commande : 
 /usr/local/code_saturne-3.2.2/libexec/code_saturne/cs_solver --param ebrsm_essai_1

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

                                  (R)
                      Code_Saturne

                      Version 3.2.2


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

  build mer. 30 avril 2014 10:01:43 CEST
  Version MPI 2.1 (Open MPI 1.4.3)


  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.

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



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

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


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




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


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

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

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


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

 --- 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          )


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


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

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

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

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


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

   - Commons
       ITHERM =              0 (0:  no thermal model        )
                               (10: temperature C           )
                               (11: temperature K           )
                               (20: enthalpy                )
                               (30: total energy            )
       ISCALT =             -1 (Thermal scalar number       )


 ** 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)     )

   - Rij-epsilon EBRSM     (ITURB = 32)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       IRIJNU =              0 (Matrix stabilization        )
       IRIJRB =              0 (Reconstruct at boundaries   )
       IGRARI =              0 (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.                  )
       CSRIJ  =    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                  )
       SIGMAE =    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 =              2 (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-01 (Minimum time step           )
       DTMAX  =    0.10000E+03 (Maximum time step           )
       DTREF  =    0.10000E+00 (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
 Dissip                1  0.1000E+01
 alpha                 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
 Dissip                1      1      1      1      0 0.00E+00 0.10E+01
 alpha                 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
    ------
       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-03  0.0000E+00
 VelocityX           100      1  0.1000E-04  0.1000E-03  0.0000E+00
 VelocityY           100      1  0.1000E-04  0.1000E-03  0.0000E+00
 VelocityZ           100      1  0.1000E-04  0.1000E-03  0.0000E+00
 R11                 100      1  0.1000E-04  0.1000E-03  0.0000E+00
 R22                 100      1  0.1000E-04  0.1000E-03  0.0000E+00
 R33                 100      1  0.1000E-04  0.1000E-03  0.0000E+00
 R12                 100      1  0.1000E-04  0.1000E-03  0.0000E+00
 R13                 100      1  0.1000E-04  0.1000E-03  0.0000E+00
 R23                 100      1  0.1000E-04  0.1000E-03  0.0000E+00
 Dissip              100      1  0.1000E-04  0.1000E-03  0.0000E+00
 alpha               100      1  0.1000E-04  0.1000E-03  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
 Dissip                1     -1  0.1500E+01
 alpha                 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              0  10000  0.1000E-04      1
 VelocityX            -1  10000  0.1000E-04      1
 VelocityY            -1  10000  0.1000E-04      1
 VelocityZ            -1  10000  0.1000E-04      1
 R11                  -1  10000  0.1000E-04      1
 R22                  -1  10000  0.1000E-04      1
 R33                  -1  10000  0.1000E-04      1
 R12                  -1  10000  0.1000E-04      1
 R13                  -1  10000  0.1000E-04      1
 R23                  -1  10000  0.1000E-04      1
 Dissip               -1  10000  0.1000E-04      1
 alpha                -1  10000  0.1000E-04      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
 Dissip                0    100     10
 alpha                 0    100     10
------------------------------

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


  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 =             20 (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 Dissip          
        13 alpha           
        16 TurbVisc        
        17 CourantNb       
        18 FourierNb       
        19 total_pressure  
        20 LocalTime       
         --           --

 --- 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 Dissip                        -1
        13 alpha                         -1
        14 Density                       -1
        15 LamVisc                       -1
        16 TurbVisc                      -1
        17 CourantNb                     -1
        18 FourierNb                     -1
        19 total_pressure                -1
        20 LocalTime                     -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 Dissip                         0
        13 alpha                          0
        16 TurbVisc                    -999
        17 CourantNb                   -999
        18 FourierNb                   -999
        19 total_pressure              -999
        20 LocalTime                   -999
         --           --                --

 --- Additional post-processing variables (ipstdv)
       ipstfo =              1 (Force exerted  at boundary)
       ipstyp =              1 (Yplus          at boundary)
       ipstft =              1 (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)


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


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

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


 Lecture du fichier :  mesh_input
 Fin de la lecture :  mesh_input

 Nombre de cellules :                                  90000

 ----------------------------------------------------------
 Nombre de cellules + cellules halo :                  90000


 ----------------------------------------------------------
 Nombre de faces internes :                            179375

 ----------------------------------------------------------
 Nombre de faces de bord :                             181250

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

 Histogramme du nombre de faces internes par cellule :

    valeur minimale =                2
    valeur maximale =                4

      1 : [          2 ;          3 [ =          4
      2 : [          3 ;          4 ] =      89996

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

 Renumérotation du maillage:

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

 Largeur de bande de la matrice pour maillage volumique :        400
 Profil/lignes de la matrice pour les maillage volumique :       400

 Coordonnées du maillage         minimale    et maximale
                       X :  0.0000000e+00  3.7000000e+00
                       Y :  0.0000000e+00  5.0000000e-01
                       Z :  0.0000000e+00  1.0000000e-02
 Maillage
     Nombre de cellules :       90000
     Nombre de faces internes : 179375
     Nombre de faces de bord :  181250
     Nombre de sommets :        181252

 Groupes :
    "bottom"
       faces de bord :              400
    "inlet"
       faces de bord :              225
    "outlet"
       faces de bord :              225
    "sym"
       faces de bord :           180000
    "top"
       faces de bord :              400

 --- Information sur les volumes
       Volume de controle minimal =  1.0211422e-09
       Volume de controle maximal =  1.3708555e-06
       Volume total du domaine    =  1.4800020e-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 %

 Computing geometric quantities (0.243 s)
                                                             
       ALMAX  =    0.24587E+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         0.0000E+00  0.0000E+00
  VelocityY         0.0000E+00  0.0000E+00
  VelocityZ         0.0000E+00  0.0000E+00
  R11               0.4000E-03  0.4000E-03
  R22               0.4000E-03  0.4000E-03
  R33               0.4000E-03  0.4000E-03
  R12               0.0000E+00  0.0000E+00
  R13               0.0000E+00  0.0000E+00
  R23               0.0000E+00  0.0000E+00
  Dissip            0.5380E-05  0.5380E-05
  alpha             0.0000E+00  0.0000E+00
 ---------------------------------

  LocalTime         0.1000E+00  0.1000E+00
 ---------------------------------



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

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



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



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


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




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


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


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1179E+01  0.1179E+01
  LamVisc           0.1830E-04  0.1830E-04
  TurbVisc          0.7098E-02  0.7098E-02
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         225
Smooth wall               5         800
Rough wall                6           0
Symmetry                  4      180000
Free outlet               3         225
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.37000E+01   0.91990E-05   0.50000E-02



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225         0.000000000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.00000E+00 0.00000E+00
   Friction velocity        uk    :  0.00000E+00 0.00000E+00
   Dimensionless distance   yplus :  0.00000E+00 0.00000E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27463E-01    1157   0.18117E-01   0.99999E+00 
c  VelocityX    0.50515E-02    2001   0.12553E-02   0.18396E+06 
c  VelocityY    0.50515E-02    2001   0.12553E-02   0.20170E+04 
c  VelocityZ    0.50515E-02    2001   0.12553E-02   0.53592E-21 
c  R11          0.25655E+00    9963   0.40128E-04   0.14740E+03 
c  R22          0.25654E+00    9963   0.40127E-04   0.14738E+03 
c  R33          0.25654E+00    9963   0.40127E-04   0.14738E+03 
c  R12          0.60478E-11    8709   0.57125E-04   0.76649E-20 
c  R13          0.47241E-20       0   0.00000E+00   0.00000E+00 
c  R23          0.10099E-28       0   0.00000E+00   0.00000E+00 
c  Dissip       0.11318E+04    9022   0.99960E-05   0.29317E+06 
c  alpha        0.13165E+00     484   0.21519E-03   0.20446E+01 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11      
a  R22      
a  R33      
a  R12      
a  R13      
a  R23      
a  Dissip   
a  alpha    
a  LocalTime      1.0712e-07                         74687


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                5.6547           13474          6593.2          6633.4
v  Velocity[x]             17.747          221.92          37.632          62.071
v  Velocity[y]            -22.454          48.744         0.41442          1.2548
v  Velocity[z]        -2.5521e-11      2.6418e-11      5.2951e-15      1.5492e-14
v  R11                 3.6647e-07          6.1979         0.47218          1.4575
v  R22                 3.6647e-07          6.1972         0.47215          1.4574
v  R33                 3.6647e-07          6.1972         0.47215          1.4574
v  R12                -5.0269e-10      7.8331e-11       1.393e-12     -8.9568e-13
v  R13                          0               0               0               0
v  R23                          0               0               0               0
v  Dissip                0.029322           611.1           156.3          49.895
v  alpha               7.0854e-06         0.98458        0.060411         0.14479
v  TurbVisc             0.0070982       0.0070982       0.0070982       0.0070982
v  CourantNb                    0               0               0               0
v  FourierNb                   10       9.335e+05           45586          713.66
v  total_pressure      1.0133e+05       1.148e+05      1.0792e+05      1.0796e+05
v  LocalTime                 0.01         0.10216        0.012691        0.023669


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier              10       9.335e+05           45586          713.66


 TIME FOR THE TIME STEP                1:        0.52296E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294652193E+00
Free inlet               13           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   :  0.28664E+00 0.11333E+02
   Friction velocity        uk    :  0.28664E+00 0.11333E+02
   Dimensionless distance   yplus :  0.32969E+01 0.25125E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25819E-01    1248   0.46575E-02   0.99995E+00 
c  VelocityX    0.20608E+01    1018   0.30342E-01   0.15639E+05 
c  VelocityY    0.20608E+01    1018   0.30342E-01   0.18892E+04 
c  VelocityZ    0.20608E+01    1018   0.30342E-01   0.15204E-20 
c  R11          0.33450E+00   10000   0.22800E-03   0.13459E+03 
c  R22          0.33325E+00   10000   0.22038E-03   0.10794E+03 
c  R33          0.31386E+00   10000   0.66528E-04   0.66129E+02 
c  R12          0.47282E+00    3024   0.48596E-03   0.12807E+03 
c  R13          0.69127E-13       0   0.00000E+00   0.00000E+00 
c  R23          0.57684E-13       0   0.00000E+00   0.00000E+00 
c  Dissip       0.12244E+02   10000   0.13484E-03   0.19365E+06 
c  alpha        0.10574E+02     285   0.28335E-04   0.71149E+02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11                -3.761                           158
a  R22               -7.0572                           283
a  R33      
a  R12               -3.8881                          7111
a  R13      
a  R23      
a  Dissip   
a  alpha                              1.0001                       15343
a  LocalTime      7.2205e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1024.6          2543.5           601.4           677.2
v  Velocity[x]            -6.6967          148.91          41.096          62.484
v  Velocity[y]            -13.862          20.942         0.50624          1.5633
v  Velocity[z]        -1.2109e-11      1.2524e-11      2.8633e-15      8.5025e-15
v  R11                      1e-24          9.3328         0.81902          1.8611
v  R22                      1e-24          7.2259         0.70994          1.9543
v  R33                 4.5808e-07          6.7686          0.7784          1.9019
v  R12                    -2.6542          4.5612        -0.15763        -0.63219
v  R13                          0               0               0               0
v  R23                          0               0               0               0
v  Dissip                0.058246           20485           41.47          44.921
v  alpha                0.0060991               1         0.89341         0.97402
v  TurbVisc            1.0394e-16        0.071523        0.003732        0.012133
v  CourantNb               19.614          238.32          44.462          70.807
v  FourierNb             0.022684      1.3849e+05          381.08          32.456
v  total_pressure       1.003e+05      1.0387e+05      1.0193e+05        1.02e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          19.647      1.3859e+05          425.54          103.26


 TIME FOR THE TIME STEP                2:        0.43585E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294642360E+00
Free inlet               13           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   :  0.27680E+00 0.68244E+01
   Friction velocity        uk    :  0.27680E+00 0.68244E+01
   Dimensionless distance   yplus :  0.12048E+00 0.24817E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13658E-01    1068   0.25112E-02   0.36556E+00 
c  VelocityX    0.20472E+01     671   0.22852E-01   0.71566E+04 
c  VelocityY    0.20472E+01     671   0.22852E-01   0.34421E+03 
c  VelocityZ    0.20472E+01     671   0.22852E-01   0.12065E-21 
c  R11          0.67431E+00    7816   0.61018E-01   0.40836E+03 
c  R22          0.41272E+00    8221   0.30211E-01   0.60547E+02 
c  R33          0.38475E+00    8272   0.22389E-01   0.72390E+02 
c  R12          0.74161E+00   10000   0.58330E-01   0.55895E+02 
c  R13          0.89939E-07     868   0.29347E-02   0.37345E-12 
c  R23          0.15499E-07    1001   0.32035E-02   0.11409E-12 
c  Dissip       0.47103E+03   10000   0.33776E-01   0.38328E+08 
c  alpha        0.51723E+01     255   0.28915E-04   0.35123E+00 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11      
a  R22      
a  R33      
a  R12                -15.74                          1386
a  R13      
a  R23      
a  Dissip   
a  alpha                                   1                       11982
a  LocalTime      6.8503e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                 -1699          2255.9          221.29          328.46
v  Velocity[x]            -8.1343          143.75          44.708          62.509
v  Velocity[y]            -11.843          18.647         0.57964          1.8371
v  Velocity[z]        -4.2197e-12      4.6384e-12      6.1013e-16     -1.6511e-15
v  R11                 3.8173e-07          15.988           1.449          3.3003
v  R22                 1.1431e-14          7.1779          1.0036          2.4483
v  R33                 3.8173e-07          6.8394          1.1845          2.5387
v  R12                     -6.124          8.2517        -0.30112        -0.74639
v  R13                -5.7133e-06      9.8607e-06      5.7409e-09      2.0194e-09
v  R23                -5.7795e-06      1.7004e-06     -3.8478e-09     -7.1673e-10
v  Dissip                 0.12134      5.0185e+05          431.02          173.13
v  alpha                0.0050962               1         0.83762         0.95998
v  TurbVisc            1.2376e-14         0.10203        0.006998        0.020466
v  CourantNb              0.17733          193.84          48.148          70.796
v  FourierNb               0.0184      1.4598e+05          714.26           59.87
v  total_pressure           99626      1.0358e+05      1.0155e+05      1.0165e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          14.612      1.4615e+05          762.41          130.67


 TIME FOR THE TIME STEP                3:        0.44129E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294637765E+00
Free inlet               13           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   :  0.99952E-01 0.47096E+01
   Friction velocity        uk    :  0.99952E-01 0.47096E+01
   Dimensionless distance   yplus :  0.56252E-01 0.26103E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.12063E-01     906   0.12522E-02   0.30012E+00 
c  VelocityX    0.20283E+01     495   0.34109E-01   0.34973E+04 
c  VelocityY    0.20283E+01     495   0.34109E-01   0.74806E+02 
c  VelocityZ    0.20283E+01     495   0.34109E-01   0.26801E-13 
c  R11          0.10063E+01     791   0.49736E-02   0.17592E+03 
c  R22          0.53917E+00     806   0.27325E-02   0.86776E+02 
c  R33          0.60206E+00     934   0.29074E-02   0.76004E+02 
c  R12          0.67446E+00     866   0.44148E-02   0.40964E+02 
c  R13          0.35348E-09     761   0.51673E+00   0.35248E-12 
c  R23          0.11720E-09     794   0.30463E+00   0.10436E-12 
c  Dissip       0.90383E+03    2032   0.94354E-01   0.78225E+09 
c  alpha        0.49528E+02     155   0.10789E-04   0.16234E+01 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -10.483                           146
a  R22               -2.9318                            39
a  R33                  -3.9                           134
a  R12               -8.6308                           412
a  R13           -7.0455e-08                           132
a  R23           -1.1909e-07                            22
a  Dissip            -353.82                             3
a  alpha                              1.0002                       18509
a  LocalTime      1.6646e-05                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1943.6          1848.4          51.156          169.73
v  Velocity[x]            -8.3177          140.42          48.055           62.51
v  Velocity[y]            -10.929          17.168          0.5443           1.778
v  Velocity[z]        -4.8456e-07      4.7879e-07      4.0158e-09     -9.5691e-13
v  R11                      1e-24          28.042          1.6125          3.8617
v  R22                      1e-24           7.718          1.2223          3.0445
v  R33                      1e-24          10.288          1.3094           3.071
v  R12                    -7.2053          5.6992        -0.22665        -0.62758
v  R13                -7.0455e-08      1.8626e-07       8.689e-10      2.5857e-10
v  R23                -1.1909e-07      2.0197e-08     -6.2844e-10      -1.259e-10
v  Dissip                  0.1692      1.4066e+06          1320.6          416.71
v  alpha                0.0033607               1         0.83291         0.99545
v  TurbVisc            4.3155e-14        0.086833       0.0073941        0.021739
v  CourantNb              0.10747          214.52          52.119          70.959
v  FourierNb             0.017007          6007.3          218.99          33.175
v  total_pressure           99381      1.0317e+05      1.0138e+05      1.0149e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.476          6063.8          271.11          104.13


 TIME FOR THE TIME STEP                4:        0.11729E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294673258E+00
Free inlet               13           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   :  0.44366E-01 0.45322E+01
   Friction velocity        uk    :  0.44366E-01 0.45322E+01
   Dimensionless distance   yplus :  0.21860E-01 0.25800E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13850E-01     996   0.11603E-02   0.35091E+00 
c  VelocityX    0.20126E+01     479   0.29326E-01   0.27681E+04 
c  VelocityY    0.20126E+01     479   0.29326E-01   0.48483E+02 
c  VelocityZ    0.20126E+01     479   0.29326E-01   0.12467E-13 
c  R11          0.14721E+01    4140   0.79040E-03   0.70073E+02 
c  R22          0.65472E+00    4802   0.79395E-03   0.65821E+02 
c  R33          0.83685E+00    4610   0.73284E-03   0.41309E+02 
c  R12          0.41415E+00     837   0.13397E-02   0.23880E+02 
c  R13          0.17051E-03       2   0.47348E-05   0.60383E-16 
c  R23          0.59698E-05     745   0.13146E-04   0.24222E-14 
c  Dissip       0.19805E+04    1757   0.99030E-02   0.30079E+09 
c  alpha        0.30100E+03     105   0.97401E-05   0.88060E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11            4.7151e-25                            20
a  R22            4.2079e-25                            20
a  R33            4.6673e-25                            20
a  R12               -3.1375                            40
a  R13      
a  R23      
a  Dissip              -9989                          1464
a  alpha                              1.0021                       17216
a  LocalTime      1.2248e-06                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2156.8          1433.3         -132.12         -2.5548
v  Velocity[x]            -9.7046           121.2          50.282          62.507
v  Velocity[y]            -10.979          15.383         0.42151           1.406
v  Velocity[z]        -1.9401e-07      1.4535e-07       4.783e-09     -1.0641e-12
v  R11                      1e-24          28.015          1.7324          4.1179
v  R22                      1e-24          8.0483          1.5627          3.6017
v  R33                      1e-24           13.02          1.5581          3.5085
v  R12                    -3.1375          8.1214        -0.18009        -0.54216
v  R13                -5.4853e-08      1.1877e-07      8.5576e-10      2.5014e-10
v  R23                -1.2709e-07      3.4003e-07      1.6874e-10      -6.823e-11
v  Dissip                 0.06068       1.101e+06          868.52          611.12
v  alpha                0.0026612               1         0.81908         0.99559
v  TurbVisc            1.9495e-52        0.086952        0.010675        0.027986
v  CourantNb             0.020651          206.22          55.795           70.73
v  FourierNb             0.015228           81647          297.19          56.344
v  total_pressure           99168      1.0276e+05      1.0119e+05      1.0132e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          19.356           81767          352.98          127.07


 TIME FOR THE TIME STEP                5:        0.19499E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294672356E+00
Free inlet               13           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   :  0.84086E-01 0.40784E+01
   Friction velocity        uk    :  0.84086E-01 0.40784E+01
   Dimensionless distance   yplus :  0.41158E-01 0.23971E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.12613E-01    1032   0.16050E-02   0.33499E+00 
c  VelocityX    0.19971E+01     510   0.18428E-01   0.19577E+04 
c  VelocityY    0.19971E+01     510   0.18428E-01   0.66771E+02 
c  VelocityZ    0.19971E+01     510   0.18428E-01   0.13535E-13 
c  R11          0.12502E+01   10000   0.43835E-02   0.68217E+02 
c  R22          0.60664E+00   10000   0.91098E-02   0.51080E+02 
c  R33          0.74892E+00   10000   0.71879E-02   0.28556E+02 
c  R12          0.33528E+00   10000   0.12349E-02   0.17115E+02 
c  R13          0.58491E-05    3692   0.13277E-04   0.19401E-14 
c  R23          0.20017E-06   10000   0.41410E-03   0.17653E-13 
c  Dissip       0.11725E+04   10000   0.28513E-02   0.47895E+09 
c  alpha        0.39953E+03      88   0.98824E-05   0.43562E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11            4.5638e-25                            19
a  R22            3.7455e-25                            19
a  R33            4.5574e-25                            19
a  R12               -3.5173                           293
a  R13      
a  R23      
a  Dissip             -34686                           684
a  alpha                              1.0007                       12135
a  LocalTime      1.3677e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2406.4          1023.6         -376.51         -235.24
v  Velocity[x]            -18.146          94.617           51.42          62.504
v  Velocity[y]            -11.627           14.01         0.29159         0.96798
v  Velocity[z]        -9.4265e-08      8.4507e-08      4.1059e-09      9.8586e-13
v  R11                      1e-24          36.835          1.9289          4.2394
v  R22                      1e-24          9.8895          1.9539           4.068
v  R33                      1e-24          16.549          1.8676          3.8321
v  R12                    -3.3937          9.8463        -0.18564        -0.39852
v  R13                -4.5956e-07      3.5987e-07      5.8495e-10      1.2924e-10
v  R23                -1.1887e-06       1.572e-06      1.8625e-09      2.8221e-10
v  Dissip                 0.10802       7.211e+05          225.18          483.94
v  alpha                0.0023574               1         0.80607         0.99478
v  TurbVisc            1.5203e-52          3.5113        0.015438        0.034504
v  CourantNb             0.019171           218.6          58.096          70.001
v  FourierNb             0.012764      7.3117e+06          1652.7          151.26
v  total_pressure           98919      1.0235e+05      1.0095e+05      1.0109e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          32.289      7.3118e+06          1710.8          221.26


 TIME FOR THE TIME STEP                6:        0.57067E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294672124E+00
Free inlet               13           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   :  0.68683E-01 0.36840E+01
   Friction velocity        uk    :  0.68683E-01 0.36840E+01
   Dimensionless distance   yplus :  0.38740E-01 0.21179E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.10694E-01    1032   0.15418E-02   0.30711E+00 
c  VelocityX    0.19844E+01     531   0.11607E-01   0.10733E+04 
c  VelocityY    0.19844E+01     531   0.11607E-01   0.53133E+02 
c  VelocityZ    0.19844E+01     531   0.11607E-01   0.11074E-13 
c  R11          0.14040E+01   10000   0.18683E-01   0.63591E+02 
c  R22          0.58597E+00   10000   0.38089E-01   0.37038E+02 
c  R33          0.77901E+00   10000   0.28565E-01   0.24279E+02 
c  R12          0.35792E+00   10000   0.23460E-01   0.12417E+02 
c  R13          0.78567E-06    4683   0.71403E-04   0.19467E-14 
c  R23          0.38923E-07   10000   0.18205E-01   0.31793E-13 
c  Dissip       0.95288E+03   10000   0.11609E-01   0.41694E+08 
c  alpha        0.28361E+03     121   0.96344E-05   0.15033E-01 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11                -1.598                           208
a  R22              -0.12439                           109
a  R33            4.3914e-25                            19
a  R12                -6.675                           446
a  R13           -2.2589e-07                           189
a  R23           -1.6216e-06                            90
a  Dissip            -1190.5                           270
a  alpha                              1.0003                       10081
a  LocalTime      1.0266e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2609.1          704.52         -595.47         -445.78
v  Velocity[x]            -28.807          90.588          51.903          62.501
v  Velocity[y]            -12.404          12.836         0.19506         0.61929
v  Velocity[z]        -3.9398e-07      1.6057e-07      2.2788e-10      1.1698e-11
v  R11                      1e-24          45.681          2.1376          4.3901
v  R22                      1e-24          12.314          2.2315          4.4365
v  R33                      1e-24          20.579          2.1124           4.103
v  R12                    -5.3935          11.426        -0.20137        -0.26288
v  R13                -2.2589e-07      2.3436e-07      2.8041e-10      2.3973e-11
v  R23                -1.6216e-06      5.0699e-07     -2.7169e-09     -2.9447e-10
v  Dissip                0.088609      6.6089e+05          358.72          528.44
v  alpha                0.0021836               1         0.79259         0.99288
v  TurbVisc             9.295e-53          11.518         0.02031        0.040198
v  CourantNb             0.017924          227.03          59.559          69.262
v  FourierNb              0.01282      9.7412e+06          3313.7          284.55
v  total_pressure           98716      1.0203e+05      1.0073e+05      1.0088e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          41.277      9.7413e+06          3373.3          353.81


 TIME FOR THE TIME STEP                7:        0.58163E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294669359E+00
Free inlet               13           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   :  0.22492E-01 0.36852E+01
   Friction velocity        uk    :  0.22492E-01 0.36852E+01
   Dimensionless distance   yplus :  0.10167E-01 0.18447E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.94499E-02     942   0.12036E-02   0.29608E+00 
c  VelocityX    0.19761E+01     520   0.21548E-01   0.54057E+03 
c  VelocityY    0.19761E+01     520   0.21548E-01   0.29596E+02 
c  VelocityZ    0.19761E+01     520   0.21548E-01   0.13893E-13 
c  R11          0.16653E+01   10000   0.20439E-01   0.60697E+02 
c  R22          0.64316E+00   10000   0.46281E-01   0.26632E+02 
c  R33          0.89690E+00   10000   0.34212E-01   0.21638E+02 
c  R12          0.40415E+00   10000   0.29640E-01   0.84328E+01 
c  R13          0.33782E-07    9858   0.24568E-02   0.33041E-15 
c  R23          0.21664E-08   10000   0.33032E-01   0.12024E-13 
c  Dissip       0.11463E+04   10000   0.46253E-01   0.13145E+09 
c  alpha        0.25424E+03     113   0.98678E-05   0.44161E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11              -0.81559                            50
a  R22            3.7231e-25                            19
a  R33            4.3559e-25                            19
a  R12               -4.4561                           192
a  R13           -9.8695e-08                            31
a  R23      
a  Dissip            -1222.5                            78
a  alpha                              1.0047                       12149
a  LocalTime      1.3821e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                 -2738          492.37         -755.11         -601.74
v  Velocity[x]            -36.637          91.049          51.994            62.5
v  Velocity[y]            -13.081          12.671         0.13061         0.37956
v  Velocity[z]        -1.9739e-07      5.9275e-07      5.0711e-09     -2.4006e-12
v  R11                      1e-24          54.122          2.1503          4.5027
v  R22                      1e-24          14.791          2.3462          4.7197
v  R33                      1e-24          24.745          2.1855          4.3045
v  R12                    -4.4561          13.438         -0.1306        -0.14252
v  R13                -9.8695e-08       1.292e-07      4.9596e-10      2.9769e-11
v  R23                -1.3064e-07      8.4882e-08      -2.006e-09     -1.3991e-10
v  Dissip                0.073268      5.6387e+05          902.35          604.32
v  alpha                0.0020411               1         0.79354         0.99344
v  TurbVisc            7.3397e-53          2.7827        0.020431        0.044026
v  CourantNb              0.01062          229.85          60.792          68.761
v  FourierNb             0.013432      7.2355e+06          1995.6          195.92
v  total_pressure           98587      1.0182e+05      1.0057e+05      1.0072e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          46.415      7.2355e+06          2056.4          264.68


 TIME FOR THE TIME STEP                8:        0.61961E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294668565E+00
Free inlet               13           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   :  0.44932E-01 0.37174E+01
   Friction velocity        uk    :  0.44932E-01 0.37174E+01
   Dimensionless distance   yplus :  0.16451E-01 0.16878E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71483E-02     762   0.91194E-03   0.24355E+00 
c  VelocityX    0.19701E+01     451   0.17506E-01   0.29338E+03 
c  VelocityY    0.19701E+01     451   0.17506E-01   0.14140E+02 
c  VelocityZ    0.19701E+01     451   0.17506E-01   0.10700E-13 
c  R11          0.19075E+01    6599   0.19811E-02   0.53680E+02 
c  R22          0.70308E+00    7114   0.30722E-02   0.17334E+02 
c  R33          0.10100E+01    6816   0.24108E-02   0.17752E+02 
c  R12          0.45874E+00    5956   0.35773E-02   0.60375E+01 
c  R13          0.12790E-07    6634   0.53176E-02   0.93676E-14 
c  R23          0.16854E-08    8983   0.37664E-01   0.30276E-14 
c  Dissip       0.13165E+04    6362   0.89125E-02   0.74437E+08 
c  alpha        0.24209E+03     108   0.96597E-05   0.26111E-01 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11              -0.83949                           103
a  R22            3.7801e-25                            19
a  R33            4.3206e-25                            19
a  R12               -3.8422                           592
a  R13           -1.1315e-06                            84
a  R23      
a  Dissip             -13231                            46
a  alpha                              1.0013                       13149
a  LocalTime      3.7059e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2813.6          356.96         -866.76         -713.46
v  Velocity[x]            -40.295          91.911          51.721          62.499
v  Velocity[y]            -13.677          13.185        0.089708          0.2327
v  Velocity[z]        -1.2268e-07      6.7656e-07      9.4336e-09     -4.2269e-11
v  R11                      1e-24          63.103          2.1166          4.5889
v  R22                      1e-24           17.28          2.4235          4.9476
v  R33                      1e-24          29.044          2.1914          4.4563
v  R12                    -3.7042          15.412       -0.065437       -0.035173
v  R13                -1.1315e-06      4.8377e-07     -3.2258e-10     -2.2545e-10
v  R23                -8.8415e-07      1.4277e-07      1.4364e-09      1.0135e-10
v  Dissip                0.060807      5.0438e+05          607.31          639.73
v  alpha                0.0019432               1         0.81251         0.99503
v  TurbVisc            5.5085e-53        0.093424         0.02106        0.048073
v  CourantNb             0.046506          220.09          61.791          68.504
v  FourierNb             0.014096      2.6984e+05          661.22          129.99
v  total_pressure           98511      1.0168e+05      1.0046e+05      1.0061e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          36.312       2.699e+05          723.01          198.49


 TIME FOR THE TIME STEP                9:        0.44128E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294660199E+00
Free inlet               13           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   :  0.61443E-01 0.37854E+01
   Friction velocity        uk    :  0.61443E-01 0.37854E+01
   Dimensionless distance   yplus :  0.24365E-01 0.16472E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on        225


 Write intermediate 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 auxiliary 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:    0.16056E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61503E-02     834   0.78200E-03   0.22325E+00 
c  VelocityX    0.19665E+01     472   0.17937E-01   0.20071E+03 
c  VelocityY    0.19665E+01     472   0.17937E-01   0.88050E+01 
c  VelocityZ    0.19665E+01     472   0.17937E-01   0.26119E-13 
c  R11          0.21999E+01    6196   0.15704E-02   0.48660E+02 
c  R22          0.77498E+00    7387   0.26822E-02   0.11588E+02 
c  R33          0.11456E+01    6990   0.22848E-02   0.14046E+02 
c  R12          0.52685E+00    5720   0.38842E-02   0.44675E+01 
c  R13          0.58250E-08    5668   0.16377E-01   0.11138E-13 
c  R23          0.27554E-08    5627   0.25293E-01   0.21812E-14 
c  Dissip       0.15030E+04    4718   0.84192E-02   0.43978E+08 
c  alpha        0.19250E+03     102   0.99876E-05   0.12540E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11              -0.52381                           102
a  R22            3.7498e-25                            19
a  R33            4.2925e-25                            19
a  R12               -3.3888                           604
a  R13           -3.9891e-07                            83
a  R23      
a  Dissip            -5590.8                           789
a  alpha                              1.0011                       12217
a  LocalTime      4.5822e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2858.8          267.82         -947.43         -796.07
v  Velocity[x]            -41.226          92.889          51.206          62.497
v  Velocity[y]            -14.263          13.751        0.067361         0.16066
v  Velocity[z]         -5.978e-07      3.7359e-07      4.2289e-09     -2.4243e-11
v  R11                      1e-24          72.222          2.1284          4.6657
v  R22                      1e-24          19.784          2.5399          5.1317
v  R33                      1e-24          33.426          2.2551           4.581
v  R12                    -3.3888          17.329        -0.06584         0.05696
v  R13                -3.9891e-07      3.3272e-07     -9.7564e-10     -8.6726e-11
v  R23                -2.9084e-07      5.6626e-07      3.0899e-09      1.1147e-10
v  Dissip                0.050364      4.1961e+05          542.93           704.2
v  alpha                0.0018477               1         0.80912         0.99489
v  TurbVisc            4.1787e-53         0.26898         0.02332        0.052168
v  CourantNb             0.038377          204.61          62.342          68.426
v  FourierNb             0.014096      2.1823e+06          756.66          150.78
v  total_pressure           98466      1.0159e+05      1.0038e+05      1.0053e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          24.821      2.1824e+06             819          219.21


 TIME FOR THE TIME STEP               10:        0.39756E+02

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


 INSTANT    0.110000000E+01   TIME STEP NUMBER              11
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294643325E+00
Free inlet               13           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   :  0.97151E-01 0.36941E+01
   Friction velocity        uk    :  0.97151E-01 0.36941E+01
   Dimensionless distance   yplus :  0.35499E-01 0.16448E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.50897E-02     816   0.72553E-03   0.19111E+00 
c  VelocityX    0.19642E+01     418   0.13638E-01   0.16309E+03 
c  VelocityY    0.19642E+01     418   0.13638E-01   0.76087E+01 
c  VelocityZ    0.19642E+01     418   0.13638E-01   0.31479E-13 
c  R11          0.25489E+01   10000   0.12098E+00   0.49011E+02 
c  R22          0.90186E+00   10000   0.34319E+00   0.87654E+01 
c  R33          0.13230E+01   10000   0.18907E+00   0.12903E+02 
c  R12          0.84739E+00   10000   0.78161E+00   0.38539E+01 
c  R13          0.43957E-07   10000   0.62715E+00   0.36949E-13 
c  R23          0.33857E-07   10000   0.67774E+00   0.69331E-13 
c  Dissip       0.17549E+04   10000   0.24636E-01   0.47788E+08 
c  alpha        0.16182E+03     120   0.99768E-05   0.36776E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -1.4235                           282
a  R22             -0.035951                            22
a  R33            4.2732e-25                            19
a  R12               -4.1761                           595
a  R13           -1.2373e-06                           263
a  R23           -1.3457e-06                             3
a  Dissip             -17747                          1666
a  alpha                              1.0004                        9279
a  LocalTime      4.4091e-09                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2884.8           210.3         -1005.1         -855.99
v  Velocity[x]            -41.074          93.928          50.662          62.497
v  Velocity[y]            -14.884          14.325        0.059609         0.14249
v  Velocity[z]        -1.5177e-06      7.2036e-07     -5.4469e-09      8.2801e-11
v  R11                      1e-24           81.06          2.1995          4.7427
v  R22                      1e-24          22.244          2.6401          5.2739
v  R33                      1e-24          37.778          2.3423          4.6835
v  R12                    -3.2475          19.178       -0.079761         0.13655
v  R13                -1.2373e-06      1.9177e-06     -1.4861e-09      2.3699e-10
v  R23                -1.3457e-06       2.858e-06      7.3546e-09      5.4152e-10
v  Dissip                0.002524      3.6947e+05          602.04          801.09
v  alpha                 0.001743               1         0.80278         0.99422
v  TurbVisc            3.2355e-53          11.215        0.025938        0.055369
v  CourantNb             0.018751          263.69          62.494          68.479
v  FourierNb             0.014096      2.2681e+07          2872.8          267.18
v  total_pressure           98440      1.0154e+05      1.0032e+05      1.0047e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          19.239      2.2681e+07          2935.3          335.66


 TIME FOR THE TIME STEP               11:        0.61313E+02

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


 INSTANT    0.120000000E+01   TIME STEP NUMBER              12
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294642571E+00
Free inlet               13           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   :  0.28995E-01 0.36363E+01
   Friction velocity        uk    :  0.28995E-01 0.36363E+01
   Dimensionless distance   yplus :  0.10517E-01 0.16608E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.47311E-02     762   0.67301E-03   0.17615E+00 
c  VelocityX    0.19629E+01     449   0.98293E-02   0.14125E+03 
c  VelocityY    0.19629E+01     449   0.98293E-02   0.69616E+01 
c  VelocityZ    0.19629E+01     449   0.98293E-02   0.16610E-12 
c  R11          0.29050E+01   10000   0.69686E-02   0.54374E+02 
c  R22          0.97143E+00   10000   0.31149E-01   0.81490E+01 
c  R33          0.14876E+01   10000   0.20623E-01   0.14239E+02 
c  R12          0.69245E+00   10000   0.22418E-01   0.39199E+01 
c  R13          0.10086E-08   10000   0.58817E+00   0.38849E-13 
c  R23          0.30107E-08   10000   0.67100E+00   0.64847E-13 
c  Dissip       0.20328E+04   10000   0.38261E-02   0.53693E+08 
c  alpha        0.14173E+03     114   0.93885E-05   0.58440E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11            4.2607e-25                            19
a  R22            3.8079e-25                            19
a  R33            4.2602e-25                            19
a  R12               -4.3026                           138
a  R13      
a  R23      
a  Dissip   
a  alpha                               1.001                       11376
a  LocalTime      2.5358e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2896.6          175.74         -1044.1         -896.64
v  Velocity[x]            -41.145          95.033          50.092          62.498
v  Velocity[y]             -15.56          14.918        0.060626         0.15291
v  Velocity[z]        -1.6259e-06      9.3084e-07     -2.1539e-08      2.0733e-10
v  R11                      1e-24          89.914          2.1944          4.8239
v  R22                      1e-24          24.566          2.6093          5.3716
v  R33                      1e-24          42.016          2.3103          4.7548
v  R12                    -4.3026          20.919       -0.075119         0.21356
v  R13                -3.1928e-07      5.9739e-07      1.0742e-09      1.3079e-11
v  R23                -9.2491e-07      1.8337e-07     -3.1864e-09     -9.5151e-12
v  Dissip                 0.03475      3.3356e+05          655.11          894.17
v  alpha                0.0016933               1         0.79804         0.99425
v  TurbVisc            2.7385e-53          9.7718        0.024198         0.05624
v  CourantNb             0.014244          325.14          62.531          68.583
v  FourierNb             0.014211      3.9435e+06          1030.6           168.2
v  total_pressure           98428       1.015e+05      1.0028e+05      1.0043e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          15.101      3.9436e+06          1093.2          236.79


 TIME FOR THE TIME STEP               12:        0.61330E+02

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


 INSTANT    0.130000000E+01   TIME STEP NUMBER              13
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294642053E+00
Free inlet               13           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   :  0.31586E-01 0.36267E+01
   Friction velocity        uk    :  0.31586E-01 0.36267E+01
   Dimensionless distance   yplus :  0.11313E-01 0.17050E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.38087E-02     672   0.63194E-03   0.13926E+00 
c  VelocityX    0.19624E+01     451   0.12668E-01   0.12299E+03 
c  VelocityY    0.19624E+01     451   0.12668E-01   0.63584E+01 
c  VelocityZ    0.19624E+01     451   0.12668E-01   0.31752E-12 
c  R11          0.33143E+01    5156   0.11240E-02   0.62352E+02 
c  R22          0.10890E+01    6409   0.23546E-02   0.81247E+01 
c  R33          0.16880E+01    6052   0.16403E-02   0.15843E+02 
c  R12          0.78999E+00    4105   0.27898E-02   0.43573E+01 
c  R13          0.29274E-08    5238   0.17396E+00   0.89675E-14 
c  R23          0.19344E-08    5935   0.17461E+00   0.25135E-13 
c  Dissip       0.23498E+04    1863   0.35771E-02   0.66565E+08 
c  alpha        0.12329E+03     118   0.97757E-05   0.49620E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -2.9804                           364
a  R22              -0.13214                            85
a  R33             -0.056256                            34
a  R12               -4.3387                           408
a  R13           -1.1266e-06                           345
a  R23           -1.1731e-06                            67
a  Dissip            -7204.5                           642
a  alpha                              1.0011                       13443
a  LocalTime      5.0256e-06                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2895.1          161.09         -1065.6         -919.09
v  Velocity[x]            -41.399          96.225          49.462          62.499
v  Velocity[y]            -16.301          15.541        0.065213         0.17259
v  Velocity[z]        -2.9856e-06      4.2282e-06     -7.8467e-09      5.5817e-11
v  R11                      1e-24          98.367          2.1793          4.9544
v  R22                      1e-24          26.762          2.6104          5.4718
v  R33                      1e-24          46.153          2.2999          4.8411
v  R12                    -4.3387          22.537       -0.035275         0.28925
v  R13                -6.8453e-07      2.5017e-07     -7.3147e-10     -7.2802e-11
v  R23                -1.1731e-06       9.666e-07     -6.8485e-09     -2.3515e-10
v  Dissip                0.028941      3.0671e+05          692.86            1000
v  alpha                0.0016336               1         0.81097         0.99484
v  TurbVisc            2.3608e-53        0.086846        0.024172        0.057423
v  CourantNb             0.010627          393.85          62.663          68.718
v  FourierNb             0.014852           19898          554.96          136.11
v  total_pressure           98430      1.0149e+05      1.0026e+05      1.0041e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           14.74           20092          617.63          204.83


 TIME FOR THE TIME STEP               13:        0.33173E+02

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


 INSTANT    0.140000000E+01   TIME STEP NUMBER              14
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294642350E+00
Free inlet               13           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   :  0.66374E-01 0.36410E+01
   Friction velocity        uk    :  0.66374E-01 0.36410E+01
   Dimensionless distance   yplus :  0.23597E-01 0.17460E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.38818E-02     492   0.61212E-03   0.14020E+00 
c  VelocityX    0.19623E+01     472   0.12367E-01   0.10988E+03 
c  VelocityY    0.19623E+01     472   0.12367E-01   0.62950E+01 
c  VelocityZ    0.19623E+01     472   0.12367E-01   0.23583E-12 
c  R11          0.37680E+01    3964   0.16788E-02   0.71924E+02 
c  R22          0.12236E+01    5053   0.16169E-02   0.92109E+01 
c  R33          0.19126E+01    4692   0.13525E-02   0.18332E+02 
c  R12          0.89867E+00    3280   0.26294E-02   0.50261E+01 
c  R13          0.44169E-04     295   0.16598E-04   0.31494E-12 
c  R23          0.23904E-06    4054   0.54505E-02   0.39519E-13 
c  Dissip       0.27147E+04    4467   0.43457E-02   0.82836E+08 
c  alpha        0.11085E+03     111   0.95299E-05   0.70125E-03 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -1.2455                           230
a  R22            2.2168e-25                            33
a  R33            4.2398e-25                            33
a  R12               -3.6683                           479
a  R13           -3.2534e-06                           197
a  R23      
a  Dissip            -4980.9                          1595
a  alpha                              1.0013                       10517
a  LocalTime       5.864e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2881.7          163.26         -1072.1          -925.8
v  Velocity[x]            -42.819          97.528          48.708          62.499
v  Velocity[y]            -17.107           16.14        0.070204         0.19195
v  Velocity[z]        -3.0775e-06      4.7614e-06      1.5426e-08     -2.5519e-10
v  R11                      1e-24           106.6          2.2086          5.1287
v  R22                      1e-24           28.82          2.6631          5.5815
v  R33                      1e-24          50.044           2.339          4.9452
v  R12                    -3.6683          23.987       -0.021793         0.36313
v  R13                -3.2534e-06       6.398e-06      2.5162e-09      1.3254e-09
v  R23                -1.2767e-06      8.2011e-07     -1.2184e-08     -1.0813e-09
v  Dissip                0.011454      3.2317e+05          655.67          1118.6
v  alpha                0.0015591               1         0.80577          0.9946
v  TurbVisc             2.015e-53         0.14184        0.024924        0.058324
v  CourantNb             0.012215          461.95          62.894          68.856
v  FourierNb             0.014852      1.7053e+05          656.57          149.31
v  total_pressure           98443      1.0149e+05      1.0025e+05       1.004e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.629      1.7059e+05          719.46          218.16


 TIME FOR THE TIME STEP               14:        0.25883E+02

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


 INSTANT    0.150000000E+01   TIME STEP NUMBER              15
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294643209E+00
Free inlet               13           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   :  0.69806E-01 0.36593E+01
   Friction velocity        uk    :  0.69806E-01 0.36593E+01
   Dimensionless distance   yplus :  0.40607E-01 0.17664E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.39230E-02     438   0.60804E-03   0.13958E+00 
c  VelocityX    0.19626E+01     464   0.11982E-01   0.10896E+03 
c  VelocityY    0.19626E+01     464   0.11982E-01   0.69433E+01 
c  VelocityZ    0.19626E+01     464   0.11982E-01   0.11411E-11 
c  R11          0.42665E+01   10000   0.18103E-02   0.83885E+02 
c  R22          0.13749E+01   10000   0.49752E-02   0.10910E+02 
c  R33          0.21610E+01   10000   0.31061E-02   0.21664E+02 
c  R12          0.10193E+01   10000   0.49226E-02   0.59930E+01 
c  R13          0.81166E-06    6337   0.29016E-02   0.37682E-12 
c  R23          0.42900E-07    9044   0.83864E-01   0.15564E-12 
c  Dissip       0.31240E+04   10000   0.20309E-02   0.96974E+08 
c  alpha        0.10086E+03     119   0.99822E-05   0.48779E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -0.3808                            70
a  R22            1.4609e-25                            28
a  R33            4.2339e-25                            22
a  R12               -3.5911                           178
a  R13           -1.3747e-06                            47
a  R23      
a  Dissip            -2348.4                           160
a  alpha                              1.0005                        8376
a  LocalTime      2.8292e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2858.7          179.16           -1067          -920.2
v  Velocity[x]            -44.447          98.925          47.981          62.499
v  Velocity[y]            -17.971           16.71        0.074156         0.20741
v  Velocity[z]        -2.2929e-06      5.0066e-06      3.9884e-08     -5.2338e-10
v  R11                      1e-24          114.29           2.333          5.3447
v  R22                      1e-24          30.714          2.7423          5.7002
v  R33                      1e-24          53.792          2.4342          5.0688
v  R12                    -3.5911           25.33      -0.0094766         0.44391
v  R13                -1.3747e-06      4.1995e-06     -9.0678e-10      6.6976e-10
v  R23                -5.7813e-06      1.0723e-06      -5.911e-09     -1.7212e-09
v  Dissip                0.020109      3.4595e+05          676.08          1256.5
v  alpha                0.0014705               1         0.79443         0.99358
v  TurbVisc            1.7537e-53          5.4388        0.026727        0.059334
v  CourantNb             0.021055          527.81          63.088          68.999
v  FourierNb             0.014852      3.5346e+06          1508.2          219.92
v  total_pressure           98466       1.015e+05      1.0026e+05       1.004e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.4132      3.5346e+06          1571.3          288.92


 TIME FOR THE TIME STEP               15:        0.57401E+02

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


 INSTANT    0.160000000E+01   TIME STEP NUMBER              16
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294643032E+00
Free inlet               13           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   :  0.11052E+00 0.38865E+01
   Friction velocity        uk    :  0.11052E+00 0.38865E+01
   Dimensionless distance   yplus :  0.40685E-01 0.17812E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.45087E-02     506   0.61880E-03   0.15679E+00 
c  VelocityX    0.19631E+01     489   0.11360E-01   0.11665E+03 
c  VelocityY    0.19631E+01     489   0.11360E-01   0.79539E+01 
c  VelocityZ    0.19631E+01     489   0.11360E-01   0.16016E-12 
c  R11          0.48146E+01   10000   0.11473E-02   0.97502E+02 
c  R22          0.15442E+01   10000   0.26434E-02   0.12880E+02 
c  R33          0.24354E+01   10000   0.18435E-02   0.24959E+02 
c  R12          0.11536E+01   10000   0.21839E-02   0.73792E+01 
c  R13          0.92226E-06    5890   0.18776E-02   0.89547E-13 
c  R23          0.70522E-08   10000   0.17540E+00   0.21434E-12 
c  Dissip       0.35818E+04   10000   0.20561E-02   0.11993E+09 
c  alpha        0.93859E+02     123   0.98756E-05   0.48045E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -1.9676                           236
a  R22            1.0005e-25                            26
a  R33             4.225e-25                            19
a  R12               -4.7466                           517
a  R13           -1.7428e-06                           217
a  R23      
a  Dissip            -4525.4                          1090
a  alpha                              1.0013                       10140
a  LocalTime       2.121e-08                         89999


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2829.5          205.34         -1053.7            -906
v  Velocity[x]            -47.581          100.43          47.337            62.5
v  Velocity[y]              -18.9          17.259        0.077277          0.2199
v  Velocity[z]         -3.242e-06      5.2714e-06       3.872e-08      -5.545e-10
v  R11                      1e-24          121.64          2.3359          5.5755
v  R22                      1e-24           32.45          2.7618          5.8251
v  R33                      1e-24          57.297          2.4593          5.1977
v  R12                    -3.6187          26.493       -0.019117          0.5352
v  R13                -1.5323e-06      7.2092e-07     -4.7859e-09      -2.386e-10
v  R23                 -1.103e-06      2.1123e-06      9.8273e-09      5.5877e-10
v  Dissip                0.016844      3.5585e+05          694.26          1405.8
v  alpha                0.0014072               1         0.80267         0.99405
v  TurbVisc            1.5374e-53          2.5492        0.025967        0.059695
v  CourantNb            0.0095359          584.52          63.365          69.165
v  FourierNb             0.014852      4.7148e+06          1231.7          185.82
v  total_pressure           98495      1.0153e+05      1.0027e+05      1.0042e+05
v  LocalTime                 0.01        0.010757            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4.8646      4.7148e+06          1295.1          254.99


 TIME FOR THE TIME STEP               16:        0.58873E+02

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


 INSTANT    0.170000000E+01   TIME STEP NUMBER              17
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294654358E+00
Free inlet               13           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   :  0.98164E-01 0.41375E+01
   Friction velocity        uk    :  0.98164E-01 0.41375E+01
   Dimensionless distance   yplus :  0.34959E-01 0.18003E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.51054E-02     546   0.63478E-03   0.17280E+00 
c  VelocityX    0.19639E+01     448   0.12153E-01   0.12401E+03 
c  VelocityY    0.19639E+01     448   0.12153E-01   0.88505E+01 
c  VelocityZ    0.19639E+01     448   0.12153E-01   0.17672E-11 
c  R11          0.54168E+01   10000   0.65650E-02   0.11435E+03 
c  R22          0.17344E+01   10000   0.16970E-01   0.15774E+02 
c  R33          0.27385E+01   10000   0.10403E-01   0.29238E+02 
c  R12          0.13033E+01   10000   0.16753E-01   0.90187E+01 
c  R13          0.53123E-06   10000   0.11517E-01   0.53540E-13 
c  R23          0.21837E-07   10000   0.55356E+00   0.42428E-13 
c  Dissip       0.40951E+04   10000   0.29555E-02   0.14781E+09 
c  alpha        0.88148E+02     115   0.95046E-05   0.12860E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11            4.2197e-25                            19
a  R22            1.1862e-25                            25
a  R33             4.219e-25                            19
a  R12               -6.1153                           567
a  R13      
a  R23      
a  Dissip   
a  alpha                              1.0005                        7782
a  LocalTime      2.1458e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2798.6          237.46         -1035.9         -887.13
v  Velocity[x]            -50.282             102          46.847          62.501
v  Velocity[y]            -19.898          17.779        0.080074         0.23163
v  Velocity[z]        -6.1935e-06      3.7531e-06      -6.138e-10     -2.5283e-10
v  R11                      1e-24          128.53          2.4964          5.8516
v  R22                      1e-24          34.061          2.7837          5.9653
v  R33                      1e-24           60.62          2.5032           5.344
v  R12                    -4.3463          27.523       -0.044867         0.63425
v  R13                -2.2769e-06      1.1547e-06      2.5322e-09      1.2847e-10
v  R23                -1.4584e-06      1.7047e-06      3.5217e-10      2.4906e-10
v  Dissip                0.014324      3.3913e+05          867.41          1581.9
v  alpha                0.0013577               1          0.7967         0.99355
v  TurbVisc            1.3511e-53          31.514        0.027735        0.060802
v  CourantNb             0.015076          644.38          63.641          69.348
v  FourierNb             0.014852      4.6604e+06          2060.9          260.28
v  total_pressure           98526      1.0156e+05      1.0029e+05      1.0044e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4.2573      4.6604e+06          2124.6          329.63


 TIME FOR THE TIME STEP               17:        0.61541E+02

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


 INSTANT    0.180000000E+01   TIME STEP NUMBER              18
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294661861E+00
Free inlet               13           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   :  0.42403E-01 0.44216E+01
   Friction velocity        uk    :  0.42403E-01 0.44216E+01
   Dimensionless distance   yplus :  0.23508E-01 0.18211E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.44869E-02     546   0.64083E-03   0.14712E+00 
c  VelocityX    0.19648E+01     519   0.13419E-01   0.12343E+03 
c  VelocityY    0.19648E+01     519   0.13419E-01   0.96269E+01 
c  VelocityZ    0.19648E+01     519   0.13419E-01   0.62755E-12 
c  R11          0.60759E+01    2890   0.52392E-02   0.13390E+03 
c  R22          0.19451E+01    3354   0.67536E-02   0.20390E+02 
c  R33          0.30709E+01    3114   0.35225E-02   0.35438E+02 
c  R12          0.14692E+01    3490   0.12560E-01   0.10943E+02 
c  R13          0.44692E-06    2714   0.11313E-01   0.57538E-13 
c  R23          0.15321E-07    5114   0.40133E+00   0.17630E-12 
c  Dissip       0.46667E+04    3642   0.27115E-02   0.17892E+09 
c  alpha        0.84874E+02     128   0.99122E-05   0.94822E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -6.1623                           477
a  R22               -1.9399                           222
a  R33               -2.4301                           178
a  R12               -4.3456                           539
a  R13           -1.1831e-06                           455
a  R23           -4.1873e-06                           197
a  Dissip            -8158.4                          1398
a  alpha                              1.0011                       13937
a  LocalTime      2.8526e-06                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2768.6          272.74         -1015.9         -866.11
v  Velocity[x]            -53.042          103.67          46.478          62.501
v  Velocity[y]            -20.963           18.33         0.08304          0.2445
v  Velocity[z]        -7.2888e-06      7.9036e-06     -4.5798e-09     -2.8433e-10
v  R11                      1e-24          135.01          2.4124          6.1328
v  R22                      1e-24          35.497          2.7471          6.1185
v  R33                      1e-24          63.709          2.4398            5.49
v  R12                    -4.3456          28.443        0.028307         0.75725
v  R13                -8.9525e-07      2.4953e-06      2.8913e-09       2.131e-10
v  R23                -4.1873e-06      1.3069e-06      1.0291e-09      2.0195e-10
v  Dissip                0.012173      3.2572e+05             906          1757.9
v  alpha                0.0013328               1         0.81458         0.99474
v  TurbVisc            1.1962e-53         0.21829        0.024463        0.061213
v  CourantNb             0.013023          675.17          63.946          69.525
v  FourierNb             0.014852           35056          582.85          131.54
v  total_pressure           98556       1.016e+05      1.0031e+05      1.0046e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4.6415           35105          646.79          201.07


 TIME FOR THE TIME STEP               18:        0.25030E+02

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


 INSTANT    0.190000000E+01   TIME STEP NUMBER              19
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294663977E+00
Free inlet               13           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   :  0.95992E-01 0.46618E+01
   Friction velocity        uk    :  0.95992E-01 0.46618E+01
   Dimensionless distance   yplus :  0.51879E-01 0.18424E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.44017E-02     510   0.64562E-03   0.14149E+00 
c  VelocityX    0.19658E+01     438   0.13043E-01   0.11950E+03 
c  VelocityY    0.19658E+01     438   0.13043E-01   0.10355E+02 
c  VelocityZ    0.19658E+01     438   0.13043E-01   0.31995E-11 
c  R11          0.67954E+01    6010   0.90908E-03   0.15324E+03 
c  R22          0.21797E+01    6468   0.12679E-02   0.25428E+02 
c  R33          0.34351E+01    6434   0.81624E-03   0.40643E+02 
c  R12          0.16535E+01    6554   0.18542E-02   0.12928E+02 
c  R13          0.15616E-03     171   0.11792E-04   0.38329E-13 
c  R23          0.33252E-06    4223   0.45161E-02   0.45752E-12 
c  Dissip       0.52989E+04    6072   0.21969E-02   0.21426E+09 
c  alpha        0.82194E+02     129   0.99271E-05   0.36000E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -9.1591                           781
a  R22                -2.578                           468
a  R33                 -3.48                           472
a  R12               -4.1626                           854
a  R13           -5.7669e-06                           602
a  R23           -1.2862e-05                           338
a  Dissip             -23162                          4294
a  alpha                              1.0005                       10955
a  LocalTime      7.5598e-08                         89999


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                 -2741          308.76            -996         -845.29
v  Velocity[x]            -55.514          105.36          45.954          62.502
v  Velocity[y]            -22.113          19.991        0.086597         0.25966
v  Velocity[z]        -3.8449e-06      9.5934e-06     -3.5546e-09     -2.8413e-10
v  R11                      1e-24          141.17          2.4912           6.473
v  R22                      1e-24          36.784          2.7974          6.3185
v  R33                      1e-24          66.537          2.4728          5.6756
v  R12                    -4.1626           32.75        0.047873         0.88752
v  R13                -4.2587e-06      1.5934e-06       2.952e-09       3.328e-10
v  R23                -1.2862e-05      5.2225e-06      -3.347e-09     -1.4223e-09
v  Dissip              0.00054636      3.3559e+05           976.9          1955.2
v  alpha                0.0013049               1          0.8059         0.99435
v  TurbVisc            1.0647e-53          3.3799        0.026008        0.065245
v  CourantNb             0.009142          705.99           64.45          69.712
v  FourierNb             0.014852      1.3228e+06          834.38          159.68
v  total_pressure           98584      1.0163e+05      1.0033e+05      1.0048e+05
v  LocalTime                 0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.4931      1.3228e+06          898.83          229.39


 TIME FOR THE TIME STEP               19:        0.33814E+02

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


 INSTANT    0.200000000E+01   TIME STEP NUMBER              20
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.294655000E+00
Smooth wall               5         800         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      180000         0.000000000E+00
Free outlet               3         225         0.294665308E+00
Free inlet               13           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   :  0.93454E-01 0.47887E+01
   Friction velocity        uk    :  0.93454E-01 0.47887E+01
   Dimensionless distance   yplus :  0.33224E-01 0.18665E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        800
   Total number of wall faces                   :        800
------------------------------------------------------------




 Write final restart files
   checkpoint at iteration         20, Physical time    0.20000E+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 auxiliary 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:    0.43899E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54728E-02     492   0.65016E-03   0.17281E+00 
c  VelocityX    0.19670E+01     479   0.13270E-01   0.13168E+03 
c  VelocityY    0.19670E+01     479   0.13270E-01   0.11445E+02 
c  VelocityZ    0.19670E+01     479   0.13270E-01   0.27347E-11 
c  R11          0.75795E+01    5341   0.21123E-01   0.17638E+03 
c  R22          0.24440E+01    8992   0.67945E-01   0.32988E+02 
c  R33          0.38326E+01    7520   0.18443E-01   0.47537E+02 
c  R12          0.18629E+01    9602   0.61202E-01   0.15745E+02 
c  R13          0.28027E-03     181   0.20760E-04   0.83526E-13 
c  R23          0.20664E-05    3079   0.18368E-02   0.42289E-12 
c  Dissip       0.59907E+04    8908   0.20038E-02   0.25181E+09 
c  alpha        0.81142E+02     122   0.97509E-05   0.11877E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -2.0385                           612
a  R22              -0.23802                           451
a  R33              -0.44398                           418
a  R12               -4.1259                           459
a  R13           -1.3551e-06                           200
a  R23           -1.0398e-06                            38
a  Dissip             -13140                          1013
a  alpha                              1.0008                       10999
a  LocalTime      1.5987e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2717.4          344.28            -978         -826.48
v  Velocity[x]            -57.619          107.11          45.461          62.501
v  Velocity[y]            -23.357          21.833        0.091193         0.27816
v  Velocity[z]        -1.8349e-05      1.3766e-05     -9.9178e-09      9.3479e-11
v  R11                      1e-24          146.89           2.557          6.8541
v  R22                      1e-24          39.196          2.8714          6.5616
v  R33                      1e-24          69.166          2.5229          5.8901
v  R12                    -4.1259          37.648        0.076715          1.0386
v  R13                -1.3551e-06      5.4312e-06      6.1978e-09      4.2806e-10
v  R23                -1.0398e-06      1.3896e-06      7.4925e-10      -2.922e-10
v  Dissip               0.0085863      3.5453e+05          904.45          2163.5
v  alpha                0.0012775               1         0.80266         0.99424
v  TurbVisc            9.5197e-54          631.28        0.039942         0.14903
v  CourantNb             0.027169          708.65          64.769          69.925
v  FourierNb             0.014852      6.2551e+05          666.33          180.57
v  total_pressure           98608      1.0167e+05      1.0035e+05       1.005e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           3.036      6.2557e+05           731.1          250.49


 TIME FOR THE TIME STEP               20:        0.41303E+02

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.73010E-02
      -----------------------                                



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




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


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

 Destruction des structures et clôture du calcul


Bilan des temps de calcul :

  Temps CPU utilisateur :      889.348 s
  Temps CPU système :            0.784 s

  Temps écoulé :               892.424 s
  Temps CPU / écoulé             0.997

Bilan de l'occupation mémoire :

  Consommation mémoire totale mesurée :           435.129 Mio
  Mémoire dynamique instrumentée théorique :      100.319 Mio
