commande : 
 ./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 =             50 (Final time step required    )

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


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


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

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

 --- Post-processed variables

       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 (0.246 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     0.26639E-01    1157   0.18195E-01   0.10000E+01 
c  VelocityX    0.49031E-02    2002   0.11440E-02   0.17443E+06 
c  VelocityY    0.49031E-02    2002   0.11440E-02   0.20126E+04 
c  VelocityZ    0.49031E-02    2002   0.11440E-02   0.50294E-21 
c  R11          0.24901E+00   10000   0.37515E-04   0.14286E+03 
c  R22          0.24900E+00   10000   0.37515E-04   0.14285E+03 
c  R33          0.24900E+00   10000   0.37515E-04   0.14285E+03 
c  R12          0.38747E-11    9479   0.72996E-04   0.64342E-20 
c  R13          0.43824E-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    9025   0.99973E-05   0.29034E+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                5.5047           13141          6419.2          6457.8
v  Velocity[x]             17.276          216.04          36.681          60.423
v  Velocity[y]            -21.858          49.424          0.4292          1.3299
v  Velocity[z]        -2.5524e-11      2.4827e-11      3.4912e-15      3.5237e-14
v  R11                 3.6031e-07          6.1994         0.46309           1.422
v  R22                  3.603e-07          6.1987         0.46307          1.4219
v  R33                  3.603e-07          6.1987         0.46307          1.4219
v  R12                -7.1968e-10      7.8381e-11      1.4109e-12     -7.0953e-13
v  R13                          0               0               0               0
v  R23                          0               0               0               0
v  Dissip                0.026616           611.1          156.11          49.117
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      1.1447e+05      1.0774e+05      1.0778e+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:        0.53514E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         225        -0.286838897E+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         0.286836225E+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   :  0.19234E+00 0.11182E+02
   Friction velocity        uk    :  0.19234E+00 0.11182E+02
   Dimensionless distance   yplus :  0.32528E+01 0.24790E+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     0.26270E-01    1284   0.45552E-02   0.99992E+00 
c  VelocityX    0.23398E+01     980   0.89077E-01   0.11002E+05 
c  VelocityY    0.23398E+01     980   0.89077E-01   0.23682E+04 
c  VelocityZ    0.23398E+01     980   0.89077E-01   0.13937E-20 
c  R11          0.29724E+00   10000   0.25358E-03   0.75235E+02 
c  R22          0.26538E+00   10000   0.23906E-03   0.51227E+02 
c  R33          0.24758E+00   10000   0.41604E-04   0.14647E+02 
c  R12          0.39203E+00    7457   0.48080E-03   0.11709E+03 
c  R13          0.60054E-13       0   0.00000E+00   0.00000E+00 
c  R23          0.52492E-13       0   0.00000E+00   0.00000E+00 
c  Dissip       0.13259E+02   10000   0.64211E-03   0.19799E+06 
c  alpha        0.10586E+02     286   0.29114E-04   0.71456E+02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11                -3.371                           156
a  R22                -6.642                           292
a  R33      
a  R12               -3.7009                          7116
a  R13      
a  R23      
a  Dissip   
a  alpha                              1.0001                       15729
a  LocalTime      7.1728e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -845.22          3055.4          847.39          932.83
v  Velocity[x]            -5.2847          149.77          39.986           62.48
v  Velocity[y]            -14.189          20.936         0.27485          1.0218
v  Velocity[z]        -1.0696e-11       1.334e-11      1.8129e-15      2.9341e-14
v  R11                      1e-24          8.8477          0.5806          1.5816
v  R22                      1e-24          6.5322         0.53755          1.6823
v  R33                 4.5038e-07          5.6487          0.6263          1.6271
v  R12                    -2.5543          3.4655        -0.15857        -0.62557
v  R13                          0               0               0               0
v  R23                          0               0               0               0
v  Dissip                0.054838           20643          40.577          46.414
v  alpha                0.0054213               1         0.89345         0.97619
v  TurbVisc            9.6007e-17        0.071567       0.0036498        0.011764
v  CourantNb               19.094             232          43.423          69.072
v  FourierNb             0.022486      1.3942e+05           380.9          32.174
v  total_pressure      1.0048e+05      1.0438e+05      1.0217e+05      1.0226e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          19.127       1.395e+05          424.32          101.25


 TIME FOR THE TIME STEP                2:        0.47915E+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         0.294642543E+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   :  0.27042E+00 0.69991E+01
   Friction velocity        uk    :  0.27042E+00 0.69991E+01
   Dimensionless distance   yplus :  0.15848E+00 0.24718E+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          7 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.14859E-01    1122   0.26347E-02   0.38391E+00 
c  VelocityX    0.27146E+01     621   0.23371E-01   0.50728E+04 
c  VelocityY    0.27146E+01     621   0.23371E-01   0.31136E+03 
c  VelocityZ    0.27146E+01     621   0.23371E-01   0.12584E-21 
c  R11          0.56691E+00    3620   0.37091E-01   0.35575E+03 
c  R22          0.29075E+00    4931   0.19288E-01   0.22539E+02 
c  R33          0.24789E+00    3037   0.30529E-01   0.29807E+02 
c  R12          0.68305E+00    4930   0.61878E-01   0.68366E+02 
c  R13          0.21799E-07     737   0.44351E-02   0.44161E-12 
c  R23          0.31572E-08     813   0.36319E-02   0.14005E-13 
c  Dissip       0.14499E+03   10000   0.10520E+00   0.14559E+08 
c  alpha        0.52428E+01     171   0.29966E-04   0.36339E+00 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11      
a  R22      
a  R33      
a  R12                -6.942                          1286
a  R13      
a  R23      
a  Dissip   
a  alpha                                   1                       13635
a  LocalTime      3.1404e-06                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1759.5          2083.6          103.29          208.35
v  Velocity[x]            -9.5707          143.07          41.124          62.517
v  Velocity[y]            -12.478          18.732         0.30353          1.1821
v  Velocity[z]        -6.1327e-12      4.2315e-12     -1.1867e-15       1.539e-14
v  R11                 3.7531e-07          13.253         0.94091          2.8663
v  R22                 1.0719e-14          6.4004         0.68767          1.8913
v  R33                 3.7531e-07          5.6454         0.82069          2.0156
v  R12                    -3.5878          7.4323        -0.28554        -0.88001
v  R13                -1.0582e-05      6.4644e-06     -2.4037e-09     -9.2124e-10
v  R23                 -2.395e-06       1.799e-07     -1.7926e-09     -3.5531e-10
v  Dissip                 0.11741      2.2009e+05           137.1          157.87
v  alpha                0.0050936               1         0.84394         0.96528
v  TurbVisc            1.1796e-14        0.085655       0.0045525        0.014686
v  CourantNb               0.1606          161.77          46.052          70.051
v  FourierNb             0.018189           31843          322.72          29.269
v  total_pressure           99566      1.0341e+05      1.0143e+05      1.0153e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           15.47           31907          368.77          99.319


 TIME FOR THE TIME STEP                3:        0.29871E+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         0.294635917E+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   :  0.10875E+00 0.47312E+01
   Friction velocity        uk    :  0.10875E+00 0.47312E+01
   Dimensionless distance   yplus :  0.59472E-01 0.26042E+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

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.12139E-01     906   0.12818E-02   0.28915E+00 
c  VelocityX    0.27384E+01     418   0.25698E-01   0.23932E+04 
c  VelocityY    0.27384E+01     418   0.25698E-01   0.61798E+02 
c  VelocityZ    0.27384E+01     418   0.25698E-01   0.64626E-14 
c  R11          0.10548E+01    1452   0.39487E-02   0.19778E+03 
c  R22          0.48064E+00    1635   0.34975E-02   0.51123E+02 
c  R33          0.56556E+00    1892   0.34305E-02   0.60951E+02 
c  R12          0.71073E+00    1484   0.43820E-02   0.46618E+02 
c  R13          0.26246E-09    2273   0.45042E+00   0.41268E-12 
c  R23          0.59853E-09    2017   0.25456E-01   0.12091E-13 
c  Dissip       0.35620E+03    2000   0.90491E-02   0.35408E+09 
c  alpha        0.52990E+02     142   0.10539E-04   0.14156E+01 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -13.853                           147
a  R22               -3.9083                            62
a  R33               -5.8773                           137
a  R12               -3.3747                           576
a  R13           -2.1169e-07                           133
a  R23           -1.7725e-07                            31
a  Dissip            -918.23                             6
a  alpha                              1.0001                       15048
a  LocalTime      2.1828e-05                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                 -2014            1572          -84.66           24.96
v  Velocity[x]             -8.176          141.43          42.188          62.512
v  Velocity[y]            -11.798           17.48         0.26674          1.1227
v  Velocity[z]        -4.8799e-07      3.0392e-07       2.158e-09     -2.0048e-12
v  R11                      1e-24          19.969          1.2146          3.5409
v  R22                      1e-24          7.5399         0.87104          2.2274
v  R33                      1e-24          8.5949          0.9792          2.4328
v  R12                    -3.3747            6.86        -0.37018        -0.92947
v  R13                -2.1169e-07      8.9795e-08     -2.1932e-10     -8.6491e-11
v  R23                -1.7725e-07      4.3519e-08      -4.746e-10       -1.09e-10
v  Dissip                 0.16889      2.9628e+05          215.58          435.59
v  alpha                0.0033526               1         0.82481         0.99532
v  TurbVisc             4.097e-14        0.039576        0.004846           0.013
v  CourantNb             0.019093          155.21          47.879          70.561
v  FourierNb             0.016721          4581.3          231.39          29.092
v  total_pressure           99311       1.029e+05      1.0124e+05      1.0135e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          13.096          4607.5          279.27          99.654


 TIME FOR THE TIME STEP                4:        0.16619E+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         0.294673166E+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   :  0.86084E-01 0.44955E+01
   Friction velocity        uk    :  0.86084E-01 0.44955E+01
   Dimensionless distance   yplus :  0.31395E-01 0.25893E+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     0.13941E-01     906   0.11166E-02   0.33569E+00 
c  VelocityX    0.27455E+01     419   0.21986E-01   0.19962E+04 
c  VelocityY    0.27455E+01     419   0.21986E-01   0.44596E+02 
c  VelocityZ    0.27455E+01     419   0.21986E-01   0.28580E-14 
c  R11          0.15553E+01    2414   0.96557E-03   0.10467E+03 
c  R22          0.62104E+00    3083   0.10144E-02   0.30502E+02 
c  R33          0.83900E+00    2373   0.87240E-03   0.35601E+02 
c  R12          0.44667E+00    3561   0.14501E-02   0.35657E+02 
c  R13          0.19399E-03       3   0.53810E-05   0.13992E-14 
c  R23          0.87049E-05     335   0.16261E-04   0.16798E-13 
c  Dissip       0.19335E+04     449   0.10048E-02   0.22187E+09 
c  alpha        0.31651E+03      99   0.97350E-05   0.84616E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11            4.5334e-25                            25
a  R22            4.0696e-25                            26
a  R33            4.4728e-25                            26
a  R12               -3.4536                            27
a  R13      
a  R23      
a  Dissip            -460.47                           182
a  alpha                              1.0032                       14998
a  LocalTime      2.8835e-05                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2167.7            1230          -199.5          -81.44
v  Velocity[x]            -9.1212          123.62          42.636          62.507
v  Velocity[y]             -11.96           15.76         0.15057         0.77441
v  Velocity[z]        -1.7451e-07      1.6252e-07       3.184e-09     -4.6052e-12
v  R11                      1e-24          26.517          1.5019          3.9867
v  R22                      1e-24          7.8605          1.0801          2.5265
v  R33                      1e-24          12.331           1.173          2.7613
v  R12                    -3.4536          6.8466        -0.52658         -1.0394
v  R13                -5.4141e-07      2.1141e-07     -2.2262e-10     -1.1027e-10
v  R23                -3.5584e-06       2.509e-07      -2.073e-09      -1.494e-10
v  Dissip                 0.13414       2.156e+05           211.4           654.7
v  alpha                 0.002645               1         0.81186         0.99527
v  TurbVisc            1.1024e-52        0.040008       0.0062414        0.015118
v  CourantNb             0.030536          152.21          49.375          70.788
v  FourierNb             0.015089            3468          267.62          41.406
v  total_pressure           99157      1.0255e+05      1.0113e+05      1.0124e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          19.314          3504.2          316.99          112.19


 TIME FOR THE TIME STEP                5:        0.15660E+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         0.294675459E+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   :  0.12069E+00 0.39467E+01
   Friction velocity        uk    :  0.12069E+00 0.39467E+01
   Dimensionless distance   yplus :  0.70628E-01 0.24208E+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     0.12640E-01     996   0.14491E-02   0.31621E+00 
c  VelocityX    0.27455E+01     424   0.14632E-01   0.13861E+04 
c  VelocityY    0.27455E+01     424   0.14632E-01   0.59340E+02 
c  VelocityZ    0.27455E+01     424   0.14632E-01   0.46739E-13 
c  R11          0.13186E+01    7976   0.12577E-02   0.12189E+03 
c  R22          0.56042E+00    7606   0.96857E-03   0.23088E+02 
c  R33          0.73847E+00    7630   0.98074E-03   0.29394E+02 
c  R12          0.37009E+00    9340   0.20930E-02   0.30426E+02 
c  R13          0.66360E-05     646   0.51629E-04   0.31823E-13 
c  R23          0.19170E-06    5209   0.13436E-02   0.10967E-12 
c  Dissip       0.12127E+04    4976   0.44274E-03   0.25588E+09 
c  alpha        0.41495E+03      83   0.92968E-05   0.47374E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11            4.4884e-25                            26
a  R22            3.8474e-25                            26
a  R33            4.4872e-25                            26
a  R12               -3.9499                            66
a  R13      
a  R23      
a  Dissip            -3103.2                           756
a  alpha                              1.0028                       12589
a  LocalTime      2.7617e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2370.9           892.8         -390.44         -262.09
v  Velocity[x]            -16.628          98.599          42.391          62.503
v  Velocity[y]            -12.618          14.494        0.035926         0.38735
v  Velocity[z]         -1.249e-06      1.5001e-06      7.9363e-09     -1.4975e-11
v  R11                      1e-24          32.521          1.9222          4.3737
v  R22                      1e-24          9.6819           1.287          2.7559
v  R33                      1e-24          15.493          1.4044          3.0136
v  R12                    -3.9499          8.8171         -0.7257         -1.0952
v  R13                -3.6175e-06      1.1471e-06     -1.6695e-09      -1.556e-10
v  R23                -3.2756e-06       5.431e-06      5.4643e-09      4.3075e-10
v  Dissip                0.023993      1.8792e+05          147.38          537.33
v  alpha                0.0023204               1         0.79895          0.9943
v  TurbVisc            1.5404e-52         0.24277       0.0081939        0.017683
v  CourantNb             0.031297          130.14              50          70.408
v  FourierNb             0.012777      3.6209e+05           482.9           68.83
v  total_pressure           98954      1.0222e+05      1.0093e+05      1.0106e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          31.132      3.6211e+05           532.9          139.24


 TIME FOR THE TIME STEP                6:        0.40860E+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         0.294671600E+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   :  0.68769E-01 0.34011E+01
   Friction velocity        uk    :  0.68769E-01 0.34011E+01
   Dimensionless distance   yplus :  0.39619E-01 0.21620E+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     0.10289E-01     996   0.13956E-02   0.27557E+00 
c  VelocityX    0.27456E+01     429   0.98213E-02   0.76927E+03 
c  VelocityY    0.27456E+01     429   0.98213E-02   0.41380E+02 
c  VelocityZ    0.27456E+01     429   0.98213E-02   0.19289E-12 
c  R11          0.15052E+01   10000   0.51074E-02   0.14354E+03 
c  R22          0.54281E+00   10000   0.12501E-01   0.21636E+02 
c  R33          0.78543E+00   10000   0.83059E-02   0.35149E+02 
c  R12          0.40070E+00   10000   0.11355E-01   0.25407E+02 
c  R13          0.76602E-06   10000   0.65590E-02   0.11630E-11 
c  R23          0.35955E-07   10000   0.17792E+00   0.10737E-12 
c  Dissip       0.10244E+04   10000   0.18112E-02   0.39752E+08 
c  alpha        0.29515E+03     103   0.97770E-05   0.57455E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11            4.3667e-25                            26
a  R22            3.7685e-25                            26
a  R33             4.366e-25                            26
a  R12               -4.7274                             7
a  R13      
a  R23      
a  Dissip            -23.744                            14
a  alpha                              1.0027                       12212
a  LocalTime      7.1977e-09                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2556.5          604.46         -589.35         -453.81
v  Velocity[x]            -26.705          92.188          41.782          62.501
v  Velocity[y]            -13.373          13.569       -0.034398         0.11569
v  Velocity[z]        -1.8962e-06        1.44e-06      -6.651e-09      3.8561e-11
v  R11                      1e-24          40.731          2.4409          4.8952
v  R22                      1e-24              12          1.4819          2.9642
v  R33                      1e-24          19.403          1.6679          3.2949
v  R12                    -4.7274          10.751        -0.89322         -1.1421
v  R13                -8.5337e-07       1.176e-05      1.5628e-08      2.6739e-09
v  R23                -1.7932e-06       7.398e-07     -9.0132e-10     -3.5265e-10
v  Dissip                0.088499       1.569e+05          181.87          593.27
v  alpha                0.0021644               1          0.7895         0.99364
v  TurbVisc            7.9741e-53          5.6169        0.010953        0.025684
v  CourantNb             0.025234          100.87          50.087          69.906
v  FourierNb             0.012259      1.3893e+07          1391.8          120.37
v  total_pressure           98769      1.0193e+05      1.0074e+05      1.0087e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          38.275      1.3893e+07          1441.9          190.28


 TIME FOR THE TIME STEP                7:        0.61913E+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         0.294672087E+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   :  0.18822E-01 0.29153E+01
   Friction velocity        uk    :  0.18822E-01 0.29153E+01
   Dimensionless distance   yplus :  0.10165E-01 0.19114E+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          4 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.79758E-02     924   0.11434E-02   0.23368E+00 
c  VelocityX    0.27458E+01     412   0.17380E-01   0.41169E+03 
c  VelocityY    0.27458E+01     412   0.17380E-01   0.20361E+02 
c  VelocityZ    0.27458E+01     412   0.17380E-01   0.11201E-12 
c  R11          0.18111E+01   10000   0.10473E-01   0.16020E+03 
c  R22          0.62281E+00    9345   0.22735E-01   0.23058E+02 
c  R33          0.93264E+00    8745   0.14674E-01   0.41641E+02 
c  R12          0.45640E+00   10000   0.22119E-01   0.21118E+02 
c  R13          0.38096E-07    7866   0.27211E-01   0.85756E-12 
c  R23          0.46733E-08   10000   0.13878E+00   0.48454E-13 
c  Dissip       0.12655E+04   10000   0.91671E-03   0.37438E+08 
c  alpha        0.26398E+03      95   0.96755E-05   0.15217E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11              -0.43423                           211
a  R22            3.6227e-25                            26
a  R33            4.3416e-25                            26
a  R12               -5.5825                           407
a  R13           -8.6251e-07                           185
a  R23      
a  Dissip   
a  alpha                              1.0011                       12154
a  LocalTime      4.3946e-06                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2682.9          447.01         -747.74         -609.41
v  Velocity[x]             -34.71          92.486          41.022            62.5
v  Velocity[y]            -14.041          13.624       -0.065146       -0.036747
v  Velocity[z]        -1.0096e-06      1.5512e-06     -6.7523e-09      5.6786e-11
v  R11                      1e-24          49.415          2.8618          5.4812
v  R22                      1e-24          14.677          1.6647          3.1845
v  R33                      1e-24          23.705           1.914          3.6046
v  R12                    -5.5825          12.847        -0.98224         -1.2102
v  R13                -8.6251e-07      8.7544e-07      8.6449e-09      5.8422e-10
v  R23                 -4.697e-07      3.7033e-07     -6.0146e-09     -1.9229e-10
v  Dissip                0.073159      1.3186e+05          272.69          692.97
v  alpha                0.0020124               1         0.78953         0.99374
v  TurbVisc            6.8631e-53          4.0189        0.011269        0.023397
v  CourantNb            0.0068358           99.74          50.217           69.62
v  FourierNb             0.012784           22755          788.15          103.43
v  total_pressure           98642      1.0177e+05      1.0058e+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          37.808           22790          838.36          173.05


 TIME FOR THE TIME STEP                8:        0.58455E+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         0.294670125E+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   :  0.18389E+00 0.24764E+01
   Friction velocity        uk    :  0.18389E+00 0.24764E+01
   Dimensionless distance   yplus :  0.68377E-01 0.17405E+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          7 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62654E-02     744   0.91087E-03   0.19993E+00 
c  VelocityX    0.27461E+01     407   0.14718E-01   0.24475E+03 
c  VelocityY    0.27461E+01     407   0.14718E-01   0.93892E+01 
c  VelocityZ    0.27461E+01     407   0.14718E-01   0.21176E-12 
c  R11          0.21007E+01    4094   0.14366E-01   0.17567E+03 
c  R22          0.70779E+00    6024   0.30488E-01   0.23775E+02 
c  R33          0.10768E+01    5334   0.19199E-01   0.46637E+02 
c  R12          0.52323E+00    8489   0.29324E-01   0.18513E+02 
c  R13          0.53867E-08    4561   0.11260E+00   0.45867E-13 
c  R23          0.20479E-08    5422   0.25704E+00   0.25087E-13 
c  Dissip       0.14797E+04    1772   0.63932E-03   0.30022E+08 
c  alpha        0.25086E+03     111   0.97265E-05   0.16077E-01 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11              -0.68537                           427
a  R22             3.714e-25                            26
a  R33            4.2984e-25                            26
a  R12               -6.4955                          1310
a  R13            -1.333e-06                           401
a  R23      
a  Dissip            -1445.1                           931
a  alpha                               1.002                       14446
a  LocalTime      2.0581e-06                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2753.6          287.08         -859.79         -722.12
v  Velocity[x]            -38.949          93.535          40.102            62.5
v  Velocity[y]            -14.617          14.034       -0.071511        -0.10386
v  Velocity[z]         -1.635e-06       2.245e-06      9.7968e-09     -6.7931e-11
v  R11                      1e-24          58.741          3.2796          6.1237
v  R22                      1e-24          17.524          1.8417          3.4227
v  R33                      1e-24          28.351          2.1156          3.9362
v  R12                    -6.4955          15.163         -1.0756         -1.3011
v  R13                 -1.333e-06      4.1131e-07     -1.5671e-09     -3.4967e-10
v  R23                -6.0012e-07      1.7732e-06     -3.1862e-09      2.0193e-10
v  Dissip                0.060615      1.1048e+05          271.09          763.05
v  alpha                0.0018778               1         0.80493         0.99488
v  TurbVisc            4.5361e-53        0.097682        0.011909        0.025205
v  CourantNb             0.031128          125.95          50.386          69.541
v  FourierNb             0.013383           48590          433.51          84.536
v  total_pressure           98571      1.0161e+05      1.0047e+05       1.006e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          34.082           48610           483.9          154.08


 TIME FOR THE TIME STEP                9:        0.33934E+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         0.294672297E+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   :  0.16651E+00 0.21694E+01
   Friction velocity        uk    :  0.16651E+00 0.21694E+01
   Dimensionless distance   yplus :  0.62062E-01 0.16951E+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         10 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54880E-02     780   0.81392E-03   0.18581E+00 
c  VelocityX    0.27468E+01     406   0.16233E-01   0.18842E+03 
c  VelocityY    0.27468E+01     406   0.16233E-01   0.65214E+01 
c  VelocityZ    0.27468E+01     406   0.16233E-01   0.50168E-12 
c  R11          0.24589E+01    6320   0.17542E-01   0.19123E+03 
c  R22          0.80975E+00    5421   0.37274E-01   0.23634E+02 
c  R33          0.12512E+01    5844   0.23464E-01   0.50034E+02 
c  R12          0.60874E+00    7294   0.34869E-01   0.16550E+02 
c  R13          0.91791E-08    5022   0.17946E+00   0.46122E-13 
c  R23          0.38157E-08    5716   0.17347E+00   0.29217E-13 
c  Dissip       0.17265E+04    2751   0.51299E-03   0.47200E+08 
c  alpha        0.20224E+03     101   0.96521E-05   0.79613E-03 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -3.1791                           347
a  R22              -0.12077                            41
a  R33              -0.35937                            46
a  R12               -7.4134                           484
a  R13           -3.2013e-06                           321
a  R23           -6.3907e-07                            22
a  Dissip            -1556.2                           795
a  alpha                              1.0013                       13146
a  LocalTime      5.6264e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2787.7           171.9         -935.95         -800.77
v  Velocity[x]            -40.508          94.905          39.122          62.497
v  Velocity[y]            -15.203          14.574       -0.064156         -0.1131
v  Velocity[z]        -2.1992e-06      3.2932e-06      2.0098e-08     -1.9184e-10
v  R11                      1e-24          68.605          3.7318          6.8192
v  R22                      1e-24          20.525           2.032          3.6746
v  R33                      1e-24          33.279          2.3592           4.293
v  R12                    -7.4134          17.536         -1.2341          -1.411
v  R13                -3.2013e-06      1.7468e-06     -3.2726e-09     -5.5298e-10
v  R23                -6.3907e-07      1.0293e-06     -2.8053e-10       1.493e-10
v  Dissip                0.050174           92554          264.37           866.8
v  alpha                0.0017614               1         0.80018         0.99464
v  TurbVisc            4.0461e-53          3.1294        0.013604        0.027888
v  CourantNb             0.028982          169.59           50.27          69.555
v  FourierNb             0.013384      1.7773e+06          600.54          104.88
v  total_pressure           98537       1.015e+05      1.0039e+05      1.0052e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          22.259      1.7773e+06          650.81          174.44


 TIME FOR THE TIME STEP               10:        0.36115E+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         0.294644250E+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   :  0.10464E+00 0.25988E+01
   Friction velocity        uk    :  0.10464E+00 0.25988E+01
   Dimensionless distance   yplus :  0.38817E-01 0.16900E+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         19 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.49338E-02     780   0.77473E-03   0.17111E+00 
c  VelocityX    0.27478E+01     404   0.13942E-01   0.17121E+03 
c  VelocityY    0.27478E+01     404   0.13942E-01   0.67378E+01 
c  VelocityZ    0.27478E+01     404   0.13942E-01   0.40494E-12 
c  R11          0.28784E+01   10000   0.19021E-01   0.19313E+03 
c  R22          0.93737E+00   10000   0.39422E-01   0.22816E+02 
c  R33          0.14604E+01   10000   0.25305E-01   0.50568E+02 
c  R12          0.70810E+00   10000   0.35740E-01   0.14925E+02 
c  R13          0.78262E-05    3938   0.35793E-03   0.17793E-12 
c  R23          0.46914E-07    8081   0.32322E-01   0.45276E-13 
c  Dissip       0.20541E+04   10000   0.44201E-03   0.61441E+08 
c  alpha        0.17305E+03     105   0.99529E-05   0.15903E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -2.8122                           376
a  R22              -0.10004                            62
a  R33             -0.060092                            36
a  R12               -8.2598                           949
a  R13           -1.4355e-06                           341
a  R23           -1.0347e-06                            25
a  Dissip            -2811.7                          3170
a  alpha                              1.0007                       11361
a  LocalTime      1.8098e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2795.5          127.24         -981.78         -849.57
v  Velocity[x]            -41.001          96.436          38.267          62.497
v  Velocity[y]             -15.78          15.168       -0.048106       -0.083476
v  Velocity[z]        -2.4307e-06      3.9745e-06      1.7714e-08     -2.8525e-10
v  R11                      1e-24           78.77          4.1744          7.5187
v  R22                      1e-24           23.61          2.2264          3.9286
v  R33                      1e-24          38.387           2.611          4.6535
v  R12                    -8.2598          19.925         -1.3991         -1.5231
v  R13                -1.4355e-06      6.2802e-06      4.9042e-09      1.2534e-09
v  R23                -1.0347e-06      1.6619e-06      2.8651e-10     -1.7838e-10
v  Dissip               0.0035912           77439          293.06          993.35
v  alpha                0.0016733               1          0.7957         0.99425
v  TurbVisc            3.1537e-53          1.6169        0.015434        0.030481
v  CourantNb             0.013095          222.22          49.943          69.623
v  FourierNb             0.013631      5.5254e+05          759.84          129.63
v  total_pressure           98530      1.0145e+05      1.0034e+05      1.0048e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          15.484      5.5257e+05          809.78          199.25


 TIME FOR THE TIME STEP               11:        0.55081E+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         0.294641895E+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   :  0.86834E-01 0.30057E+01
   Friction velocity        uk    :  0.86834E-01 0.30057E+01
   Dimensionless distance   yplus :  0.31609E-01 0.17079E+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


 Write intermediate restart files
   checkpoint at iteration         12, Physical time    0.12000E+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:    0.15916E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.47150E-02     708   0.75273E-03   0.16262E+00 
c  VelocityX    0.27487E+01     403   0.90099E-02   0.16453E+03 
c  VelocityY    0.27487E+01     403   0.90099E-02   0.70909E+01 
c  VelocityZ    0.27487E+01     403   0.90099E-02   0.32638E-12 
c  R11          0.33413E+01   10000   0.24809E-01   0.19014E+03 
c  R22          0.10847E+01   10000   0.58420E-01   0.21518E+02 
c  R33          0.16948E+01   10000   0.37117E-01   0.49584E+02 
c  R12          0.82489E+00   10000   0.72185E-01   0.13397E+02 
c  R13          0.26441E-04    7810   0.88155E-03   0.24772E-12 
c  R23          0.18124E-06   10000   0.47820E-01   0.57886E-13 
c  Dissip       0.24206E+04   10000   0.94808E-03   0.72155E+08 
c  alpha        0.15319E+03     111   0.99086E-05   0.18246E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11            4.2557e-25                            37
a  R22            -0.0029613                            44
a  R33            4.2557e-25                            36
a  R12               -8.9815                           428
a  R13      
a  R23           -8.3123e-07                             5
a  Dissip            -218.92                           120
a  alpha                              1.0014                       10887
a  LocalTime      1.8082e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2785.3          113.93         -1003.3         -873.71
v  Velocity[x]            -41.232          97.949           37.49          62.498
v  Velocity[y]            -16.425          15.781       -0.028663       -0.034018
v  Velocity[z]        -3.0894e-06      3.0238e-06      1.0785e-08     -3.9708e-10
v  R11                      1e-24          89.297          4.5803          8.1972
v  R22                      1e-24          26.715          2.3968          4.1753
v  R33                      1e-24          43.598          2.8365          5.0038
v  R12                    -8.9815          22.325         -1.5213         -1.6199
v  R13                -5.0867e-06       4.415e-07     -2.8265e-09     -8.5859e-10
v  R23                -8.3123e-07      1.9548e-06       3.102e-09      3.8204e-10
v  Dissip                0.034681           64754          331.06          1129.5
v  alpha                 0.001598               1         0.79006         0.99385
v  TurbVisc            2.6542e-53           13.41          0.0186         0.03305
v  CourantNb             0.010886          276.04          49.761          69.747
v  FourierNb             0.013278      5.5302e+06          1638.4          223.73
v  total_pressure           98540      1.0144e+05      1.0032e+05      1.0045e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.354      5.5303e+06          1688.2          293.48


 TIME FOR THE TIME STEP               12:        0.59753E+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         0.294641833E+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   :  0.47540E-01 0.33778E+01
   Friction velocity        uk    :  0.47540E-01 0.33778E+01
   Dimensionless distance   yplus :  0.16993E-01 0.17559E+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         43 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.48046E-02     546   0.72546E-03   0.16097E+00 
c  VelocityX    0.27504E+01     404   0.10431E-01   0.15416E+03 
c  VelocityY    0.27504E+01     404   0.10431E-01   0.71323E+01 
c  VelocityZ    0.27504E+01     404   0.10431E-01   0.74707E-12 
c  R11          0.38579E+01   10000   0.22317E-01   0.18571E+03 
c  R22          0.12454E+01   10000   0.47056E-01   0.20104E+02 
c  R33          0.19543E+01   10000   0.31399E-01   0.47826E+02 
c  R12          0.94732E+00   10000   0.41401E-01   0.12638E+02 
c  R13          0.67550E-06   10000   0.25535E-01   0.78673E-12 
c  R23          0.33353E-07   10000   0.33369E+00   0.10115E-12 
c  Dissip       0.28329E+04   10000   0.76767E-03   0.93219E+08 
c  alpha        0.13540E+03     122   0.98180E-05   0.45216E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -4.3644                           321
a  R22            5.7231e-26                            33
a  R33            4.2458e-25                            26
a  R12               -9.5452                           313
a  R13           -1.2284e-05                           295
a  R23      
a  Dissip            -2.3206                             1
a  alpha                              1.0021                       12447
a  LocalTime      3.8611e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                 -2761          125.65         -1004.7         -876.84
v  Velocity[x]            -41.537          99.562          36.661          62.498
v  Velocity[y]            -17.198          16.358       -0.010381        0.019772
v  Velocity[z]        -2.6144e-06      2.2724e-06      -1.182e-09     -4.3817e-10
v  R11                      1e-24           99.99          4.8616           8.842
v  R22                      1e-24          29.812          2.5331          4.4123
v  R33                      1e-24          48.942          3.0208           5.341
v  R12                    -9.5452          24.711         -1.5829         -1.6921
v  R13                -1.2284e-05      1.0778e-06      4.8047e-10     -1.6153e-09
v  R23                -9.3836e-07      4.1287e-06      5.0946e-09      6.8486e-10
v  Dissip                0.028894           70174          411.29          1287.3
v  alpha                 0.001517               1         0.79055          0.9937
v  TurbVisc            2.2819e-53          2.3487        0.018466        0.034943
v  CourantNb              0.01161          334.43          49.872          69.906
v  FourierNb             0.012421      2.5899e+06          1076.5          169.08
v  total_pressure           98564      1.0145e+05      1.0032e+05      1.0045e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.9378        2.59e+06          1126.4          238.99


 TIME FOR THE TIME STEP               13:        0.61107E+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         0.294641821E+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   :  0.10701E+00 0.36867E+01
   Friction velocity        uk    :  0.10701E+00 0.36867E+01
   Dimensionless distance   yplus :  0.50636E-01 0.18071E+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         49 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.48352E-02     600   0.69607E-03   0.15608E+00 
c  VelocityX    0.27517E+01     404   0.10230E-01   0.15120E+03 
c  VelocityY    0.27517E+01     404   0.10230E-01   0.72429E+01 
c  VelocityZ    0.27517E+01     404   0.10230E-01   0.86759E-12 
c  R11          0.44342E+01    5230   0.24141E-01   0.18885E+03 
c  R22          0.14291E+01    5711   0.50565E-01   0.20288E+02 
c  R33          0.22459E+01    5269   0.34567E-01   0.48571E+02 
c  R12          0.10891E+01    6576   0.46671E-01   0.12079E+02 
c  R13          0.10077E-05    1659   0.11810E-01   0.55774E-12 
c  R23          0.15698E-07    4288   0.28589E+00   0.18680E-12 
c  Dissip       0.33043E+04    3119   0.40797E-03   0.11665E+09 
c  alpha        0.12278E+03     124   0.98532E-05   0.80509E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -0.8592                           128
a  R22            2.1946e-25                            33
a  R33             4.236e-25                            32
a  R12               -9.9502                           627
a  R13           -1.7786e-06                            96
a  R23      
a  Dissip            -1422.5                          1110
a  alpha                              1.0013                       13379
a  LocalTime      1.2088e-06                         89999


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2725.8           156.3         -991.04         -864.08
v  Velocity[x]            -42.892          101.25          35.714          62.499
v  Velocity[y]            -18.064          16.922       0.0036066        0.066435
v  Velocity[z]        -5.0474e-06      6.6786e-06     -1.5789e-08      -2.516e-10
v  R11                      1e-24          110.73          5.1301          9.4693
v  R22                      1e-24          32.884          2.6158          4.6396
v  R33                      1e-24          54.285          3.1444          5.6611
v  R12                    -9.9502          27.011         -1.6423          -1.744
v  R13                -1.7786e-06      1.6212e-06      2.1579e-09      3.6367e-11
v  R23                -3.5436e-06      1.8122e-06     -8.7243e-09     -5.4727e-10
v  Dissip                0.024082           79064          396.26            1452
v  alpha                0.0014493               1         0.80254         0.99454
v  TurbVisc            1.9381e-53         0.10284        0.018321        0.036545
v  CourantNb             0.018871          395.48          50.178           70.07
v  FourierNb             0.011795           82728          541.76          125.84
v  total_pressure           98599      1.0148e+05      1.0033e+05      1.0046e+05
v  LocalTime                 0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.4716           82749          591.94          195.91


 TIME FOR THE TIME STEP               14:        0.30632E+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         0.294642405E+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   :  0.15680E+00 0.39429E+01
   Friction velocity        uk    :  0.15680E+00 0.39429E+01
   Dimensionless distance   yplus :  0.57325E-01 0.18420E+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         53 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.42367E-02     582   0.67991E-03   0.13262E+00 
c  VelocityX    0.27535E+01     403   0.10049E-01   0.16668E+03 
c  VelocityY    0.27535E+01     403   0.10049E-01   0.81797E+01 
c  VelocityZ    0.27535E+01     403   0.10049E-01   0.17591E-11 
c  R11          0.50700E+01   10000   0.23608E-01   0.18862E+03 
c  R22          0.16342E+01   10000   0.49070E-01   0.20087E+02 
c  R33          0.25686E+01   10000   0.34625E-01   0.48007E+02 
c  R12          0.12472E+01   10000   0.47980E-01   0.11806E+02 
c  R13          0.27410E-06   10000   0.16008E+00   0.39249E-11 
c  R23          0.11008E-06   10000   0.20265E+00   0.94059E-12 
c  Dissip       0.38344E+04   10000   0.62965E-03   0.14306E+09 
c  alpha        0.11370E+03     123   0.96711E-05   0.67319E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11            4.2279e-25                            26
a  R22            3.6833e-26                            33
a  R33            4.2278e-25                            26
a  R12               -10.267                            65
a  R13      
a  R23      
a  Dissip            -552.84                           562
a  alpha                               1.001                       11792
a  LocalTime      6.7183e-08                         89998


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2684.1          199.73         -968.79         -841.95
v  Velocity[x]            -46.253          103.04          34.782          62.499
v  Velocity[y]            -19.024          17.486        0.012192         0.10029
v  Velocity[z]        -3.4528e-06      9.5497e-06      6.1271e-09     -1.6618e-10
v  R11                      1e-24           121.6           5.445          10.079
v  R22                      1e-24          35.857          2.7305          4.8654
v  R33                      1e-24          59.594           3.313          5.9773
v  R12                    -10.267          29.234         -1.7412          -1.776
v  R13                -8.9035e-06       3.035e-05      1.8089e-09      5.8902e-10
v  R23                -1.2144e-05      4.5243e-06      -1.426e-08       -1.61e-09
v  Dissip                0.020076           91402           416.5          1636.6
v  alpha                0.0013602               1         0.78893          0.9935
v  TurbVisc            1.6761e-53          2.2217        0.020283        0.038702
v  CourantNb             0.024316          452.75          50.593          70.237
v  FourierNb             0.011983      1.4885e+06          1120.9          176.48
v  total_pressure           98641      1.0152e+05      1.0036e+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           3.547      1.4885e+06          1171.5          246.72


 TIME FOR THE TIME STEP               15:        0.61161E+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         0.294639980E+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   :  0.13904E+00 0.41883E+01
   Friction velocity        uk    :  0.13904E+00 0.41883E+01
   Dimensionless distance   yplus :  0.79627E-01 0.18736E+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         55 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.46238E-02     544   0.67673E-03   0.13983E+00 
c  VelocityX    0.27550E+01     402   0.99614E-02   0.20106E+03 
c  VelocityY    0.27550E+01     402   0.99614E-02   0.10134E+02 
c  VelocityZ    0.27550E+01     402   0.99614E-02   0.18059E-11 
c  R11          0.57710E+01   10000   0.24045E-01   0.20021E+03 
c  R22          0.18615E+01   10000   0.45521E-01   0.22205E+02 
c  R33          0.29241E+01   10000   0.32426E-01   0.50911E+02 
c  R12          0.14232E+01   10000   0.59386E-01   0.12601E+02 
c  R13          0.20686E-06   10000   0.17664E+00   0.30626E-11 
c  R23          0.66461E-07   10000   0.56331E+00   0.84389E-12 
c  Dissip       0.44304E+04   10000   0.12147E-02   0.17761E+09 
c  alpha        0.10689E+03     139   0.99547E-05   0.56428E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11            4.2211e-25                            26
a  R22             5.467e-26                            32
a  R33            4.2209e-25                            26
a  R12               -10.509                           103
a  R13      
a  R23      
a  Dissip            -5.2712                            38
a  alpha                              1.0018                       11781
a  LocalTime      1.2441e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2640.5          250.49         -943.99         -816.54
v  Velocity[x]            -50.392             105          34.025            62.5
v  Velocity[y]            -20.092          18.033        0.016321         0.12146
v  Velocity[z]        -5.8304e-06      8.0878e-06      3.6569e-08     -5.4607e-10
v  R11                      1e-24          132.37          5.7085          10.666
v  R22                      1e-24          38.758           2.821          5.0901
v  R33                      1e-24          64.895          3.4547          6.2846
v  R12                    -10.509          31.379         -1.8169          -1.781
v  R13                -4.8882e-06      4.6734e-06     -9.8155e-09     -1.5202e-09
v  R23                -2.1875e-06       2.043e-06      1.4943e-08      1.1826e-09
v  Dissip                0.016738      1.0556e+05          487.74          1842.6
v  alpha                0.0012901               1         0.78237          0.9929
v  TurbVisc            1.4606e-53           9.772        0.021971        0.041651
v  CourantNb             0.025592          505.79          51.114          70.416
v  FourierNb             0.012826      8.0378e+06          1895.7          226.53
v  total_pressure           98685      1.0158e+05      1.0038e+05      1.0051e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           3.467      8.0379e+06          1946.9          296.95


 TIME FOR THE TIME STEP               16:        0.61117E+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         0.294648963E+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   :  0.12102E+00 0.45077E+01
   Friction velocity        uk    :  0.12102E+00 0.45077E+01
   Dimensionless distance   yplus :  0.69574E-01 0.19033E+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         58 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.50708E-02     546   0.68967E-03   0.14866E+00 
c  VelocityX    0.27568E+01     401   0.10599E-01   0.23916E+03 
c  VelocityY    0.27568E+01     401   0.10599E-01   0.12777E+02 
c  VelocityZ    0.27568E+01     401   0.10599E-01   0.21870E-11 
c  R11          0.65433E+01   10000   0.27243E-01   0.21369E+03 
c  R22          0.21306E+01   10000   0.55851E-01   0.26336E+02 
c  R33          0.33191E+01   10000   0.36861E-01   0.54503E+02 
c  R12          0.16186E+01   10000   0.54284E-01   0.13757E+02 
c  R13          0.20466E-06    8247   0.14568E+00   0.32762E-12 
c  R23          0.20952E-07   10000   0.12710E+01   0.33026E-12 
c  Dissip       0.51012E+04    5270   0.15000E-02   0.21922E+09 
c  alpha        0.10232E+03     121   0.98015E-05   0.94060E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -4.3649                          1124
a  R22              -0.25231                            49
a  R33            4.2144e-25                            26
a  R12               -10.859                          1186
a  R13           -2.8199e-06                          1087
a  R23           -1.5837e-06                            12
a  Dissip            -458.72                           719
a  alpha                              1.0018                       13585
a  LocalTime      3.7627e-06                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2598.9          304.14          -921.4         -792.81
v  Velocity[x]            -53.254           107.1          33.362          62.501
v  Velocity[y]            -21.286          18.526        0.017697         0.13399
v  Velocity[z]        -1.0979e-05      6.1656e-06     -9.1893e-09     -3.9456e-10
v  R11                      1e-24          143.05          5.7902          11.227
v  R22                      1e-24          41.537          2.8754          5.3222
v  R33                      1e-24          70.063          3.5233          6.5815
v  R12                    -10.859          33.446         -1.8028         -1.7533
v  R13                -1.5833e-06      1.2916e-06     -4.2019e-09     -5.4267e-10
v  R23                -1.5837e-06      3.1053e-06      3.2155e-08      1.5827e-09
v  Dissip                0.013955      1.2163e+05          530.51          2067.5
v  alpha                0.0012523               1         0.79118         0.99371
v  TurbVisc            1.2757e-53          127.24        0.027215        0.077713
v  CourantNb             0.019472          550.43          51.818          70.614
v  FourierNb             0.013753           26577          803.35          177.51
v  total_pressure           98726      1.0163e+05       1.004e+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          2.9979           26627          855.17          248.12


 TIME FOR THE TIME STEP               17:        0.55903E+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         0.294663341E+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   :  0.15690E+00 0.48600E+01
   Friction velocity        uk    :  0.15690E+00 0.48600E+01
   Dimensionless distance   yplus :  0.55802E-01 0.19289E+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         63 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54304E-02     546   0.71610E-03   0.15461E+00 
c  VelocityX    0.27584E+01     401   0.97238E-02   0.27322E+03 
c  VelocityY    0.27584E+01     401   0.97238E-02   0.15964E+02 
c  VelocityZ    0.27584E+01     401   0.97238E-02   0.85100E-11 
c  R11          0.73871E+01    7336   0.19625E-01   0.22663E+03 
c  R22          0.23991E+01    7887   0.40972E-01   0.32081E+02 
c  R33          0.37478E+01    7871   0.30145E-01   0.58539E+02 
c  R12          0.18332E+01    8702   0.41065E-01   0.15462E+02 
c  R13          0.18871E-06    7368   0.26835E-01   0.73403E-12 
c  R23          0.85128E-08    9915   0.45424E+00   0.29425E-12 
c  Dissip       0.58522E+04    2512   0.50071E-03   0.26811E+09 
c  alpha        0.99102E+02     119   0.97076E-05   0.14485E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -7.3677                           350
a  R22               -1.0215                           113
a  R33            4.2091e-25                            31
a  R12               -11.324                           921
a  R13           -1.6731e-06                           319
a  R23           -3.0347e-06                            74
a  Dissip            -2689.1                           784
a  alpha                              1.0007                       11716
a  LocalTime      5.8279e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2561.7          357.93         -903.32         -773.29
v  Velocity[x]            -55.468          109.33           32.59          62.502
v  Velocity[y]            -22.638          19.388        0.018148         0.14338
v  Velocity[z]        -2.1425e-05      1.1171e-05     -8.2194e-08      5.0366e-10
v  R11                      1e-24           153.7          5.9343           11.78
v  R22                      1e-24          44.154          2.9387          5.5643
v  R33                      1e-24          75.108          3.6004          6.8745
v  R12                    -11.324          35.367         -1.8125         -1.7043
v  R13                -1.6731e-06      1.1526e-05      3.1159e-08      1.8674e-09
v  R23                -3.0347e-06      3.4327e-06      1.1651e-08      8.5808e-10
v  Dissip                0.011635      1.3967e+05          555.32          2314.7
v  alpha                0.0012089               1         0.79406          0.9939
v  TurbVisc            1.1221e-53          27.386         0.02461        0.055533
v  CourantNb             0.043215          583.85          52.668          70.863
v  FourierNb             0.014096      1.7159e+05          731.72           168.2
v  total_pressure           98763      1.0168e+05      1.0042e+05      1.0055e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.0443      1.7162e+05          784.39          239.07


 TIME FOR THE TIME STEP               18:        0.46333E+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         0.294668821E+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   :  0.19650E+00 0.51524E+01
   Friction velocity        uk    :  0.19650E+00 0.51524E+01
   Dimensionless distance   yplus :  0.69942E-01 0.19517E+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         68 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.54715E-02     546   0.75924E-03   0.15104E+00 
c  VelocityX    0.27603E+01     400   0.10392E-01   0.31199E+03 
c  VelocityY    0.27603E+01     400   0.10392E-01   0.18866E+02 
c  VelocityZ    0.27603E+01     400   0.10392E-01   0.77587E-11 
c  R11          0.83117E+01    8884   0.19999E-01   0.25049E+03 
c  R22          0.27107E+01    8134   0.39407E-01   0.34097E+02 
c  R33          0.42204E+01    8282   0.31321E-01   0.65112E+02 
c  R12          0.20757E+01   10000   0.43232E-01   0.17048E+02 
c  R13          0.10124E-06   10000   0.64751E+00   0.15558E-11 
c  R23          0.35760E-07   10000   0.73649E+00   0.81406E-12 
c  Dissip       0.66881E+04    5735   0.48709E-03   0.32597E+09 
c  alpha        0.96744E+02     130   0.98874E-05   0.74399E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11             -0.028585                            41
a  R22              -0.40779                            51
a  R33             4.204e-25                            29
a  R12               -11.725                           292
a  R13           -7.0649e-06                            12
a  R23           -5.8904e-06                            20
a  Dissip            -582.59                           890
a  alpha                              1.0018                       10592
a  LocalTime      5.7626e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2528.9          413.26         -888.98         -757.38
v  Velocity[x]             -57.45          111.82          31.888          62.502
v  Velocity[y]            -24.131          21.431        0.019327         0.15466
v  Velocity[z]        -1.3725e-05      2.7117e-05     -7.6871e-08       1.304e-09
v  R11                      1e-24          164.02          6.1066          12.322
v  R22                      1e-24          46.655          3.0118           5.794
v  R33                      1e-24          80.088          3.6946          7.1619
v  R12                    -11.725          37.128         -1.8397         -1.6488
v  R13                -7.0649e-06       4.013e-06      -2.154e-08     -2.3306e-09
v  R23                -5.8904e-06      1.1004e-05      1.8782e-08      3.1139e-09
v  Dissip               0.0096987      1.5966e+05          570.52          2585.8
v  alpha                0.0011673               1         0.78685         0.99329
v  TurbVisc            9.9065e-54          6.4939        0.023627        0.048124
v  CourantNb             0.058113          598.92          53.472          71.196
v  FourierNb             0.014096      1.7353e+06          973.84          177.89
v  total_pressure           98796      1.0174e+05      1.0044e+05      1.0057e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9148      1.7353e+06          1027.3          249.08


 TIME FOR THE TIME STEP               19:        0.53884E+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         0.294670123E+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   :  0.18144E+00 0.52815E+01
   Friction velocity        uk    :  0.18144E+00 0.52815E+01
   Dimensionless distance   yplus :  0.74236E-01 0.19751E+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         73 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57805E-02     510   0.81893E-03   0.15462E+00 
c  VelocityX    0.27622E+01     401   0.10816E-01   0.36193E+03 
c  VelocityY    0.27622E+01     401   0.10816E-01   0.21338E+02 
c  VelocityZ    0.27622E+01     401   0.10816E-01   0.12584E-10 
c  R11          0.93184E+01   10000   0.17534E-01   0.27531E+03 
c  R22          0.30614E+01   10000   0.33734E-01   0.39958E+02 
c  R33          0.47355E+01   10000   0.27447E-01   0.71849E+02 
c  R12          0.23447E+01   10000   0.39131E-01   0.20041E+02 
c  R13          0.17452E-06   10000   0.41494E+00   0.31238E-11 
c  R23          0.12394E-06   10000   0.31871E+00   0.10460E-11 
c  Dissip       0.76170E+04   10000   0.58351E-03   0.39719E+09 
c  alpha        0.94792E+02     141   0.99550E-05   0.10285E-01 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -1.1363                           197
a  R22              -0.18589                           242
a  R33            -0.0028728                            27
a  R12               -12.048                           457
a  R13           -3.6398e-06                           173
a  R23           -5.0788e-06                           214
a  Dissip            -425.22                           283
a  alpha                               1.002                       10960
a  LocalTime      1.3177e-08                         89999


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2501.6          471.38         -877.48         -744.28
v  Velocity[x]            -59.189          114.46          31.356          62.503
v  Velocity[y]            -25.669          23.677        0.022366         0.17144
v  Velocity[z]        -1.6539e-05      2.4931e-05     -1.1102e-07      1.5568e-09
v  R11                      1e-24          174.21          6.3152          12.881
v  R22                      1e-24          48.955           3.078          6.0353
v  R33                      1e-24          84.872          3.8046          7.4593
v  R12                    -12.048          40.629          -1.861         -1.5708
v  R13                -3.6398e-06      1.3485e-05       2.485e-08      4.4025e-09
v  R23                -5.0788e-06      9.5461e-06     -1.3847e-08     -1.1153e-09
v  Dissip               0.0080843      1.8159e+05          677.21          2892.6
v  alpha                0.0011405               1         0.77533         0.99212
v  TurbVisc            8.7998e-54          182.51        0.027514        0.068819
v  CourantNb             0.058111          607.23          54.379          71.616
v  FourierNb             0.014096      7.5891e+06          1617.8          219.71
v  total_pressure           98823       1.018e+05      1.0045e+05      1.0058e+05
v  LocalTime                 0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4523      7.5891e+06          1672.2          291.32


 TIME FOR THE TIME STEP               20:        0.61063E+02

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


 INSTANT    0.210000000E+01   TIME STEP NUMBER              21
 ============================================================= 




   ** 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         0.294671749E+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   :  0.15435E+00 0.52126E+01
   Friction velocity        uk    :  0.15435E+00 0.52126E+01
   Dimensionless distance   yplus :  0.55076E-01 0.20000E+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         77 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64416E-02     510   0.88379E-03   0.16596E+00 
c  VelocityX    0.27644E+01     405   0.11547E-01   0.42297E+03 
c  VelocityY    0.27644E+01     405   0.11547E-01   0.23886E+02 
c  VelocityZ    0.27644E+01     405   0.11547E-01   0.92221E-11 
c  R11          0.10416E+02    8632   0.15269E-01   0.31376E+03 
c  R22          0.34564E+01   10000   0.30359E-01   0.48981E+02 
c  R33          0.52993E+01    9316   0.24241E-01   0.81706E+02 
c  R12          0.26477E+01   10000   0.33301E-01   0.24830E+02 
c  R13          0.28301E-06    5868   0.11682E+00   0.23896E-11 
c  R23          0.24830E-07    8287   0.11535E+01   0.20850E-11 
c  Dissip       0.86477E+04    2408   0.71218E-03   0.48283E+09 
c  alpha        0.93765E+02     128   0.97495E-05   0.27068E-01 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -3.3273                           749
a  R22               -1.1985                           120
a  R33              -0.58152                            62
a  R12               -12.271                          1026
a  R13           -1.2274e-05                           723
a  R23           -9.6877e-06                            94
a  Dissip            -4021.8                          1353
a  alpha                              1.0012                       13117
a  LocalTime      1.4455e-06                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2592.3          532.88         -867.61         -732.95
v  Velocity[x]            -60.743          117.17          30.983          62.503
v  Velocity[y]            -27.337           26.08         0.02797         0.19568
v  Velocity[z]          -2.32e-05      2.7431e-05     -7.1925e-08      1.1576e-09
v  R11                      1e-24          184.14          6.3569          13.448
v  R22                      1e-24          51.156          3.1153           6.306
v  R33                      1e-24          89.463          3.8282          7.7619
v  R12                    -12.271          47.064         -1.7966         -1.4706
v  R13                 -1.074e-05      5.5258e-06     -4.5268e-09      1.0429e-10
v  R23                -9.3722e-06      1.0877e-05     -3.7274e-08     -2.3491e-09
v  Dissip               0.0067384      2.0571e+05          738.19          3223.8
v  alpha                0.0011336               1          0.7964         0.99402
v  TurbVisc            7.8492e-54          17.717        0.026566        0.065185
v  CourantNb             0.061451          593.37          55.365          72.107
v  FourierNb             0.014096           69180          735.34          170.61
v  total_pressure           98733      1.0186e+05      1.0046e+05      1.0059e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5664           69198          790.71          242.71


 TIME FOR THE TIME STEP               21:        0.48653E+02

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


 INSTANT    0.220000000E+01   TIME STEP NUMBER              22
 ============================================================= 




   ** 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         0.294673492E+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   :  0.18284E+00 0.49495E+01
   Friction velocity        uk    :  0.18284E+00 0.49495E+01
   Dimensionless distance   yplus :  0.76031E-01 0.20269E+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         82 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.64799E-02     492   0.93404E-03   0.16044E+00 
c  VelocityX    0.27667E+01     414   0.12380E-01   0.52077E+03 
c  VelocityY    0.27667E+01     414   0.12380E-01   0.27867E+02 
c  VelocityZ    0.27667E+01     414   0.12380E-01   0.41966E-10 
c  R11          0.11614E+02    8904   0.15448E-01   0.39805E+03 
c  R22          0.39059E+01   10000   0.34539E-01   0.63798E+02 
c  R33          0.59181E+01   10000   0.24402E-01   0.10257E+03 
c  R12          0.29905E+01   10000   0.33154E-01   0.31886E+02 
c  R13          0.53029E-04    4289   0.38519E-03   0.11843E-11 
c  R23          0.33745E-06    6563   0.48910E-01   0.15868E-11 
c  Dissip       0.97964E+04    3385   0.89835E-03   0.59637E+09 
c  alpha        0.92388E+02     126   0.97037E-05   0.29613E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -5.9736                           342
a  R22              -0.91104                           237
a  R33               -1.1519                           196
a  R12               -12.402                           535
a  R13           -1.3163e-05                           292
a  R23           -8.0908e-06                           184
a  Dissip            -9299.5                          2676
a  alpha                              1.0011                       12213
a  LocalTime      2.4165e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2779.1          597.63         -857.33         -721.64
v  Velocity[x]            -62.473          119.83          30.595          62.503
v  Velocity[y]            -29.182           28.54        0.036403         0.22786
v  Velocity[z]        -2.0575e-05      4.0269e-05      5.3303e-08      2.3321e-10
v  R11                      1e-24          193.88          6.5945          14.108
v  R22                      1e-24          59.389          3.1958           6.621
v  R33                      1e-24          93.924           3.939          8.1129
v  R12                    -12.402          54.517         -1.8071          -1.371
v  R13                -1.3163e-05       3.643e-06     -2.5182e-08     -1.8693e-09
v  R23                -8.0908e-06      1.2851e-05     -1.0538e-08     -8.8913e-10
v  Dissip              0.00010385      2.3193e+05          803.19          3607.8
v  alpha                0.0011397               1          0.7913         0.99364
v  TurbVisc             7.046e-54          88.663        0.031745        0.091422
v  CourantNb             0.059626          560.76          56.417          72.649
v  FourierNb             0.014096      4.1382e+05          856.94          196.49
v  total_pressure           98546      1.0192e+05      1.0047e+05       1.006e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.1464      4.1386e+05          913.36          269.14


 TIME FOR THE TIME STEP               22:        0.47967E+02

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


 INSTANT    0.230000000E+01   TIME STEP NUMBER              23
 ============================================================= 




   ** 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         0.294673687E+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   :  0.58190E-01 0.48004E+01
   Friction velocity        uk    :  0.58190E-01 0.48004E+01
   Dimensionless distance   yplus :  0.20800E-01 0.20561E+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         86 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67073E-02     528   0.95390E-03   0.15868E+00 
c  VelocityX    0.27694E+01     439   0.15211E-01   0.72288E+03 
c  VelocityY    0.27694E+01     439   0.15211E-01   0.38965E+02 
c  VelocityZ    0.27694E+01     439   0.15211E-01   0.41554E-10 
c  R11          0.12929E+02    7373   0.15607E-01   0.49592E+03 
c  R22          0.44527E+01    9499   0.47591E-01   0.81802E+02 
c  R33          0.66064E+01    8381   0.23331E-01   0.12793E+03 
c  R12          0.33911E+01    9115   0.31692E-01   0.41331E+02 
c  R13          0.18360E-03    1576   0.30980E-03   0.21828E-11 
c  R23          0.17795E-05    4722   0.21985E-01   0.25557E-11 
c  Dissip       0.11079E+05    6932   0.62097E-02   0.74783E+09 
c  alpha        0.92743E+02     118   0.98622E-05   0.14372E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11             -0.092357                           152
a  R22           -2.6681e-05                           156
a  R33           -0.00084161                           140
a  R12               -15.083                           289
a  R13           -5.2392e-06                            22
a  R23           -6.1526e-06                            10
a  Dissip            -850.93                           972
a  alpha                              1.0006                       10083
a  LocalTime      2.9864e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2960.8          668.19          -842.7         -706.76
v  Velocity[x]            -64.074          122.29          30.405          62.503
v  Velocity[y]            -31.122          31.109        0.047875         0.26806
v  Velocity[z]        -4.8155e-05      5.6563e-05      1.2688e-07     -4.2841e-11
v  R11                      1e-24          203.16          6.8517          14.812
v  R22                      1e-24          69.294          3.3103          6.9705
v  R33                      1e-24           98.14           4.077          8.4968
v  R12                    -15.083           62.82         -1.8568         -1.2682
v  R13                -5.2392e-06      1.1607e-05      2.0834e-08      1.4949e-09
v  R23                -6.1526e-06       1.351e-05     -6.1847e-09     -1.1331e-09
v  Dissip               0.0046823      2.6009e+05          890.31          4054.9
v  alpha                0.0011972               1         0.79177         0.99357
v  TurbVisc            6.3553e-54          255.93        0.036002         0.11265
v  CourantNb             0.070052          594.74          57.256          73.225
v  FourierNb             0.014096      3.3485e+05          886.94          206.79
v  total_pressure           98364      1.0199e+05      1.0048e+05      1.0062e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.4335      3.3489e+05          944.19          280.02


 TIME FOR THE TIME STEP               23:        0.43277E+02

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


 INSTANT    0.240000000E+01   TIME STEP NUMBER              24
 ============================================================= 




   ** 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         0.294674532E+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   :  0.12142E+00 0.58836E+01
   Friction velocity        uk    :  0.12142E+00 0.58836E+01
   Dimensionless distance   yplus :  0.52192E-01 0.20867E+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         89 outlet faces on        225


 Write intermediate restart files
   checkpoint at iteration         24, Physical time    0.24000E+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:    0.53607E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.79952E-02     546   0.97767E-03   0.17936E+00 
c  VelocityX    0.27722E+01     430   0.16233E-01   0.11949E+04 
c  VelocityY    0.27722E+01     430   0.16233E-01   0.71959E+02 
c  VelocityZ    0.27722E+01     430   0.16233E-01   0.66269E-10 
c  R11          0.14345E+02   10000   0.13610E-01   0.67872E+03 
c  R22          0.50065E+01   10000   0.37475E-01   0.11207E+03 
c  R33          0.73492E+01   10000   0.20259E-01   0.17281E+03 
c  R12          0.38356E+01   10000   0.28565E-01   0.58448E+02 
c  R13          0.48012E-05    9906   0.32175E-01   0.57113E-11 
c  R23          0.13581E-06   10000   0.43760E+00   0.21823E-11 
c  Dissip       0.12512E+05   10000   0.16463E-02   0.97021E+09 
c  alpha        0.97351E+02     127   0.98907E-05   0.65030E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -3.2132                           113
a  R22               -5.5167                           369
a  R33              -0.28935                            53
a  R12                -17.62                           369
a  R13           -1.7493e-05                            93
a  R23           -9.6944e-06                           186
a  Dissip            -4125.7                           807
a  alpha                              1.0006                        9812
a  LocalTime      1.1282e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -3095.9          745.47         -819.42         -684.74
v  Velocity[x]            -64.415           124.3          30.647          62.502
v  Velocity[y]            -33.034          33.655        0.062851         0.31692
v  Velocity[z]        -4.1139e-05      4.6947e-05      1.1653e-07     -2.7864e-12
v  R11                      1e-24          212.07          7.1195          15.589
v  R22                      1e-24          80.662          3.4398          7.3907
v  R33                      1e-24          102.18          4.2347          8.9358
v  R12                     -17.62          72.173         -1.8557         -1.1267
v  R13                -1.7493e-05      6.5528e-06     -5.5363e-08     -2.0658e-09
v  R23                -9.6944e-06      1.2264e-05      -6.023e-09     -3.2579e-10
v  Dissip               0.0039031      3.0676e+05          1074.8            4593
v  alpha                0.0013566               1         0.78603         0.99278
v  TurbVisc            5.7665e-54          211.34        0.042887          0.1375
v  CourantNb              0.05785          750.12          58.059          73.836
v  FourierNb             0.014096      8.8635e+06          1874.3           287.6
v  total_pressure           98229      1.0207e+05      1.0051e+05      1.0064e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5923      8.8636e+06          1932.3          361.44


 TIME FOR THE TIME STEP               24:        0.62241E+02

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


 INSTANT    0.250000000E+01   TIME STEP NUMBER              25
 ============================================================= 




   ** 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         0.294673810E+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   :  0.23713E+00 0.74098E+01
   Friction velocity        uk    :  0.23713E+00 0.74098E+01
   Dimensionless distance   yplus :  0.84496E-01 0.21229E+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         93 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.87813E-02     582   0.11670E-02   0.18571E+00 
c  VelocityX    0.27753E+01     405   0.20704E-01   0.20494E+04 
c  VelocityY    0.27753E+01     405   0.20704E-01   0.17429E+03 
c  VelocityZ    0.27753E+01     405   0.20704E-01   0.60581E-10 
c  R11          0.15903E+02    5579   0.11788E-01   0.86589E+03 
c  R22          0.56666E+01    6097   0.20392E-01   0.14083E+03 
c  R33          0.81771E+01    5940   0.16587E-01   0.22243E+03 
c  R12          0.43575E+01    6605   0.21588E-01   0.82114E+02 
c  R13          0.25352E-05    5000   0.21661E-01   0.60631E-11 
c  R23          0.44876E-07    7872   0.81721E+00   0.39787E-11 
c  Dissip       0.14149E+05    2324   0.76260E-02   0.12888E+10 
c  alpha        0.93993E+02     144   0.98895E-05   0.14700E-01 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -10.777                           574
a  R22               -15.239                           336
a  R33               -2.2383                           169
a  R12               -17.884                           809
a  R13           -1.6052e-05                           534
a  R23           -1.2294e-05                           192
a  Dissip            -9214.1                          2540
a  alpha                              1.0006                       12629
a  LocalTime      7.1184e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -3118.2          830.17         -781.63         -650.84
v  Velocity[x]            -60.062          126.12          31.137            62.5
v  Velocity[y]            -35.135          36.288        0.082585         0.37692
v  Velocity[z]        -7.2009e-05      6.3635e-05      6.0997e-08     -1.3126e-09
v  R11                      1e-24          220.73          7.1629          16.311
v  R22                      1e-24          93.577          3.5201          7.8203
v  R33                      1e-24          113.72          4.2914          9.3704
v  R12                    -17.884          82.774         -1.7564        -0.96724
v  R13                -1.6052e-05      1.3695e-05      -3.632e-08     -1.6429e-09
v  R23                -1.2294e-05      1.3278e-05      4.3767e-08      3.5741e-09
v  Dissip               0.0032524      3.6624e+05          1236.8          5218.9
v  alpha                0.0013481               1         0.80586         0.99446
v  TurbVisc            5.2748e-54           570.1        0.041398         0.14463
v  CourantNb             0.073814          874.37          59.324          74.495
v  FourierNb             0.014096      1.4048e+06           789.7          197.16
v  total_pressure           98207      1.0216e+05      1.0054e+05      1.0067e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           4.535      1.4048e+06          849.02          271.65


 TIME FOR THE TIME STEP               25:        0.36539E+02

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


 INSTANT    0.260000000E+01   TIME STEP NUMBER              26
 ============================================================= 




   ** 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         0.294673238E+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   :  0.19359E+00 0.92210E+01
   Friction velocity        uk    :  0.19359E+00 0.92210E+01
   Dimensionless distance   yplus :  0.87509E-01 0.21616E+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         97 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.93439E-02     636   0.16604E-02   0.18659E+00 
c  VelocityX    0.27785E+01     477   0.23431E-01   0.23333E+04 
c  VelocityY    0.27785E+01     477   0.23431E-01   0.32040E+03 
c  VelocityZ    0.27785E+01     477   0.23431E-01   0.11419E-09 
c  R11          0.17637E+02   10000   0.16091E-01   0.95024E+03 
c  R22          0.64953E+01   10000   0.44059E-01   0.17542E+03 
c  R33          0.91959E+01   10000   0.92772E-01   0.25065E+03 
c  R12          0.49885E+01   10000   0.30793E-01   0.11983E+03 
c  R13          0.69583E-04    4428   0.97156E-03   0.42544E-11 
c  R23          0.92818E-06    9144   0.26175E+00   0.83891E-11 
c  Dissip       0.16065E+05   10000   0.18187E-02   0.16396E+10 
c  alpha        0.11424E+03     118   0.99268E-05   0.32441E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -10.706                           366
a  R22               -6.0964                           432
a  R33               -2.0094                           207
a  R12               -16.009                           559
a  R13           -2.4943e-05                           252
a  R23           -2.3905e-05                           131
a  Dissip            -3663.5                          1500
a  alpha                              1.0007                       11716
a  LocalTime      3.4513e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -3022.3          935.69         -721.11         -597.43
v  Velocity[x]            -56.451          128.93          31.261          62.498
v  Velocity[y]            -37.141          41.796         0.10743         0.44904
v  Velocity[z]        -6.8138e-05      7.3546e-05      -1.443e-07     -1.6536e-09
v  R11                      1e-24          232.59          7.3262          16.851
v  R22                      1e-24          108.18          3.6315          8.2314
v  R33                      1e-24          129.25          4.3844          9.7481
v  R12                    -16.009          94.531          -1.722        -0.77634
v  R13                -2.4943e-05      1.6481e-05     -1.2727e-08      2.9392e-10
v  R23                -2.3905e-05      1.7381e-05     -1.6566e-08     -3.8244e-09
v  Dissip               0.0027091      4.3879e+05          1336.9          5801.7
v  alpha                0.0013053               1         0.79947         0.99403
v  TurbVisc            4.8628e-54          273.65        0.044724         0.14069
v  CourantNb              0.16598           945.7          60.355          75.069
v  FourierNb             0.014096      2.8975e+06          1064.5          245.74
v  total_pressure           98303      1.0226e+05       1.006e+05      1.0073e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.4458      2.8976e+06          1124.8          320.81


 TIME FOR THE TIME STEP               26:        0.56217E+02

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


 INSTANT    0.270000000E+01   TIME STEP NUMBER              27
 ============================================================= 




   ** 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         0.294672830E+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   :  0.35518E+00 0.10708E+02
   Friction velocity        uk    :  0.35518E+00 0.10708E+02
   Dimensionless distance   yplus :  0.12727E+00 0.22021E+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        102 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.10222E-01     636   0.21783E-02   0.19324E+00 
c  VelocityX    0.27819E+01     491   0.26111E-01   0.19701E+04 
c  VelocityY    0.27819E+01     491   0.26111E-01   0.37887E+03 
c  VelocityZ    0.27819E+01     491   0.26111E-01   0.27185E-09 
c  R11          0.19521E+02    8876   0.11234E-01   0.12811E+04 
c  R22          0.73980E+01    9746   0.17970E-01   0.24529E+03 
c  R33          0.10158E+02   10000   0.14495E-01   0.33590E+03 
c  R12          0.57102E+01    9664   0.17982E-01   0.16397E+03 
c  R13          0.21160E-04    3447   0.22833E-02   0.10187E-10 
c  R23          0.10298E-06   10000   0.45660E+00   0.81302E-11 
c  Dissip       0.18401E+05    4978   0.10559E-01   0.24602E+10 
c  alpha        0.94038E+02     121   0.98997E-05   0.21318E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -4.8393                           363
a  R22               -4.3011                           348
a  R33              -0.64284                           199
a  R12               -17.326                           690
a  R13           -3.3214e-05                           180
a  R23           -2.2134e-05                            76
a  Dissip            -2805.2                          2468
a  alpha                              1.0008                       10256
a  LocalTime      1.3549e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2913.5          1069.6         -638.48         -524.54
v  Velocity[x]             -53.14          132.41          31.228          62.497
v  Velocity[y]            -38.887          51.755         0.13619         0.52847
v  Velocity[z]        -0.00010844      0.00015218     -3.0423e-08      8.9309e-10
v  R11                      1e-24           261.2          7.2813          17.264
v  R22                      1e-24          124.39          3.7022          8.5883
v  R33                      1e-24          146.17          4.4139          10.072
v  R12                    -17.326          107.43         -1.7284        -0.59506
v  R13                -3.3214e-05       1.229e-05     -9.0253e-08     -3.2245e-09
v  R23                -2.2134e-05      2.7628e-05      5.1116e-08       3.573e-09
v  Dissip               0.0022564      5.2248e+05          1365.4            6422
v  alpha                0.0012518               1         0.80234         0.99415
v  TurbVisc            4.4958e-54          292.27        0.039858          0.1319
v  CourantNb              0.22597          881.47          60.473          75.579
v  FourierNb             0.014283      7.3807e+05          957.68          217.03
v  total_pressure           98411      1.0239e+05      1.0069e+05       1.008e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.1865       7.381e+05          1018.1          292.61


 TIME FOR THE TIME STEP               27:        0.50809E+02

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


 INSTANT    0.280000000E+01   TIME STEP NUMBER              28
 ============================================================= 




   ** 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         0.294676327E+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   :  0.33720E+00 0.10800E+02
   Friction velocity        uk    :  0.33720E+00 0.10800E+02
   Dimensionless distance   yplus :  0.12241E+00 0.22431E+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        110 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.11020E-01     654   0.24756E-02   0.19583E+00 
c  VelocityX    0.27861E+01     499   0.28732E-01   0.17683E+04 
c  VelocityY    0.27861E+01     499   0.28732E-01   0.40648E+03 
c  VelocityZ    0.27861E+01     499   0.28732E-01   0.29403E-09 
c  R11          0.21562E+02   10000   0.10379E-01   0.13405E+04 
c  R22          0.84747E+01   10000   0.18706E-01   0.31765E+03 
c  R33          0.11314E+02   10000   0.13418E-01   0.37473E+03 
c  R12          0.65420E+01   10000   0.19146E-01   0.21350E+03 
c  R13          0.77681E-06   10000   0.48834E+00   0.17817E-10 
c  R23          0.25366E-06   10000   0.95456E+00   0.13878E-10 
c  Dissip       0.21138E+05    8581   0.92376E-02   0.27725E+10 
c  alpha        0.10402E+03     141   0.99123E-05   0.17615E-01 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -5.4693                           142
a  R22                -4.038                           467
a  R33                -1.107                           102
a  R12               -19.568                           522
a  R13           -1.6399e-05                            56
a  R23           -3.1503e-05                            84
a  Dissip             -18112                           831
a  alpha                              1.0015                       11104
a  LocalTime      1.0664e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2791.3            1217         -545.09         -442.56
v  Velocity[x]            -51.647          135.64           31.34          62.496
v  Velocity[y]            -40.381          52.401         0.16776         0.61719
v  Velocity[z]        -0.00012943      0.00016661      6.3617e-08      4.2589e-09
v  R11                      1e-24          291.68           7.295          17.671
v  R22                      1e-24          142.25          3.7303           8.834
v  R33                      1e-24          164.17          4.4609          10.372
v  R12                    -19.568          121.01         -1.7246        -0.49871
v  R13                -1.6399e-05      4.9377e-05     -4.2182e-08     -2.4115e-09
v  R23                -3.1503e-05      1.9101e-05      9.5551e-08       7.434e-09
v  Dissip               0.0018799      6.1446e+05          1417.2          6933.6
v  alpha                0.0011744               1         0.78649         0.99242
v  TurbVisc            4.2037e-54          61.108        0.037105        0.099347
v  CourantNb              0.22977          762.76          60.427          76.046
v  FourierNb             0.014852      9.3775e+05          1403.1          248.48
v  total_pressure           98534      1.0254e+05      1.0078e+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          3.7471      9.3779e+05          1463.5          324.53


 TIME FOR THE TIME STEP               28:        0.60384E+02

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


 INSTANT    0.290000000E+01   TIME STEP NUMBER              29
 ============================================================= 




   ** 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         0.294677342E+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   :  0.35602E+00 0.10198E+02
   Friction velocity        uk    :  0.35602E+00 0.10198E+02
   Dimensionless distance   yplus :  0.14896E+00 0.22856E+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        119 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.10825E-01     636   0.26187E-02   0.18445E+00 
c  VelocityX    0.27904E+01     525   0.30606E-01   0.18646E+04 
c  VelocityY    0.27904E+01     525   0.30606E-01   0.47433E+03 
c  VelocityZ    0.27904E+01     525   0.30606E-01   0.47190E-09 
c  R11          0.23792E+02    5691   0.70728E-02   0.17809E+04 
c  R22          0.97075E+01    6287   0.10671E-01   0.45092E+03 
c  R33          0.12590E+02    6391   0.10143E-01   0.49844E+03 
c  R12          0.74679E+01    6707   0.12550E-01   0.25881E+03 
c  R13          0.15696E-05    6289   0.26735E+00   0.40011E-10 
c  R23          0.16146E-06    8394   0.20673E+01   0.30621E-10 
c  Dissip       0.24371E+05    2416   0.31817E-02   0.34558E+10 
c  alpha        0.97959E+02     133   0.95358E-05   0.19288E-01 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -5.2326                           737
a  R22               -18.703                           445
a  R33                -1.803                           206
a  R12               -17.711                           775
a  R13           -4.3282e-05                           554
a  R23            -4.262e-05                           114
a  Dissip            -4318.4                          1483
a  alpha                              1.0014                       12063
a  LocalTime      7.9284e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2674.7            1363         -446.92         -356.64
v  Velocity[x]            -51.289          138.48          31.613          62.495
v  Velocity[y]            -40.629          48.975          0.1975         0.70189
v  Velocity[z]        -0.00022727      0.00011634      -2.512e-07      2.9789e-09
v  R11                      1e-24          320.91          7.2817          18.343
v  R22                      1e-24          159.95          3.7547          9.1969
v  R33                      1e-24          182.37           4.468           10.79
v  R12                    -17.711          134.31         -1.6384        -0.29818
v  R13                -4.3282e-05      4.3623e-05     -4.8372e-08       8.088e-10
v  R23                 -4.262e-05      4.0082e-05     -1.9663e-08     -8.4246e-11
v  Dissip               0.0015669      7.0401e+05          1534.9          7710.9
v  alpha                0.0011293               1         0.80226         0.99402
v  TurbVisc            3.8865e-54           273.5        0.032097        0.095667
v  CourantNb               0.2116          631.91          60.699          76.518
v  FourierNb             0.014852      1.2613e+06          908.42          190.77
v  total_pressure           98650      1.0269e+05      1.0088e+05      1.0097e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.5964      1.2613e+06          969.12          267.29


 TIME FOR THE TIME STEP               29:        0.39401E+02

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


 INSTANT    0.300000000E+01   TIME STEP NUMBER              30
 ============================================================= 




   ** 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         0.294671370E+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   :  0.35646E+00 0.97665E+01
   Friction velocity        uk    :  0.35646E+00 0.97665E+01
   Dimensionless distance   yplus :  0.17933E+00 0.23286E+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        129 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.11135E-01     618   0.26288E-02   0.17995E+00 
c  VelocityX    0.27950E+01     504   0.30862E-01   0.20805E+04 
c  VelocityY    0.27950E+01     504   0.30862E-01   0.53466E+03 
c  VelocityZ    0.27950E+01     504   0.30862E-01   0.57990E-09 
c  R11          0.26014E+02   10000   0.67718E-02   0.16021E+04 
c  R22          0.10969E+02   10000   0.10509E-01   0.47453E+03 
c  R33          0.13890E+02   10000   0.94658E-02   0.42745E+03 
c  R12          0.84109E+01   10000   0.12169E-01   0.27703E+03 
c  R13          0.55558E-05   10000   0.31145E-01   0.53496E-10 
c  R23          0.13587E-06   10000   0.60563E+00   0.27064E-10 
c  Dissip       0.27692E+05    8837   0.43807E-02   0.35220E+10 
c  alpha        0.99340E+02     131   0.10001E-04   0.67088E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -4.6255                           450
a  R22               -6.2113                           582
a  R33               -1.2003                           281
a  R12               -16.754                           660
a  R13           -0.00011439                           203
a  R23           -7.4013e-05                           122
a  Dissip             -18890                          1320
a  alpha                              1.0011                       11873
a  LocalTime      1.2556e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2559.5          1502.1          -344.8         -267.18
v  Velocity[x]            -50.566          139.72          31.922          62.495
v  Velocity[y]            -40.845          48.931          0.2274         0.79376
v  Velocity[z]        -0.00024933       0.0001771     -3.3732e-07      3.9696e-10
v  R11                      1e-24          349.72          7.4221          18.839
v  R22                      1e-24          178.42          3.7623          9.3364
v  R33                      1e-24          200.34          4.5136          11.088
v  R12                    -16.754          147.23         -1.6137        -0.17331
v  R13                -0.00011439      0.00010101      3.1513e-09     -1.8852e-09
v  R23                -7.2985e-05      3.6366e-05      3.2492e-08      4.6133e-09
v  Dissip               0.0013074      7.8857e+05          1612.8          8256.4
v  alpha                 0.001103               1         0.79995         0.99382
v  TurbVisc            3.6782e-54          197.91        0.031709        0.085551
v  CourantNb              0.20715          553.05          61.744          77.055
v  FourierNb             0.014852       7.964e+05          878.35          200.64
v  total_pressure           98766      1.0283e+05      1.0098e+05      1.0106e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          5.1919      7.9645e+05          940.09           277.7


 TIME FOR THE TIME STEP               30:        0.60713E+02

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


 INSTANT    0.310000000E+01   TIME STEP NUMBER              31
 ============================================================= 




   ** 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         0.294670592E+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   :  0.35691E+00 0.93784E+01
   Friction velocity        uk    :  0.35691E+00 0.93784E+01
   Dimensionless distance   yplus :  0.18790E+00 0.23670E+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        135 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.11383E-01     627   0.26692E-02   0.18084E+00 
c  VelocityX    0.27990E+01     486   0.31222E-01   0.22968E+04 
c  VelocityY    0.27990E+01     486   0.31222E-01   0.58580E+03 
c  VelocityZ    0.27990E+01     486   0.31222E-01   0.10236E-08 
c  R11          0.28340E+02    7412   0.86055E-02   0.39808E+04 
c  R22          0.12601E+02    7967   0.23495E-01   0.10366E+04 
c  R33          0.15284E+02    8225   0.13328E-01   0.11786E+04 
c  R12          0.94970E+01    6283   0.24437E-01   0.46822E+03 
c  R13          0.10909E-05    5467   0.17456E+00   0.49162E-10 
c  R23          0.11305E-06    6812   0.10657E+01   0.50199E-10 
c  Dissip       0.31121E+05    1352   0.11057E-01   0.71921E+10 
c  alpha        0.12881E+03     122   0.97872E-05   0.44952E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -4.5497                           358
a  R22               -26.451                           521
a  R33               -1.2907                           295
a  R12               -17.053                           417
a  R13            -5.344e-05                           133
a  R23           -7.0962e-05                           133
a  Dissip             -10635                          3163
a  alpha                              1.0014                       11554
a  LocalTime       1.686e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2454.1          1626.9         -241.65         -176.03
v  Velocity[x]            -49.335          141.11          32.381          62.495
v  Velocity[y]            -40.121          51.123         0.25642         0.87809
v  Velocity[z]        -0.00020278      0.00026019     -2.7849e-07      3.4252e-09
v  R11                      1e-24           374.1          7.5886          19.819
v  R22                      1e-24          193.32          3.8339          9.7584
v  R33                      1e-24          215.84          4.6117          11.681
v  R12                    -17.053          158.27         -1.6317        0.033036
v  R13                 -5.344e-05      2.9642e-05      7.0245e-08      4.7814e-09
v  R23                -7.0962e-05       6.911e-05      9.7497e-08      7.3784e-09
v  Dissip               0.0010941      8.4415e+05          1787.6          9485.8
v  alpha                0.0010997               1         0.80496         0.99404
v  TurbVisc            3.4672e-54          236.34        0.035476         0.10565
v  CourantNb              0.24727          465.03          62.871          77.613
v  FourierNb             0.014852      5.9313e+05          841.64          203.18
v  total_pressure           98871      1.0295e+05      1.0108e+05      1.0115e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.2733      5.9315e+05          904.51          280.79


 TIME FOR THE TIME STEP               31:        0.40245E+02

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


 INSTANT    0.320000000E+01   TIME STEP NUMBER              32
 ============================================================= 




   ** 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         0.294659455E+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   :  0.35737E+00 0.90264E+01
   Friction velocity        uk    :  0.35737E+00 0.90264E+01
   Dimensionless distance   yplus :  0.14220E+00 0.24038E+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        137 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.15677E-01     633   0.24407E-02   0.22693E+00 
c  VelocityX    0.28037E+01     488   0.29194E-01   0.24208E+04 
c  VelocityY    0.28037E+01     488   0.29194E-01   0.67255E+03 
c  VelocityZ    0.28037E+01     488   0.29194E-01   0.23272E-08 
c  R11          0.31240E+02   10000   0.14291E-01   0.34523E+04 
c  R22          0.15614E+02   10000   0.11430E+00   0.12332E+04 
c  R33          0.17035E+02   10000   0.10803E-01   0.81420E+03 
c  R12          0.10676E+02   10000   0.28354E-01   0.59474E+03 
c  R13          0.16484E-03   10000   0.33583E-02   0.55674E-10 
c  R23          0.25097E-05   10000   0.16997E+00   0.43044E-10 
c  Dissip       0.33809E+05    7348   0.48572E-01   0.62230E+10 
c  alpha        0.10580E+03     128   0.96512E-05   0.67354E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -3.6915                           332
a  R22               -30.348                           620
a  R33               -1.0272                           304
a  R12                -17.47                           282
a  R13           -3.5525e-05                            53
a  R23           -3.3135e-05                            53
a  Dissip             -55834                           790
a  alpha                              1.0012                       11523
a  LocalTime       8.832e-09                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2346.1            1739         -133.91         -79.016
v  Velocity[x]            -47.778          142.66          33.094          62.495
v  Velocity[y]            -38.886           54.03         0.29699           1.017
v  Velocity[z]        -0.00029203      0.00057089       1.132e-08      1.2448e-08
v  R11                      1e-24          398.04          7.6486          19.994
v  R22                      1e-24          206.54          3.8203          9.6929
v  R33                      1e-24          230.47          4.6586          11.855
v  R12                     -17.47          167.97         -1.6727       -0.064458
v  R13                -3.5525e-05      5.0083e-05      6.2493e-08      7.1114e-09
v  R23                -3.3135e-05       6.109e-05     -3.0102e-08     -3.5385e-09
v  Dissip              0.00091729      8.8563e+05          1820.9          9808.7
v  alpha                0.0011135               1         0.79474         0.99304
v  TurbVisc            6.4218e-54          289.23        0.043338         0.13912
v  CourantNb              0.23948           427.7          63.148          77.994
v  FourierNb             0.014852      1.1322e+07          1864.7          286.25
v  total_pressure           98979      1.0306e+05      1.0119e+05      1.0125e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.9973      1.1322e+07          1927.8          364.25


 TIME FOR THE TIME STEP               32:        0.59705E+02

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


 INSTANT    0.330000000E+01   TIME STEP NUMBER              33
 ============================================================= 




   ** 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         0.294639361E+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   :  0.35784E+00 0.87988E+01
   Friction velocity        uk    :  0.35784E+00 0.87988E+01
   Dimensionless distance   yplus :  0.20998E+00 0.24503E+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        144 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13942E-01     636   0.23943E-02   0.20392E+00 
c  VelocityX    0.28071E+01     487   0.29135E-01   0.23708E+04 
c  VelocityY    0.28071E+01     487   0.29135E-01   0.71007E+03 
c  VelocityZ    0.28071E+01     487   0.29135E-01   0.19088E-08 
c  R11          0.32706E+02    5461   0.11076E-01   0.39510E+04 
c  R22          0.14808E+02    5343   0.12675E-01   0.11221E+04 
c  R33          0.17725E+02    5467   0.11218E-01   0.11872E+04 
c  R12          0.11039E+02    6007   0.10904E-01   0.48420E+03 
c  R13          0.32089E-05    9323   0.13668E+00   0.19409E-09 
c  R23          0.24275E-06   10000   0.20793E+01   0.28704E-09 
c  Dissip       0.36662E+05    1572   0.90924E-02   0.99731E+10 
c  alpha        0.11637E+03     123   0.96776E-05   0.86309E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -6.7949                          1055
a  R22               -8.5496                           537
a  R33               -1.0314                           311
a  R12               -17.643                          1028
a  R13           -0.00016167                           779
a  R23           -0.00014428                            81
a  Dissip             -15448                          1240
a  alpha                              1.0022                       12243
a  LocalTime      2.5566e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2214.4          1835.8         -19.141          27.707
v  Velocity[x]            -45.568           141.1          33.934          62.497
v  Velocity[y]            -38.293          55.579         0.33397          1.1229
v  Velocity[z]        -0.00032183      0.00030414      1.7442e-07       1.064e-08
v  R11                      1e-24          416.63          7.7566          21.055
v  R22                      1e-24          217.03          3.9188          10.341
v  R33                      1e-24           241.7          4.7358          12.459
v  R12                    -17.643           175.2         -1.5887         0.18389
v  R13                -0.00016167      7.0928e-05      -2.021e-07     -9.8712e-09
v  R23                -0.00014428      0.00013138      2.7729e-07      1.8905e-08
v  Dissip              0.00077535      9.0132e+05          2019.4           11082
v  alpha                0.0011254               1         0.80148         0.99382
v  TurbVisc             3.743e-54          84.808        0.031948        0.088608
v  CourantNb              0.23565          451.47          63.105          78.174
v  FourierNb             0.014852      3.9115e+05          863.12           191.7
v  total_pressure           99111      1.0316e+05      1.0131e+05      1.0135e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.4087      3.9117e+05          926.22          269.88


 TIME FOR THE TIME STEP               33:        0.40029E+02

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


 INSTANT    0.340000000E+01   TIME STEP NUMBER              34
 ============================================================= 




   ** 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         0.294633856E+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   :  0.32499E+00 0.85858E+01
   Friction velocity        uk    :  0.32499E+00 0.85858E+01
   Dimensionless distance   yplus :  0.17171E+00 0.24803E+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        144 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.14976E-01     690   0.20650E-02   0.19891E+00 
c  VelocityX    0.28105E+01     476   0.26645E-01   0.22591E+04 
c  VelocityY    0.28105E+01     476   0.26645E-01   0.72358E+03 
c  VelocityZ    0.28105E+01     476   0.26645E-01   0.73416E-08 
c  R11          0.34559E+02   10000   0.68864E-02   0.42318E+04 
c  R22          0.15574E+02   10000   0.11868E-01   0.14144E+04 
c  R33          0.18794E+02   10000   0.76867E-02   0.10985E+04 
c  R12          0.11720E+02   10000   0.10978E-01   0.66529E+03 
c  R13          0.12547E-04   10000   0.11671E-01   0.77257E-09 
c  R23          0.54869E-06   10000   0.17658E+00   0.15167E-09 
c  Dissip       0.38863E+05    2743   0.58811E-02   0.10595E+11 
c  alpha        0.11264E+03     123   0.97815E-05   0.44619E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -1.6086                           345
a  R22               -12.644                           676
a  R33              -0.81231                           313
a  R12               -17.723                           580
a  R13           -8.3021e-05                            41
a  R23           -0.00014217                            46
a  Dissip             -47915                          1161
a  alpha                              1.0011                       12517
a  LocalTime      1.2763e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2041.9          1926.4          108.72          149.95
v  Velocity[x]            -42.547          145.23          34.755            62.5
v  Velocity[y]            -37.911          57.304         0.38766          1.3079
v  Velocity[z]        -0.00069876      0.00050851     -1.0716e-06      5.7409e-09
v  R11                      1e-24          426.64          7.8497          21.173
v  R22                      1e-24          217.21          3.8956          10.203
v  R33                      1e-24          247.51          4.7693          12.571
v  R12                    -17.723          177.79         -1.6273         0.12014
v  R13                -8.3021e-05      0.00038365      3.9156e-07      1.4123e-08
v  R23                -0.00014217      0.00011325      7.2646e-08     -8.8176e-10
v  Dissip              0.00065159      8.6212e+05          2050.2           11213
v  alpha                0.0011562               1         0.79699         0.99355
v  TurbVisc            2.5265e-54          156.18        0.031155        0.081578
v  CourantNb              0.21184          515.65          62.887          78.137
v  FourierNb             0.014852      7.8354e+06          1159.2          219.96
v  total_pressure           99283      1.0325e+05      1.0143e+05      1.0147e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.4641      7.8355e+06            1222           298.1


 TIME FOR THE TIME STEP               34:        0.56237E+02

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


 INSTANT    0.350000000E+01   TIME STEP NUMBER              35
 ============================================================= 




   ** 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         0.294621928E+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   :  0.26881E+00 0.83184E+01
   Friction velocity        uk    :  0.26881E+00 0.83184E+01
   Dimensionless distance   yplus :  0.96548E-01 0.24991E+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        156 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.14680E-01     708   0.19401E-02   0.20144E+00 
c  VelocityX    0.28129E+01     466   0.25356E-01   0.21240E+04 
c  VelocityY    0.28129E+01     466   0.25356E-01   0.73189E+03 
c  VelocityZ    0.28129E+01     466   0.25356E-01   0.51396E-08 
c  R11          0.36606E+02    5348   0.15460E-01   0.47269E+04 
c  R22          0.16575E+02    5948   0.18773E-01   0.13498E+04 
c  R33          0.19790E+02    6502   0.15207E-01   0.13693E+04 
c  R12          0.12208E+02    6097   0.24375E-01   0.67664E+03 
c  R13          0.12435E-04    9555   0.26780E+00   0.83751E-09 
c  R23          0.10786E-05    9484   0.87519E+00   0.69121E-09 
c  Dissip       0.41210E+05    1403   0.10612E-01   0.13230E+11 
c  alpha        0.10950E+03     133   0.98299E-05   0.66267E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -1.1104                           399
a  R22               -22.376                           665
a  R33               -0.7375                           392
a  R12               -17.495                           360
a  R13           -9.1752e-05                            78
a  R23           -0.00025504                           119
a  Dissip             -47479                          1013
a  alpha                              1.0011                       12607
a  LocalTime      1.5924e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1826.6          2015.5          249.03          288.42
v  Velocity[x]            -38.821           142.8          35.622          62.504
v  Velocity[y]            -37.297          58.925         0.43835          1.4794
v  Velocity[z]        -0.00086499      0.00066853     -1.6209e-06       8.487e-09
v  R11                      1e-24           435.3          8.1235          22.405
v  R22                      1e-24          215.91          4.0234          10.734
v  R33                      1e-24          250.84          4.9336           13.29
v  R12                    -17.495          178.76         -1.5961         0.37975
v  R13                -9.1752e-05      0.00023373       3.673e-07     -6.9534e-09
v  R23                -0.00025504      0.00025305     -1.2261e-07      4.5226e-09
v  Dissip              0.00054681      9.6598e+05          2199.4           12196
v  alpha                0.0011882               1         0.79928         0.99335
v  TurbVisc            2.5976e-54          2090.2        0.068976         0.22201
v  CourantNb               0.2147          546.14           62.05          77.873
v  FourierNb             0.014904      6.2797e+05          931.07          285.95
v  total_pressure           99498      1.0334e+05      1.0157e+05      1.0161e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4.4002      6.2806e+05          993.12          363.82


 TIME FOR THE TIME STEP               35:        0.41391E+02

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


 INSTANT    0.360000000E+01   TIME STEP NUMBER              36
 ============================================================= 




   ** 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         0.294621358E+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   :  0.35930E+00 0.80382E+01
   Friction velocity        uk    :  0.35930E+00 0.80382E+01
   Dimensionless distance   yplus :  0.14983E+00 0.25241E+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        156 outlet faces on        225


 Write intermediate restart files
   checkpoint at iteration         36, Physical time    0.36000E+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:    0.68515E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.16681E-01     726   0.16134E-02   0.21858E+00 
c  VelocityX    0.28152E+01     452   0.23883E-01   0.20438E+04 
c  VelocityY    0.28152E+01     452   0.23883E-01   0.78421E+03 
c  VelocityZ    0.28152E+01     452   0.23883E-01   0.40814E-07 
c  R11          0.38110E+02    7883   0.54480E-02   0.39159E+04 
c  R22          0.17091E+02    8668   0.80462E-02   0.12793E+04 
c  R33          0.20620E+02    8935   0.68533E-02   0.93908E+03 
c  R12          0.12650E+02    9998   0.83177E-02   0.60110E+03 
c  R13          0.69204E-04    8775   0.22476E-01   0.11252E-08 
c  R23          0.96038E-06   10000   0.85837E+00   0.33433E-09 
c  Dissip       0.43528E+05    2383   0.35059E-02   0.10628E+11 
c  alpha        0.12003E+03     121   0.97341E-05   0.43480E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11              -0.82922                           344
a  R22               -22.087                           718
a  R33              -0.42665                           337
a  R12               -17.049                           361
a  R13           -0.00032828                            18
a  R23           -0.00016526                            23
a  Dissip             -42560                          1168
a  alpha                              1.0011                       12082
a  LocalTime      7.2384e-08                         89999


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1568.9          2102.4          397.07          437.43
v  Velocity[x]            -34.194          149.31          36.573          62.507
v  Velocity[y]            -37.713          62.279         0.49842          1.7072
v  Velocity[z]         -0.0011403       0.0018338       4.262e-07      1.5803e-08
v  R11                      1e-24          436.06          7.9965           22.08
v  R22                      1e-24           206.2           3.953          10.511
v  R33                      1e-24          249.48          4.8944          13.163
v  R12                    -17.049          176.77         -1.6483         0.27356
v  R13                -0.00032828      0.00010244     -1.1828e-06     -3.7083e-08
v  R23                -0.00016526      0.00035742      6.2903e-07      4.1039e-08
v  Dissip              0.00045141      1.0583e+06          2109.2           11894
v  alpha                0.0011975               1         0.79526           0.993
v  TurbVisc            2.1678e-54          62.674        0.027971        0.065662
v  CourantNb              0.19964          549.28          61.104          77.403
v  FourierNb             0.015654      1.3815e+06            1144          213.96
v  total_pressure           99756      1.0343e+05      1.0172e+05      1.0176e+05
v  LocalTime                 0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.2829      1.3816e+06          1205.1          291.36


 TIME FOR THE TIME STEP               36:        0.52138E+02

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


 INSTANT    0.370000000E+01   TIME STEP NUMBER              37
 ============================================================= 




   ** 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         0.294618939E+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   :  0.35981E+00 0.77453E+01
   Friction velocity        uk    :  0.35981E+00 0.77453E+01
   Dimensionless distance   yplus :  0.13351E+00 0.25350E+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        168 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.19741E-01     744   0.14405E-02   0.26817E+00 
c  VelocityX    0.28159E+01     437   0.22905E-01   0.20100E+04 
c  VelocityY    0.28159E+01     437   0.22905E-01   0.77338E+03 
c  VelocityZ    0.28159E+01     437   0.22905E-01   0.19774E-07 
c  R11          0.39770E+02    6722   0.20742E-01   0.10321E+05 
c  R22          0.17855E+02    8698   0.31265E-01   0.23595E+04 
c  R33          0.21381E+02    8098   0.17195E-01   0.30305E+04 
c  R12          0.12908E+02    6240   0.24837E-01   0.96176E+03 
c  R13          0.15427E-05   10000   0.13632E+01   0.50685E-08 
c  R23          0.13619E-05   10000   0.12750E+01   0.20175E-08 
c  Dissip       0.46306E+05    3684   0.22177E-01   0.31565E+11 
c  alpha        0.13905E+03     117   0.96173E-05   0.85889E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -5.5553                           745
a  R22               -32.315                           652
a  R33              -0.28407                           359
a  R12               -16.458                           718
a  R13           -0.00025743                           393
a  R23           -0.00050819                            69
a  Dissip             -19757                           617
a  alpha                              1.0031                       11960
a  LocalTime      2.8562e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1278.1          2175.4           537.5          582.21
v  Velocity[x]            -29.514          146.61          37.607          62.514
v  Velocity[y]            -41.255          62.493         0.53948          1.8886
v  Velocity[z]         -0.0015089       0.0023952      1.3173e-07      4.0575e-08
v  R11                      1e-24          433.97          8.3016          23.812
v  R22                      1e-24          191.94          4.0949          11.272
v  R33                      1e-24          245.16          5.0894           14.14
v  R12                    -16.458          170.65         -1.5212          0.7321
v  R13                -0.00023724      0.00056093      2.4853e-06      9.6273e-08
v  R23                -0.00050819      0.00033192     -2.3573e-07     -3.5484e-09
v  Dissip              0.00037417      1.1457e+06            2433           13582
v  alpha                 0.001163               1         0.79921         0.99326
v  TurbVisc            2.1069e-54          882.39        0.044101         0.14213
v  CourantNb              0.23809          543.11          60.266          76.748
v  FourierNb             0.015654      3.5012e+06          1281.4          249.19
v  total_pressure      1.0005e+05       1.035e+05      1.0186e+05      1.0191e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier             1.6      3.5012e+06          1341.7          325.94


 TIME FOR THE TIME STEP               37:        0.48830E+02

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


 INSTANT    0.380000000E+01   TIME STEP NUMBER              38
 ============================================================= 




   ** 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         0.294622837E+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   :  0.18325E+00 0.74962E+01
   Friction velocity        uk    :  0.18325E+00 0.74962E+01
   Dimensionless distance   yplus :  0.70584E-01 0.25671E+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        171 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.21094E-01     690   0.11336E-02   0.26079E+00 
c  VelocityX    0.28172E+01     434   0.22541E-01   0.20331E+04 
c  VelocityY    0.28172E+01     434   0.22541E-01   0.84305E+03 
c  VelocityZ    0.28172E+01     434   0.22541E-01   0.88250E-07 
c  R11          0.40513E+02    4653   0.53941E-02   0.10190E+05 
c  R22          0.18087E+02    5437   0.91628E-02   0.31854E+04 
c  R33          0.21829E+02    5484   0.65533E-02   0.25427E+04 
c  R12          0.12984E+02    6023   0.91047E-02   0.14514E+04 
c  R13          0.19123E-04    5222   0.43007E-01   0.72503E-08 
c  R23          0.20734E-05    6079   0.30298E+00   0.23099E-08 
c  Dissip       0.47102E+05    1353   0.52144E-02   0.26260E+11 
c  alpha        0.11765E+03     119   0.97708E-05   0.52150E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -5.8376                           547
a  R22               -19.227                           809
a  R33              -0.91383                           408
a  R12               -18.049                           652
a  R13           -0.00061952                           184
a  R23           -0.00061529                           136
a  Dissip             -93977                          1528
a  alpha                              1.0014                       12734
a  LocalTime      3.0386e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -970.38          2208.7           638.5          689.85
v  Velocity[x]            -28.581          156.75          38.431          62.517
v  Velocity[y]            -51.769          72.896         0.57037           2.081
v  Velocity[z]         -0.0032691       0.0015414     -1.7857e-06     -6.7074e-09
v  R11                      1e-24          414.43          8.2079          23.185
v  R22                      1e-24          185.02          4.0185          11.009
v  R33                      1e-24          230.56           5.016          13.889
v  R12                    -15.873          157.47         -1.5696         0.62671
v  R13                -0.00061952      0.00039856     -8.7989e-07       1.951e-09
v  R23                -0.00061529      0.00036874     -1.3989e-06     -9.4152e-08
v  Dissip              0.00030755       1.058e+06          2255.5           12789
v  alpha                0.0011262               1         0.79952         0.99352
v  TurbVisc            2.0541e-54          708.23        0.036855         0.11651
v  CourantNb              0.26085          538.02          59.252          75.923
v  FourierNb             0.015654       3.291e+06          945.87          208.51
v  total_pressure      1.0035e+05      1.0353e+05      1.0196e+05      1.0201e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3159       3.291e+06          1005.1          284.43


 TIME FOR THE TIME STEP               38:        0.33357E+02

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


 INSTANT    0.390000000E+01   TIME STEP NUMBER              39
 ============================================================= 




   ** 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         0.294617662E+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   :  0.17516E+00 0.72612E+01
   Friction velocity        uk    :  0.17516E+00 0.72612E+01
   Dimensionless distance   yplus :  0.62823E-01 0.26038E+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        177 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.24034E-01     456   0.11859E-02   0.30031E+00 
c  VelocityX    0.28154E+01     411   0.24885E-01   0.21482E+04 
c  VelocityY    0.28154E+01     411   0.24885E-01   0.94205E+03 
c  VelocityZ    0.28154E+01     411   0.24885E-01   0.99446E-07 
c  R11          0.41752E+02   10000   0.16247E-01   0.82705E+04 
c  R22          0.19414E+02   10000   0.20343E-01   0.34427E+04 
c  R33          0.22406E+02   10000   0.15715E-01   0.22790E+04 
c  R12          0.13244E+02   10000   0.30497E-01   0.13891E+04 
c  R13          0.31097E-04    5887   0.21454E-01   0.46383E-08 
c  R23          0.50386E-05   10000   0.77532E+00   0.47028E-08 
c  Dissip       0.49040E+05    3630   0.66169E-02   0.17653E+11 
c  alpha        0.11135E+03     123   0.99245E-05   0.71375E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11              -0.18744                           388
a  R22               -32.082                           715
a  R33              -0.11099                           388
a  R12               -15.209                           262
a  R13           -0.00059078                             6
a  R23           -0.00061422                           134
a  Dissip             -74872                           610
a  alpha                              1.0021                       12241
a  LocalTime      3.0813e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -908.6          2145.8          648.37          710.21
v  Velocity[x]            -27.259          147.17          39.108           62.52
v  Velocity[y]            -54.455          70.808         0.54702           2.083
v  Velocity[z]          -0.003003       0.0029265       1.829e-06     -2.4499e-08
v  R11                      1e-24          421.39          8.5931          24.679
v  R22                      1e-24          189.95           4.217          11.811
v  R33                      1e-24          225.51          5.2261          14.736
v  R12                    -15.209          146.26         -1.4902          1.1259
v  R13                -0.00059078       0.0004528     -1.4979e-06     -5.9339e-08
v  R23                -0.00061422      0.00036409     -1.0664e-06     -3.4878e-08
v  Dissip              0.00025515      1.0697e+06            2514           14011
v  alpha                0.0010756               1         0.79725         0.99307
v  TurbVisc            2.0834e-54          114.75        0.034548        0.094468
v  CourantNb              0.18786          535.89          58.325          74.968
v  FourierNb             0.015654      3.2454e+06          1123.7          228.53
v  total_pressure      1.0042e+05      1.0347e+05      1.0197e+05      1.0204e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4038      3.2455e+06          1182.1           303.5


 TIME FOR THE TIME STEP               39:        0.53082E+02

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


 INSTANT    0.400000000E+01   TIME STEP NUMBER              40
 ============================================================= 




   ** 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         0.294625316E+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   :  0.32696E+00 0.69851E+01
   Friction velocity        uk    :  0.32696E+00 0.69851E+01
   Dimensionless distance   yplus :  0.14292E+00 0.26167E+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        181 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.28315E-01     618   0.11094E-02   0.32622E+00 
c  VelocityX    0.28120E+01     402   0.26638E-01   0.24677E+04 
c  VelocityY    0.28120E+01     402   0.26638E-01   0.99767E+03 
c  VelocityZ    0.28120E+01     402   0.26638E-01   0.24181E-06 
c  R11          0.42271E+02    6894   0.54167E-02   0.61420E+04 
c  R22          0.20028E+02    7961   0.61376E-02   0.23585E+04 
c  R33          0.22858E+02    7448   0.68450E-02   0.14148E+04 
c  R12          0.13594E+02   10000   0.74019E-02   0.10190E+04 
c  R13          0.17296E-05   10000   0.62066E+00   0.83284E-08 
c  R23          0.10012E-05   10000   0.17199E+01   0.10648E-07 
c  Dissip       0.48995E+05    1290   0.34811E-02   0.15123E+11 
c  alpha        0.11230E+03     125   0.95980E-05   0.68565E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -1.0399                           487
a  R22               -22.969                           720
a  R33             -0.080788                           350
a  R12               -14.491                           638
a  R13            -0.0011459                           138
a  R23            -0.0015354                           110
a  Dissip             -74181                          1974
a  alpha                              1.0019                       12399
a  LocalTime      1.4384e-06                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1177.8          1921.6          505.43          580.45
v  Velocity[x]            -26.199          153.43          39.667          62.524
v  Velocity[y]            -56.565          68.273         0.48092          1.9469
v  Velocity[z]          -0.003124       0.0028634      5.5772e-06     -8.1165e-08
v  R11                      1e-24          422.44          8.4443          24.221
v  R22                      1e-24          211.83          4.1331          11.474
v  R33                      1e-24          226.07          5.1626          14.466
v  R12                    -14.491           161.2         -1.5292          1.0579
v  R13                 -0.0011459      0.00049485      2.2831e-06      1.8765e-07
v  R23                 -0.0015354       0.0011412     -6.9746e-07     -4.0152e-08
v  Dissip              0.00021985      9.6895e+05          2374.3           13572
v  alpha                0.0010133               1          0.8051         0.99357
v  TurbVisc            2.2239e-54          91.385        0.029463        0.072771
v  CourantNb             0.011094          540.88          57.341          74.038
v  FourierNb             0.017463           69519          984.96          210.21
v  total_pressure      1.0015e+05      1.0325e+05      1.0183e+05      1.0191e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.1117           69555          1042.3          284.25


 TIME FOR THE TIME STEP               40:        0.48245E+02

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


 INSTANT    0.410000000E+01   TIME STEP NUMBER              41
 ============================================================= 




   ** 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         0.294656133E+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   :  0.25085E+00 0.68833E+01
   Friction velocity        uk    :  0.25085E+00 0.68833E+01
   Dimensionless distance   yplus :  0.89546E-01 0.25608E+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        180 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.22573E-01     672   0.63498E-03   0.25224E+00 
c  VelocityX    0.28064E+01     402   0.32438E-01   0.25925E+04 
c  VelocityY    0.28064E+01     402   0.32438E-01   0.95283E+03 
c  VelocityZ    0.28064E+01     402   0.32438E-01   0.80809E-06 
c  R11          0.43639E+02   10000   0.14992E-01   0.14286E+05 
c  R22          0.21013E+02   10000   0.21489E-01   0.40371E+04 
c  R33          0.23487E+02   10000   0.13262E-01   0.36854E+04 
c  R12          0.13985E+02   10000   0.17734E-01   0.17350E+04 
c  R13          0.40683E-05   10000   0.63469E+00   0.28886E-07 
c  R23          0.10552E-04   10000   0.52649E+00   0.17887E-07 
c  Dissip       0.49424E+05    9582   0.76925E-02   0.43697E+11 
c  alpha        0.10391E+03     128   0.10664E-04   0.10612E-01 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -4.8953                           515
a  R22               -43.162                           725
a  R33             -0.035873                           332
a  R12               -28.224                           738
a  R13            -0.0029907                           185
a  R23           -0.00044042                           204
a  Dissip        -1.0619e+05                           625
a  alpha                              1.0013                       11793
a  LocalTime      1.4805e-08                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1606.6          1523.5           178.6           271.8
v  Velocity[x]            -30.101          150.46          40.011          62.519
v  Velocity[y]            -52.261           71.47         0.31369          1.5038
v  Velocity[z]         -0.0076661        0.011263      6.7536e-06     -1.7923e-07
v  R11                      1e-24          438.93          8.7752          25.913
v  R22                      1e-24          227.37          4.2428          12.013
v  R33                      1e-24          228.28          5.3674          15.388
v  R12                    -25.795          179.09         -1.4039          1.5134
v  R13                 -0.0029907       0.0010475     -3.6663e-06     -9.4107e-08
v  R23                -0.00044042      0.00079288     -3.0547e-07     -1.2148e-07
v  Dissip              0.00095428      9.7608e+05          2783.8           15431
v  alpha                0.0010034               1         0.79906         0.99294
v  TurbVisc            2.4552e-54          46.368        0.030756        0.074686
v  CourantNb              0.12399          545.48           56.53          73.106
v  FourierNb             0.017463      6.7546e+06          1731.1          258.99
v  total_pressure           99718      1.0285e+05       1.015e+05       1.016e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2146      6.7547e+06          1787.6           332.1


 TIME FOR THE TIME STEP               41:        0.61691E+02

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


 INSTANT    0.420000000E+01   TIME STEP NUMBER              42
 ============================================================= 




   ** 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         0.294689685E+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   :  0.34352E+00 0.95074E+01
   Friction velocity        uk    :  0.34352E+00 0.95074E+01
   Dimensionless distance   yplus :  0.12234E+00 0.24728E+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          4 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27223E-01     690   0.34094E-03   0.27165E+00 
c  VelocityX    0.28015E+01     404   0.30290E-01   0.23181E+04 
c  VelocityY    0.28015E+01     404   0.30290E-01   0.80313E+03 
c  VelocityZ    0.28015E+01     404   0.30290E-01   0.97337E-06 
c  R11          0.44609E+02    2787   0.50014E-02   0.15569E+05 
c  R22          0.21438E+02    3565   0.84330E-02   0.48252E+04 
c  R33          0.24107E+02    3866   0.60148E-02   0.35972E+04 
c  R12          0.14634E+02    3793   0.91873E-02   0.22528E+04 
c  R13          0.38601E-05   10000   0.53022E+00   0.46623E-07 
c  R23          0.78606E-05   10000   0.33266E+00   0.33219E-07 
c  Dissip       0.48694E+05    3025   0.72423E-02   0.49852E+11 
c  alpha        0.11396E+03     129   0.10341E-04   0.14017E-01 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -7.2541                           621
a  R22               -56.469                           984
a  R33              -0.67159                           373
a  R12               -21.363                          1230
a  R13            -0.0019361                           254
a  R23            -0.0019268                           420
a  Dissip        -1.7423e+05                          2126
a  alpha                              1.0025                       13300
a  LocalTime       2.892e-07                         90000


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2121.6          1063.2         -242.61         -130.87
v  Velocity[x]            -41.744          159.71          39.659           62.51
v  Velocity[y]            -50.856          76.319        0.092972         0.87699
v  Velocity[z]          -0.005156       0.0034028     -1.4937e-06     -2.2145e-07
v  R11                      1e-24          445.33          8.5783          25.142
v  R22                      1e-24           245.7          4.0405          11.198
v  R33                      1e-24          241.92          5.2341          15.041
v  R12                    -13.276          190.84         -1.4831          1.1215
v  R13                 -0.0019361       0.0013894     -3.5464e-07      9.3187e-08
v  R23                 -0.0019268       0.0014847      -3.991e-06     -2.3461e-07
v  Dissip              0.00080267      9.2755e+05          2534.8           14571
v  alpha                0.0015593               1         0.81212         0.99413
v  TurbVisc            2.3667e-54          768.97        0.034246         0.11478
v  CourantNb             0.040884          542.93          56.246          72.176
v  FourierNb             0.015654      3.4578e+05          789.44          186.95
v  total_pressure           99203      1.0239e+05      1.0108e+05      1.0119e+05
v  LocalTime                 0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.3145       3.458e+05          845.68          259.12


 TIME FOR THE TIME STEP               42:        0.35581E+02

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


 INSTANT    0.430000000E+01   TIME STEP NUMBER              43
 ============================================================= 




   ** 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         0.294695629E+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   :  0.46476E-01 0.41897E+01
   Friction velocity        uk    :  0.46476E-01 0.41897E+01
   Dimensionless distance   yplus :  0.16535E-01 0.24254E+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          7 outlet faces on        225

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.28447E-01     669   0.33399E-03   0.29748E+00 
c  VelocityX    0.27962E+01     402   0.39620E-01   0.10651E+04 
c  VelocityY    0.27962E+01     402   0.39620E-01   0.42284E+03 
c  VelocityZ    0.27962E+01     402   0.39620E-01   0.17589E-05 
c  R11          0.46294E+02    9632   0.26195E-01   0.11246E+05 
c  R22          0.22497E+02   10000   0.30736E-01   0.38249E+04 
c  R33          0.24956E+02   10000   0.20892E-01   0.34049E+04 
c  R12          0.15161E+02   10000   0.26591E-01   0.15758E+04 
c  R13          0.34099E-04    7573   0.82933E-01   0.52248E-07 
c  R23          0.70784E-05    9463   0.33262E+00   0.23313E-07 
c  Dissip       0.50768E+05    8708   0.21868E-01   0.30943E+11 
c  alpha        0.10984E+03     121   0.98625E-05   0.10182E-01 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11               -3.1202                           529
a  R22                -79.59                           793
a  R33              -0.31498                           386
a  R12               -25.965                           693
a  R13            -0.0022755                           141
a  R23            -0.0028716                           284
a  Dissip        -1.2286e+05                           998
a  alpha                              1.0016                       12401
a  LocalTime      4.7248e-08                         89998


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2447.5          744.01         -542.79         -419.81
v  Velocity[x]            -45.717             149          38.889          62.505
v  Velocity[y]            -46.329          81.481       -0.019094         0.41609
v  Velocity[z]          -0.010274       0.0094527       3.434e-06     -3.4991e-07
v  R11                      1e-24          464.66          9.0172           26.89
v  R22                      1e-24          265.99          4.2002          11.712
v  R33                      1e-24          262.87          5.4556          16.005
v  R12                    -11.494          199.67         -1.4269          1.5742
v  R13                 -0.0022755       0.0025881     -3.3193e-06       -4.78e-08
v  R23                 -0.0028716      0.00090533     -8.7057e-06     -4.0902e-07
v  Dissip              0.00058355      1.1326e+06          2809.3           15669
v  alpha                0.0014196               1         0.80295         0.99323
v  TurbVisc            2.1597e-54           282.5        0.033425        0.086376
v  CourantNb              0.03913           551.3            55.3          71.106
v  FourierNb             0.015654      2.1165e+06          1345.4          248.25
v  total_pressure           98877      1.0207e+05      1.0078e+05      1.0091e+05
v  LocalTime                 0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.8483      2.1166e+06          1400.7          319.36


 TIME FOR THE TIME STEP               43:        0.58912E+02

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


 INSTANT    0.440000000E+01   TIME STEP NUMBER              44
 ============================================================= 



 Options positionnées ou modifiées par fichier "control_file" :
 --------------------------------------------------------------

  max_time_step                              44 (courant : 44)

 Lecture de "control_file" terminée.



   ** 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         0.294657460E+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   :  0.26872E+00 0.40514E+01
   Friction velocity        uk    :  0.26872E+00 0.40514E+01
   Dimensionless distance   yplus :  0.95544E-01 0.24651E+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         12 outlet faces on        225


 Write final restart files
   checkpoint at iteration         44, Physical time    0.44000E+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:    0.66107E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25057E-01     600   0.39234E-03   0.24434E+00 
c  VelocityX    0.27941E+01     401   0.32664E-01   0.72854E+03 
c  VelocityY    0.27941E+01     401   0.32664E-01   0.25271E+03 
c  VelocityZ    0.27941E+01     401   0.32664E-01   0.14269E-05 
c  R11          0.46229E+02   10000   0.78339E-02   0.10842E+05 
c  R22          0.21749E+02   10000   0.10995E-01   0.26479E+04 
c  R33          0.25150E+02   10000   0.88104E-02   0.27604E+04 
c  R12          0.15042E+02   10000   0.16729E-01   0.12998E+04 
c  R13          0.35371E-04    8983   0.13846E+01   0.84186E-07 
c  R23          0.10605E-04   10000   0.48322E+01   0.21571E-06 
c  Dissip       0.50589E+05    4505   0.71528E-02   0.27178E+11 
c  alpha        0.13951E+03     112   0.97353E-05   0.38577E-02 
---------------------------------------------------------------
  
  

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

   champ          min. init.      max. init.   lim. à min.   lim. à max.
-  ---------  --------------  --------------  ------------  ------------
a  R11              -0.34608                           430
a  R22               -87.018                           776
a  R33           -7.9864e-06                           375
a  R12               -27.051                           469
a  R13            -0.0021785                            59
a  R23            -0.0045566                           225
a  Dissip         -1.215e+05                           913
a  alpha                               1.001                       12681
a  LocalTime      5.1631e-08                         89998


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

   champ                  minimum         maximum   moy. ensemble   moy. spatiale
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2633.1          578.91         -705.98            -579
v  Velocity[x]            -44.387          155.63          38.235          62.502
v  Velocity[y]            -49.741          85.004       -0.049625         0.25908
v  Velocity[z]          -0.010374        0.017562      2.0728e-05     -6.5673e-07
v  R11                      1e-24          481.33          8.9936           26.74
v  R22                      1e-24          257.59          4.0995          11.174
v  R33                      1e-24          270.36          5.4481          15.954
v  R12                    -11.217          196.57         -1.4632          1.5762
v  R13                 -0.0021785       0.0033561      1.1198e-06      -2.272e-08
v  R23                 -0.0045566       0.0027494     -4.4578e-06     -2.6693e-07
v  Dissip              0.00013905      1.2755e+06          2599.4           14748
v  alpha                0.0013391               1         0.80217          0.9929
v  TurbVisc            1.9857e-54          22.069        0.027663        0.061282
v  CourantNb             0.058615          592.66          54.871          70.744
v  FourierNb             0.015501      1.9368e+06          1204.9          219.95
v  total_pressure           98692       1.019e+05      1.0062e+05      1.0075e+05
v  LocalTime                 0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum   moy. ensemble   moy. spatiale
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.0047      1.9369e+06          1259.8          290.69


 TIME FOR THE TIME STEP               44:        0.57588E+02

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.73940E-02
      -----------------------                                



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




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


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

 Destruction des structures et clôture du calcul


Bilan des temps de calcul :

  Temps CPU utilisateur :     2127.849 s
  Temps CPU système :            1.628 s

  Temps écoulé :              2134.576 s
  Temps CPU / écoulé             0.998

Bilan de l'occupation mémoire :

  Consommation mémoire totale mesurée :           435.137 Mio
  Mémoire dynamique instrumentée théorique :      100.319 Mio
