   :  0.22204E-02 0.82941E+00
   Friction velocity        uk    :  0.22204E-02 0.82941E+00
   Dimensionless distance   yplus :  0.34511E-01 0.53320E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :        401
------------------------------------------------------------




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


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

 Start writing
   End writing the dimensions                           
   End writing the options                              
   End writing the main variables                       
 End writing

   ** Writing the auxilliary restart file
      -----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
   End writing the mass fluxes                          
   End writing the boundary conditions                  
 End writing


 Time for restart files:    0.26889E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24715E-02     217   0.88114E-08   0.18389E+00 
c  VelocityX    0.11069E+03    2167   0.99566E-08   0.18941E+00 
c  VelocityY    0.88797E-03    5879   0.35793E-05   0.31486E-06 
c  VelocityZ    0.52065E+01    2165   0.99447E-08   0.41773E-03 
c  R11          0.13177E+01   10000   0.86886E-04   0.52678E+00 
c  R22          0.12137E+01   10000   0.94332E-04   0.52561E+00 
c  R33          0.12323E+01   10000   0.92905E-04   0.52578E+00 
c  R12          0.48333E-02    1517   0.99845E-08   0.42081E-04 
c  R13          0.16602E-02     228   0.92915E-08   0.21449E-05 
c  R23          0.24883E-03    1493   0.99862E-08   0.12604E-06 
c  Turb Dissipa 0.26359E+06   10000   0.18332E-06   0.25277E+08 
c  Alphap       0.49061E+04     101   0.77299E-08   0.21119E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.48821E-01   0.29816E+00         --         -- 
v  VelocityX    0.24288E-01   0.21260E+02         --         -- 
v  VelocityY   -0.23422E-02   0.15738E-02         --         -- 
v  VelocityZ    0.11413E-02   0.10000E+01         --         -- 
v  R11          0.52533E-02   0.91487E+00          0          0 
v  R22          0.66830E-10   0.23191E+00          0          0 
v  R33          0.20154E-02   0.27251E+00          0          0 
v  R12         -0.40362E-11   0.88703E-01          0          0 
v  R13         -0.74611E-07   0.30344E-01          0          0 
v  R23         -0.76392E-04   0.41156E-02          0          0 
v  Turb Dissipa 0.27593E+02   0.25102E+06          0          0 
v  Alphap       0.41300E-02   0.10000E+01          2          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  R11          0.52533E-02   0.91487E+00          0          0 
a  R22          0.66830E-10   0.23191E+00          0          0 
a  R33          0.20154E-02   0.27251E+00          0          0 
a  R12         -0.40362E-11   0.88703E-01          0          0 
a  R13         -0.74611E-07   0.30344E-01          0          0 
a  R23         -0.76392E-04   0.41156E-02          0          0 
a  Turb Dissipa 0.27593E+02   0.25102E+06          0          0 
a  Alphap       0.41300E-02   0.10000E+01          2          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.10000E+00  0.72285E-06  0.10000E+00  
Courant max  0.35965E-02  0.10000E+00  0.99997E+00  0.10000E+00  
Fourier min  0.83731E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Fourier max  0.18230E+06  0.10000E+00  0.22047E-05  0.10000E+00  
Cou_Fou min  0.83817E-03  0.10000E+00  0.48809E+00  0.10000E+00  
Cou_Fou max  0.18230E+06  0.10000E+00  0.22047E-05  0.10000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               10:        0.13021E+02

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.53700E-02
      -----------------------                                



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




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


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

 Destruction des structures et clôture du calcul


Bilan des temps de calcul :

  Temps CPU utilisateur :      135.970 s
  Temps CPU système :            0.290 s
  Temps CPU cumulé :           272.540 s

  Temps écoulé :               134.440 s
  Temps CPU / écoulé             1.014

Bilan de l'occupation mémoire :

  Consommation mémoire totale mesurée :           672.773 Mio
                             minimum local :      336.344 Mio  (rang 1)
                             maximum local :      336.430 Mio  (rang 0)
  Mémoire dynamique instrumentée théorique :      578.000 Kio
                             minimum local :      264.000 Kio  (rang 1)
                             maximum local :      314.000 Kio  (rang 0)
