commande : 
 /home/calcul/Bureau/BOSFOR/1_INITIALIZATION_CS/INITIALIZATION_TEMPLATE/RESU/20121128-1749/cs_solver --param INITIALIZATION.xml --mpi

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

                                  (R)
                      Code_Saturne

                      Version 3.0.0-betaR4215


  Copyright (C) 1998-2012 EDF S.A., France

  build mar. 27 nov. 2012 10:52:41 CET
  Version MPI 2.1 (Open MPI 1.6.3)


  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.

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


Configuration locale du cas :

  Date :               mer. 28 nov. 2012 17:49:12 CET
  Système :            Linux 2.6.32-39-generic
  Machine :            ZC-TITI
  Processeur :         model name	: Intel(R) Xeon(R) CPU           W5590  @ 3.33GHz
  Mémoire :            24153 Mo
  Utilisateur :        calcul (calcul)
  Répertoire :         /home/calcul/Bureau/BOSFOR/1_INITIALIZATION_CS/INITIALIZATION_TEMPLATE/RESU/20121128-1749
  Rangs MPI :          8 (attribut appnum : 0)
  méthode de lecture : entrées/sorties standard, accès parallèle
  méthode d'écriture : entrées/sorties standard, accès série
   pas des rangs E/S :  1

  Bibliothèques externes pour le partitionnement :
    ParMETIS 3.1
    SCOTCH

 Lecture des méta-données du fichier: "mesh_input"

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

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


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




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


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

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

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


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

 --- Geometry
       NPRFML =              1 (Nb max. family properties   )
       NFML   =              9 (Nb families                 )

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


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


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

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

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

  -- Continuous phase:

       RO0    =    0.12250E+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

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


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

 --- Continuous phase:

   - Commons
       ITURB  =             60 (Turbulence model            )
       IDEUCH =              0 (0: one-scale model          )
                               (1: two-scale model          )
                               (2: invariant wall function  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.23810E+01 (Limit Y+                    )
       ILOGPO =              1 (0: power law (forbidden for
                                              k-epsilon)    )
                               (1: one-scale log law        )
       IGRHOK =              0 (1: computed Grad(rho k)     )
       ISCALT =             -1 (Temperature salar number    )

   - k-omega SST         (ITURB = 60)
       ALMAX  =    0.40000E+01 (Characteristic length       )
       UREF   =    0.50000E-01 (Characteristic velocity     )
       IKECOU =              0 (k-epsilon coupling mode     )
       IGRAKE =              0 (Account for gravity         )
       RELAXV =    0.70000E+00 for k      (Relaxation)
       RELAXV =    0.70000E+00 for omega  (Relaxation)

   - Rotation/curvature correction
       IRCCOR =              0 (0: desactivated             )
                               (1: activated                )

 --- Constants

   - Commons
       XKAPPA =    0.42000E+00 (Von Karman constant         )
       CSTLOG =    0.52000E+01 (U+=Log(y+)/kappa +CSTLOG    )
       APOW   =    0.83000E+01 (U+=APOW (y+)**BPOW (W&W law))
       BPOW   =    0.14286E+00 (U+=APOW (y+)**BPOW (W&W law))

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


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


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

 --- Continuous phase:         1
       IVISSE = 

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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

       IDTVAR =              0 (0 cst; 1,2 var (t, t-space  )
       IPTLRO =              0 (1: rho-related DT clipping  )
       COUMAX =    0.10000E+01 (Maximum target CFL          )
       FOUMAX =    0.10000E+02 (Maximum target Fourier      )
       VARRDT =    0.10000E+00 (For var. DT, max. increase  )
       DTMIN  =    0.30000E-01 (Minimum time step           )
       DTMAX  =    0.30000E+03 (Maximum time step           )
       DTREF  =    0.30000E+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
 TurbEner              1  0.1000E+01
 omega                 1  0.1000E+01
----------------------------

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

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

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


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

---------------------------------------------------------------------
 Variable          ICONV  IDIFF IDIFFT ISCHCV ISSTPC   BLENCV  THETAV
---------------------------------------------------------------------
 Pressure              0      1      1      1      0 0.00E+00 0.10E+01
 VelocityX             1      1      1      0      0 0.10E+01 0.10E+01
 VelocityY             1      1      1      0      0 0.10E+01 0.10E+01
 VelocityZ             1      1      1      0      0 0.10E+01 0.10E+01
 TurbEner              1      1      1      0      0 0.10E+01 0.10E+01
 omega                 1      1      1      0      0 0.10E+01 0.10E+01
-------------------------------------------------------------

       ICONV  =  0 ou  1       (1 for convection active     )
       IDIFF  =  0 ou  1       (1 for total diffusion active)
       IDIFFT =  0 ou  1       (1 for turbulent diff. active)
       ISCHCV =  0 ou  1       (SOLU or CD                  )
       ISSTPC =  0 ou  1       (1: no slope test            )
       BLENCV =  [0.;1.]       (1-upwind proportion         )
       THETAV =  [0.;1.]       (0.5 Crank-Nicolson/AB       )
                               (theta for convection-       )
                               (diffusion terms uses        )
                               ((1-theta).old+theta.new     )


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


 ** STOKES
    ------
       IVELCO =              1 (0: segregated solving of the
                                   velocity components during
                                   the prediction step
                                1: coupled solving of the
                                   velocity components       )
       IPHYDR =              0 (1: account for explicit
                                   balance between pressure
                                   gradient, gravity source
                                   terms, and head losses     )
       ICALHY =              0 (1: compute hydrastatic
                                   pressure for Dirichlet
                                   conditions for pressure
                                   on outlet                  )
       IPRCO  =              1 (1: pressure-continuity        )
       IPUCOU =              0 (1: reinforced U-P coupling    )
       NTERUP =              1 (n: n sweeps on navsto for
                                   velocity/pressure coupling )

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

       RELAXV =    0.80000E+00 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 =              1 (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
 TurbEner            100      1  0.1000E-04  0.1000E-03  0.0000E+00
 omega               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
 TurbEner              1      1  0.1500E+01
 omega                 1      1  0.1500E+01
-----------------------------------

       NSWRGR =                (nb sweep gradient reconstr. )
       NSWRSM =                (nb sweep rhs reconstrcution )
       EPSRGR =                (grad. reconstruction prec.  )
       EPSRSM =                (rhs   reconstruction prec.  )
       EXTRAG =  [0.;1.]       (gradients extrapolation     )
       IRCFLU =  0 ou  1       (flow reconstruction         )
       IMLIGR =  < 0, 0 ou 1   (gradient limitation method  )
       CLIMGR =  > 1 ou 1      (gradient limitation coeff.  )


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


 ** FACE INTERPOLATION
    ------------------
       IMVISF =              0 (0 arithmetic                )


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


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

       NBMOMT =              0 (Number of moments           )

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


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

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


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

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


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


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

--------------------------------------------------
 Variable         IRESOL NITMAX      EPSILO IDIRCL
--------------------------------------------------
 Pressure              0     30  0.1000E-04      1
 VelocityX            -1     30  0.1000E-04      1
 VelocityY            -1     30  0.1000E-04      1
 VelocityZ            -1     30  0.1000E-04      1
 TurbEner             -1     30  0.1000E-04      1
 omega                -1     30  0.1000E-04      1
-----------------------------------

       IRESOL =            -1  (automatic solver choice     )
                IPOL*1000 + 0  (p conjuguate gradient       )
                            1  (Jacobi                      )
                IPOL*1000 + 2  (bicgstab                    )
                  avec IPOL    (preconditioning degree      )
       NITMAX =                (max number of iterations    )
       EPSILO =                (resolution precision        )
       IDIRCL = 0 ou 1         (shift diagonal if   
                                ISTAT=0 and no Dirichlet    )


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


 ** 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
 TurbEner              0    100     10
 omega                 0    100     10
------------------------------

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


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

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

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


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

 --- Restarted calculation
       ISUITE =              0 (1: restarted calculuation   )
       ILEAUX =              1 (1: also read  suiamx        )
       IECAUX =              1 (1: also write suiavx        )

       suiamx and suiavx are the auxiliary restart files.

 --- 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 TurbEner        
         7 omega           
        10 TurbVisc        
        11 CourantNb       
        12 FourierNb       
        13 total_pressure  
         --           --

 --- 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 TurbEner                      -1
         7 omega                         -1
         8 Density                       -1
         9 LamVisc                       -1
        10 TurbVisc                      -1
        11 CourantNb                     -1
        12 FourierNb                     -1
        13 total_pressure                -1
         --           --                --

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

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

         2 Pressure                       0
         3 VelocityX                      0
         4 VelocityY                      0
         5 VelocityZ                      0
         6 TurbEner                       0
         7 omega                          0
        10 TurbVisc                    -999
        11 CourantNb                   -999
        12 FourierNb                   -999
        13 total_pressure              -999
         --           --                --

 --- Additional post-processing variables (ipstdv)
       ipstfo =              1 (Force exerted  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)


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


 Lecture du fichier :  mesh_input
 Fin de la lecture :  mesh_input
 Pas de fichier "partition_input/domain_number_8" disponible;

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

 Partitionnement par courbe fractale : Morton (dans boîte englobante).
  Nombre de cellules par domaine (histogramme) :
    [       9334 ;       9334 ] =          8

 Écriture du fichier : partition_output/domain_number_8
 Fin de l'écriture :  partition_output/domain_number_8

 Partitionnement terminé (0.481 s)


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

  -1: nom: results
      répertoire: postprocessing
      format: EnSight Gold
      options: binary
      dépendence en temps: maillage fixe
      sorties: tous les 50 pas de temps et à la fin du calcul


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

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

 Création de l'interface entre faces
 Création de l'interface entre sommets
 Création des halos
 Définition des halos
    Définition du halo local
    Création du halo distant
    Mise à jour de la connectivité faces -> cellules

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

    valeur minimale =             9334
    valeur maximale =             9334

      1 : [       9334 ;       9334 ] =          8

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

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

    valeur minimale =             9477
    valeur maximale =             9699

      1 : [       9477 ;       9521 [ =          2
      2 : [       9521 ;       9565 [ =          1
      3 : [       9565 ;       9610 [ =          3
      4 : [       9610 ;       9654 [ =          0
      5 : [       9654 ;       9699 ] =          2

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

 Histogramme de la distribution des cellules fantômes sur les rangs :

    valeur minimale =              143
    valeur maximale =              365

      1 : [        143 ;        187 [ =          2
      2 : [        187 ;        231 [ =          1
      3 : [        231 ;        276 [ =          3
      4 : [        276 ;        320 [ =          0
      5 : [        320 ;        365 ] =          2

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

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

    valeur minimale =            14006
    valeur maximale =            16931

      1 : [      14006 ;      14591 [ =          2
      2 : [      14591 ;      15176 [ =          1
      3 : [      15176 ;      15761 [ =          2
      4 : [      15761 ;      16346 [ =          1
      5 : [      16346 ;      16931 ] =          2

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

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

    valeur minimale =            18798
    valeur maximale =            19353

      1 : [      18798 ;      18909 [ =          3
      2 : [      18909 ;      19020 [ =          3
      3 : [      19020 ;      19131 [ =          1
      4 : [      19131 ;      19242 [ =          0
      5 : [      19242 ;      19353 ] =          1

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

 Histogramme du nombre de faces internes par cellule :

    valeur minimale =                1
    valeur maximale =                4

      1 : [          1 ;          2 [ =          6
      2 : [          2 ;          3 [ =       1228
      3 : [          3 ;          4 ] =      73438

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

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

    valeur minimale =                3
    valeur maximale =                6

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

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

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

 Renumérotation du maillage:

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

 Coordonnées du maillage         minimale    et maximale
                       X : -2.5000000e+02  5.0000000e+02
                       Y : -1.7500000e+02  1.7500000e+02
                       Z :  0.0000000e+00  1.0000000e+00
 Maillage
     Nombre de cellules :       74672
     Nombre de faces internes : 122132
     Nombre de faces de bord :  151862
     Nombre de sommets :        99956

 Groupes :
    "DEFORMABLEFaces"
       faces de bord :            39934
    "FIXEDFaces"
       faces de bord :             2812
    "FLUIDVolumes"
       cellules :                 74672
    "INLETFaces"
       faces de bord :               41
    "OUTFLOWFaces"
       faces de bord :               41
    "RIGIDFaces"
       faces de bord :           106598
    "SYMMFaces"
       faces de bord :              182
    "WALLFaces"
       faces de bord :             2254

 --- Information sur les volumes
       Volume de controle minimal =  4.4500823e-05
       Volume de controle maximal =  8.2201854e+01
       Volume total du domaine    =  2.6228650e+05

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

  Critère 2 : décentrement :
    Nombre de mauvaises cellules détecté : 14 -->   0 %

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

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

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

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

    Le maillage devrait être revu en fonction des critères indiqués.

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

 Calcul des grandeurs géométriques (0.0179 s)
                                                             

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


 ** 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
  TurbEner          0.1500E-05  0.1500E-05
  omega             0.3062E-03  0.3062E-03
 ---------------------------------

  Local Time Step   0.3000E+00  0.3000E+00
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.300000000E+00   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  Density           0.1225E+01  0.1225E+01
  LamVisc           0.1830E-04  0.1830E-04
  TurbVisc          0.6001E-02  0.6001E-02
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2          41
Smooth wall               5        2254
Rough wall                6           0
Symmetry                  4      149526
Free outlet               3          41
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.50000E+03   0.00000E+00   0.50000E+00



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41         0.000000000E+00
Smooth wall               5        2254         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         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     :       2254
   Total number of wall faces                   :       2254
------------------------------------------------------------


                                                             
 ** WALL DISTANCE                                            
    -------------                                            
                                                             
  Min distance =    0.21879E-02 Max distance =    0.59268E+03
                                                             
     (Distance calculation done in       1818 iterations)


   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.33522E+01     980   0.15006E+01   0.10000E+01 
c  VelocityX    0.35804E-02       3   0.10000E+01   0.76293E-02 
c  VelocityY    0.35804E-02       3   0.10000E+01   0.13053E-05 
c  VelocityZ    0.35804E-02       3   0.10000E+01   0.32301E-30 
c  TurbEner     0.20535E-01       5   0.25764E-03   0.20440E-16 
c  omega        0.59233E+04      30   0.10000E+01   0.71281E+04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure     0.68130E+00   0.14632E+03         --         -- 
v  VelocityX   -0.57060E-01   0.11109E+00         --         -- 
v  VelocityY   -0.13762E+00   0.11828E+00         --         -- 
v  VelocityZ   -0.96402E-14   0.65512E-14         --         -- 
v  TurbEner     0.47015E-06   0.15000E-05          0          0 
v  omega        0.30618E-03   0.41226E+06          0          0 
v  TurbVisc     0.60012E-02   0.60012E-02          0          0 
v  CourantNb    0.00000E+00   0.00000E+00          0          0 
v  FourierNb    0.41060E-04   0.14218E+03          0          0 
v  total_pressu 0.10133E+06   0.10147E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.28792E-07   0.15000E-05          0          0 
a  omega        0.30618E-03   0.58895E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.19080E+03 -0.17105E+03  0.50000E+00  
Courant max  0.00000E+00 -0.19080E+03 -0.17105E+03  0.50000E+00  
Fourier min  0.41060E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.14218E+03  0.28864E+02  0.11082E+01  0.50000E+00  
Cou_Fou min  0.41060E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.14218E+03  0.28864E+02  0.11082E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                1:        0.78627E+00

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


 INSTANT    0.600000000E+00   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214365110E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72066E-01 0.37527E-01
   Friction velocity        uet   :  0.94890E-05 0.20623E-01
   Friction velocity        uk    :  0.00000E+00 0.10995E-01
   Dimensionless distance   yplus :  0.26680E-02 0.13139E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        517
   Nb of faces within the viscous sub-layer     :       1220
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.33142E+01    1083   0.31790E+01   0.25126E+01 
c  VelocityX    0.13045E+04       4   0.49999E+00   0.54966E-04 
c  VelocityY    0.13045E+04       4   0.49999E+00   0.24756E-05 
c  VelocityZ    0.13045E+04       4   0.49999E+00   0.57624E-31 
c  TurbEner     0.20534E-01       2   0.14701E-02   0.97505E-16 
c  omega        0.11479E+04       7   0.22741E+04   0.34817E+04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure     0.53962E-01   0.11975E+02         --         -- 
v  VelocityX   -0.63574E-01   0.11484E+00         --         -- 
v  VelocityY   -0.10725E+00   0.73756E-01         --         -- 
v  VelocityZ   -0.11318E-13   0.10789E-13         --         -- 
v  TurbEner     0.14108E-06   0.15275E-05         12          0 
v  omega        0.91862E-04   0.12371E+06         98          0 
v  TurbVisc     0.13970E-11   0.60012E-02          0          0 
v  CourantNb    0.00000E+00   0.78428E+01          0          0 
v  FourierNb    0.54076E-04   0.10924E+01          0          0 
v  total_pressu 0.10133E+06   0.10134E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.43471E-09   0.15392E-05         12          0 
a  omega       -0.12166E+02   0.75048E+02         98          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.78428E+01  0.28864E+02  0.11082E+01  0.50000E+00  
Fourier min  0.54076E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.10924E+01 -0.11207E+02  0.27859E+01  0.50000E+00  
Cou_Fou min  0.15707E-02 -0.60250E+02 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.82751E+01  0.28864E+02  0.11082E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                2:        0.55862E+00

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


 INSTANT    0.900000000E+00   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.129680744E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214378441E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76293E-01 0.26573E-01
   Friction velocity        uet   :  0.39771E-05 0.15510E-01
   Friction velocity        uk    :  0.00000E+00 0.11166E-01
   Dimensionless distance   yplus :  0.18948E-02 0.13416E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        565
   Nb of faces within the viscous sub-layer     :       1258
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.22288E+01     906   0.12198E+01   0.27017E+01 
c  VelocityX    0.76034E+03       3   0.75273E-01   0.86905E-05 
c  VelocityY    0.76034E+03       3   0.75273E-01   0.17291E-06 
c  VelocityZ    0.76034E+03       3   0.75273E-01   0.18446E-32 
c  TurbEner     0.20534E-01       2   0.25590E-03   0.13535E-16 
c  omega        0.36188E+03       8   0.64989E+03   0.31334E+03 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.47418E+01  -0.23077E-01         --         -- 
v  VelocityX   -0.47003E-01   0.10339E+00         --         -- 
v  VelocityY   -0.86960E-01   0.64082E-01         --         -- 
v  VelocityZ   -0.10026E-13   0.97324E-14         --         -- 
v  TurbEner     0.42353E-07   0.15659E-05         15          0 
v  omega        0.21173E-03   0.37145E+05          5          0 
v  TurbVisc     0.13970E-11   0.60023E-02          0          0 
v  CourantNb    0.67631E-06   0.47083E+01          0          0 
v  FourierNb    0.54076E-04   0.79540E+00          0          0 
v  total_pressu 0.10132E+06   0.10132E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.92748E-09   0.15824E-05         15          0 
a  omega       -0.88749E+02   0.17816E+03          5          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.67631E-06  0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.47083E+01  0.28860E+02  0.11130E+01  0.50000E+00  
Fourier min  0.54076E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.79540E+00  0.19507E+02  0.28508E+01  0.50000E+00  
Cou_Fou min  0.15781E-02  0.15608E+03  0.17115E+03  0.50000E+00  
Cou_Fou max  0.51059E+01  0.28860E+02  0.11130E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                3:        0.49440E+00

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


 INSTANT    0.120000000E+01   TIME STEP NUMBER               4
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.757035697E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214377280E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72410E-01 0.23065E-01
   Friction velocity        uet   :  0.61513E-05 0.14355E-01
   Friction velocity        uk    :  0.00000E+00 0.10283E-01
   Dimensionless distance   yplus :  0.17295E-02 0.13161E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        521
   Nb of faces within the viscous sub-layer     :       1271
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.45127E+00     795   0.14216E+00   0.73675E+00 
c  VelocityX    0.66612E+03       3   0.33712E-01   0.59973E-06 
c  VelocityY    0.66612E+03       3   0.33712E-01   0.62328E-07 
c  VelocityZ    0.66612E+03       3   0.33712E-01   0.20105E-33 
c  TurbEner     0.20533E-01       2   0.21873E-03   0.40916E-17 
c  omega        0.13090E+03       9   0.16223E+03   0.28166E+02 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.93261E+00  -0.39703E-02         --         -- 
v  VelocityX   -0.34070E-01   0.97914E-01         --         -- 
v  VelocityY   -0.79815E-01   0.61201E-01         --         -- 
v  VelocityZ   -0.88815E-14   0.87798E-14         --         -- 
v  TurbEner     0.12736E-07   0.16014E-05         14          0 
v  omega        0.25929E-03   0.11185E+05          4          0 
v  TurbVisc     0.13968E-11   0.60118E-02          0          0 
v  CourantNb    0.85749E-06   0.42456E+01          0          0 
v  FourierNb    0.54076E-04   0.83062E+00          0          0 
v  total_pressu 0.10132E+06   0.10132E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.12811E-08   0.16165E-05         14          0 
a  omega       -0.83408E+02   0.22195E+03          4          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.85749E-06  0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.42456E+01  0.28871E+02  0.11111E+01  0.50000E+00  
Fourier min  0.54076E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.83062E+00  0.19637E+02  0.27434E+01  0.50000E+00  
Cou_Fou min  0.15808E-02  0.18558E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.46172E+01  0.28871E+02  0.11111E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                4:        0.45223E+00

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


 INSTANT    0.150000000E+01   TIME STEP NUMBER               5
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.444057023E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214373432E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71501E-01 0.23017E-01
   Friction velocity        uet   :  0.53148E-05 0.14058E-01
   Friction velocity        uk    :  0.00000E+00 0.98271E-02
   Dimensionless distance   yplus :  0.14943E-02 0.13101E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        507
   Nb of faces within the viscous sub-layer     :       1274
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.20139E+00     672   0.14269E+00   0.41339E+00 
c  VelocityX    0.67977E+03       3   0.10053E-01   0.12013E-06 
c  VelocityY    0.67977E+03       3   0.10053E-01   0.19234E-08 
c  VelocityZ    0.67977E+03       3   0.10053E-01   0.33570E-34 
c  TurbEner     0.20533E-01       2   0.21777E-03   0.35006E-17 
c  omega        0.64743E+02      11   0.29745E+02   0.24849E+01 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure     0.63047E-03   0.14447E+00         --         -- 
v  VelocityX   -0.32394E-01   0.96835E-01         --         -- 
v  VelocityY   -0.84227E-01   0.61203E-01         --         -- 
v  VelocityZ   -0.78683E-14   0.79214E-14         --         -- 
v  TurbEner     0.38510E-08   0.16319E-05          3          0 
v  omega        0.27171E-03   0.34265E+04          5          0 
v  TurbVisc     0.13949E-11   0.60080E-02          0          0 
v  CourantNb    0.00000E+00   0.41449E+01          0          0 
v  FourierNb    0.54076E-04   0.83168E+00          0          0 
v  total_pressu 0.10133E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.82014E-09   0.19268E-05          3          0 
a  omega       -0.48562E+02   0.28068E+03          5          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.41449E+01  0.28871E+02  0.11111E+01  0.50000E+00  
Fourier min  0.54076E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.83168E+00  0.28685E+02  0.23094E+01  0.50000E+00  
Cou_Fou min  0.15804E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.45166E+01  0.28871E+02  0.11111E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                5:        0.41004E+00

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


 INSTANT    0.180000000E+01   TIME STEP NUMBER               6
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.361047794E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214373806E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70746E-01 0.22892E-01
   Friction velocity        uet   :  0.18139E-05 0.13925E-01
   Friction velocity        uk    :  0.00000E+00 0.97353E-02
   Dimensionless distance   yplus :  0.51506E-03 0.13050E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        498
   Nb of faces within the viscous sub-layer     :       1277
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.10936E+00     399   0.54916E-01   0.26464E+00 
c  VelocityX    0.68411E+03       2   0.49028E-02   0.57826E-07 
c  VelocityY    0.68411E+03       2   0.49028E-02   0.49716E-09 
c  VelocityZ    0.68411E+03       2   0.49028E-02   0.30305E-34 
c  TurbEner     0.20532E-01       2   0.21716E-03   0.43526E-17 
c  omega        0.46587E+02      12   0.36817E+01   0.18603E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.65730E-02   0.82676E-01         --         -- 
v  VelocityX   -0.32945E-01   0.96506E-01         --         -- 
v  VelocityY   -0.82685E-01   0.61151E-01         --         -- 
v  VelocityZ   -0.69718E-14   0.71477E-14         --         -- 
v  TurbEner     0.11847E-08   0.26025E-05          2          0 
v  omega        0.27482E-03   0.11958E+04          6          0 
v  TurbVisc     0.13767E-11   0.60153E-02          0          0 
v  CourantNb    0.00000E+00   0.40875E+01          0          0 
v  FourierNb    0.54076E-04   0.10753E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.21741E-09   0.30311E-05          2          0 
a  omega       -0.58595E+02   0.67868E+03          6          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.40875E+01  0.28871E+02  0.11111E+01  0.50000E+00  
Fourier min  0.54076E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.10753E+01 -0.25286E+02 -0.69474E+00  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.44592E+01  0.28871E+02  0.11111E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                6:        0.30799E+00

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


 INSTANT    0.210000000E+01   TIME STEP NUMBER               7
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.185923732E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214376010E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70912E-01 0.22110E-01
   Friction velocity        uet   :  0.47655E-05 0.13975E-01
   Friction velocity        uk    :  0.00000E+00 0.97238E-02
   Dimensionless distance   yplus :  0.10533E-02 0.13061E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        489
   Nb of faces within the viscous sub-layer     :       1284
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.67109E-01     384   0.36654E-01   0.18299E+00 
c  VelocityX    0.68407E+03       2   0.37916E-02   0.43348E-07 
c  VelocityY    0.68407E+03       2   0.37916E-02   0.11590E-09 
c  VelocityZ    0.68407E+03       2   0.37916E-02   0.30461E-34 
c  TurbEner     0.20532E-01       2   0.21973E-03   0.49265E-17 
c  omega        0.42008E+02      12   0.35097E+00   0.15101E-01 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.31397E-01   0.45261E-01         --         -- 
v  VelocityX   -0.32910E-01   0.96029E-01         --         -- 
v  VelocityY   -0.82296E-01   0.61447E-01         --         -- 
v  VelocityZ   -0.62199E-14   0.64502E-14         --         -- 
v  TurbEner     0.38058E-09   0.40497E-05          1          0 
v  omega        0.27645E-03   0.88772E+03          8          0 
v  TurbVisc     0.12136E-11   0.60333E-02          0          0 
v  CourantNb    0.13948E-06   0.39390E+01          0          0 
v  FourierNb    0.54075E-04   0.11336E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.12477E-10   0.47491E-05          1          0 
a  omega       -0.13282E+03   0.91822E+03          8          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.13948E-06  0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.39390E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.11336E+01  0.28654E+02  0.23525E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.42643E+01  0.28871E+02  0.11111E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                7:        0.30388E+00

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


 INSTANT    0.240000000E+01   TIME STEP NUMBER               8
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.510906451E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375925E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71286E-01 0.22354E-01
   Friction velocity        uet   :  0.18060E-05 0.14180E-01
   Friction velocity        uk    :  0.00000E+00 0.96921E-02
   Dimensionless distance   yplus :  0.28728E-03 0.13087E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        481
   Nb of faces within the viscous sub-layer     :       1290
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.53655E-01     134   0.32855E-01   0.16420E+00 
c  VelocityX    0.68409E+03       2   0.31077E-02   0.29349E-07 
c  VelocityY    0.68409E+03       2   0.31077E-02   0.60010E-10 
c  VelocityZ    0.68409E+03       2   0.31077E-02   0.28593E-34 
c  TurbEner     0.20531E-01       2   0.22203E-03   0.51945E-17 
c  omega        0.40960E+02      12   0.11395E+00   0.26439E-02 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.36394E-01   0.30757E-01         --         -- 
v  VelocityX   -0.32970E-01   0.95486E-01         --         -- 
v  VelocityY   -0.82707E-01   0.61484E-01         --         -- 
v  VelocityZ   -0.58302E-14   0.58214E-14         --         -- 
v  TurbEner     0.12587E-09   0.57422E-05          0          0 
v  omega        0.27844E-03   0.89252E+03          8          0 
v  TurbVisc     0.57017E-12   0.60346E-02          0          0 
v  CourantNb    0.14941E-06   0.39880E+01          0          0 
v  FourierNb    0.54075E-04   0.12284E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.90813E-11   0.64676E-05          0          0 
a  omega       -0.12984E+03   0.92460E+03          8          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.14941E-06  0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.39880E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.12284E+01 -0.22071E+02  0.33369E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.43064E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                8:        0.21173E+00

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


 INSTANT    0.270000000E+01   TIME STEP NUMBER               9
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.577726101E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375745E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71159E-01 0.18405E-01
   Friction velocity        uet   :  0.10934E-05 0.14151E-01
   Friction velocity        uk    :  0.00000E+00 0.96176E-02
   Dimensionless distance   yplus :  0.30742E-03 0.13078E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        476
   Nb of faces within the viscous sub-layer     :       1293
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.42133E-01      84   0.28580E-01   0.14284E+00 
c  VelocityX    0.68405E+03       2   0.25459E-02   0.20972E-07 
c  VelocityY    0.68405E+03       2   0.25459E-02   0.36591E-10 
c  VelocityZ    0.68405E+03       2   0.25459E-02   0.27375E-34 
c  TurbEner     0.20531E-01       2   0.22326E-03   0.52644E-17 
c  omega        0.40368E+02      12   0.72587E-01   0.88119E-03 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.29580E-01   0.27654E-01         --         -- 
v  VelocityX   -0.33061E-01   0.94990E-01         --         -- 
v  VelocityY   -0.82036E-01   0.61491E-01         --         -- 
v  VelocityZ   -0.57780E-14   0.52545E-14         --         -- 
v  TurbEner     0.41401E-10   0.73665E-05          0          0 
v  omega        0.28072E-03   0.87626E+03          8          0 
v  TurbVisc     0.17276E-12   0.61141E-02          0          0 
v  CourantNb    0.69288E-07   0.40282E+01          0          0 
v  FourierNb    0.54075E-04   0.18533E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.31537E-12   0.80626E-05          0          0 
a  omega       -0.11413E+03   0.88087E+03          8          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.69288E-07  0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.40282E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.18533E+01  0.24039E+01  0.40054E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.43466E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                9:        0.19570E+00

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


 INSTANT    0.300000000E+01   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.213134665E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374360E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70969E-01 0.18237E-01
   Friction velocity        uet   :  0.25903E-05 0.14329E-01
   Friction velocity        uk    :  0.00000E+00 0.95816E-02
   Dimensionless distance   yplus :  0.72831E-03 0.13065E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        468
   Nb of faces within the viscous sub-layer     :       1296
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.33971E-01     100   0.25242E-01   0.12616E+00 
c  VelocityX    0.68409E+03       2   0.21472E-02   0.15459E-07 
c  VelocityY    0.68409E+03       2   0.21472E-02   0.26687E-10 
c  VelocityZ    0.68409E+03       2   0.21472E-02   0.26353E-34 
c  TurbEner     0.20530E-01       2   0.22407E-03   0.52170E-17 
c  omega        0.40032E+02      13   0.53784E-01   0.42638E-03 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.23604E-01   0.26532E-01         --         -- 
v  VelocityX   -0.33125E-01   0.94533E-01         --         -- 
v  VelocityY   -0.80633E-01   0.61467E-01         --         -- 
v  VelocityZ   -0.57279E-14   0.47432E-14         --         -- 
v  TurbEner     0.13671E-10   0.88556E-05         27          0 
v  omega        0.28321E-03   0.87595E+03         14          0 
v  TurbVisc     0.58568E-13   0.60802E-02          0          0 
v  CourantNb    0.00000E+00   0.40466E+01          0          0 
v  FourierNb    0.54075E-04   0.13165E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.50552E-10   0.94938E-05         27          0 
a  omega       -0.12334E+03   0.87812E+03         14          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.40466E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.13165E+01  0.16509E+01  0.40330E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.43649E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               10:        0.20297E+00

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


 INSTANT    0.330000000E+01   TIME STEP NUMBER              11
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.300484938E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374356E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70725E-01 0.17592E-01
   Friction velocity        uet   :  0.49645E-06 0.14225E-01
   Friction velocity        uk    :  0.00000E+00 0.95622E-02
   Dimensionless distance   yplus :  0.13958E-03 0.13049E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        463
   Nb of faces within the viscous sub-layer     :       1295
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27994E-01      74   0.22573E-01   0.11282E+00 
c  VelocityX    0.68416E+03       2   0.18592E-02   0.12064E-07 
c  VelocityY    0.68416E+03       2   0.18592E-02   0.22968E-10 
c  VelocityZ    0.68416E+03       2   0.18592E-02   0.25539E-34 
c  TurbEner     0.20530E-01       2   0.22459E-03   0.51192E-17 
c  omega        0.39816E+02      13   0.42522E-01   0.22422E-03 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.19892E-01   0.25289E-01         --         -- 
v  VelocityX   -0.33043E-01   0.94135E-01         --         -- 
v  VelocityY   -0.79558E-01   0.61658E-01         --         -- 
v  VelocityZ   -0.56794E-14   0.44081E-14         --         -- 
v  TurbEner     0.45128E-11   0.10183E-04        130          0 
v  omega        0.28586E-03   0.87923E+03         19          0 
v  TurbVisc     0.19151E-13   0.60602E-02          0          0 
v  CourantNb    0.00000E+00   0.40827E+01          0          0 
v  FourierNb    0.54075E-04   0.14547E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.43514E-07   0.10752E-04        130          0 
a  omega       -0.12071E+03   0.88063E+03         19          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.40827E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.14547E+01  0.16509E+01  0.40330E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.44011E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               11:        0.18937E+00

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


 INSTANT    0.360000000E+01   TIME STEP NUMBER              12
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.382858892E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374641E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70547E-01 0.16760E-01
   Friction velocity        uet   :  0.12732E-05 0.14342E-01
   Friction velocity        uk    :  0.00000E+00 0.95076E-02
   Dimensionless distance   yplus :  0.34699E-03 0.13037E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        459
   Nb of faces within the viscous sub-layer     :       1299
   Total number of wall faces                   :       2254
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         12, 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 auxilliary restart file
      -----------------------------------

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


 Time for restart files:    0.87719E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23236E-01      59   0.20197E-01   0.10107E+00 
c  VelocityX    0.68422E+03       2   0.16337E-02   0.95727E-08 
c  VelocityY    0.68422E+03       2   0.16337E-02   0.21279E-10 
c  VelocityZ    0.68422E+03       2   0.16337E-02   0.24902E-34 
c  TurbEner     0.20529E-01       2   0.22491E-03   0.50075E-17 
c  omega        0.39671E+02      13   0.38115E-01   0.19102E-03 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.17734E-01   0.22557E-01         --         -- 
v  VelocityX   -0.32812E-01   0.93725E-01         --         -- 
v  VelocityY   -0.79878E-01   0.61790E-01         --         -- 
v  VelocityZ   -0.56325E-14   0.43723E-14         --         -- 
v  TurbEner     0.14898E-11   0.11340E-04        242          0 
v  omega        0.28862E-03   0.88164E+03         21          0 
v  TurbVisc     0.63424E-14   0.60811E-02          0          0 
v  CourantNb    0.00000E+00   0.40698E+01          0          0 
v  FourierNb    0.54075E-04   0.17026E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.31637E-07   0.11836E-04        242          0 
a  omega       -0.12217E+03   0.88268E+03         21          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.40698E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.17026E+01  0.16509E+01  0.40330E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.43882E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               12:        0.27342E+00

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


 INSTANT    0.390000000E+01   TIME STEP NUMBER              13
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.121093948E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374986E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69946E-01 0.16735E-01
   Friction velocity        uet   :  0.10142E-05 0.14227E-01
   Friction velocity        uk    :  0.00000E+00 0.94763E-02
   Dimensionless distance   yplus :  0.19397E-03 0.12996E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        453
   Nb of faces within the viscous sub-layer     :       1300
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.19821E-01      42   0.18508E-01   0.92600E-01 
c  VelocityX    0.68426E+03       2   0.14516E-02   0.77307E-08 
c  VelocityY    0.68426E+03       2   0.14516E-02   0.20307E-10 
c  VelocityZ    0.68426E+03       2   0.14516E-02   0.24231E-34 
c  TurbEner     0.20528E-01       2   0.22509E-03   0.48881E-17 
c  omega        0.39569E+02      14   0.32045E-01   0.10498E-03 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.15612E-01   0.20465E-01         --         -- 
v  VelocityX   -0.32575E-01   0.93345E-01         --         -- 
v  VelocityY   -0.80384E-01   0.61373E-01         --         -- 
v  VelocityZ   -0.55872E-14   0.43368E-14         --         -- 
v  TurbEner     0.49157E-12   0.12351E-04        212          0 
v  omega        0.29005E-03   0.88392E+03         25          0 
v  TurbVisc     0.20916E-14   0.60997E-02          0          0 
v  CourantNb    0.00000E+00   0.40953E+01          0          0 
v  FourierNb    0.54075E-04   0.16045E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.22608E-07   0.12784E-04        212          0 
a  omega       -0.12001E+03   0.88490E+03         25          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.26218E+02  0.11491E+01  0.50000E+00  
Courant max  0.40953E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.16045E+01  0.16509E+01  0.40330E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.44137E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               13:        0.17885E+00

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


 INSTANT    0.420000000E+01   TIME STEP NUMBER              14
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.158805443E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375176E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69378E-01 0.16703E-01
   Friction velocity        uet   :  0.34512E-06 0.14320E-01
   Friction velocity        uk    :  0.00000E+00 0.94614E-02
   Dimensionless distance   yplus :  0.15561E-03 0.12958E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :       1298
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.17208E-01      42   0.17184E-01   0.85979E-01 
c  VelocityX    0.68431E+03       2   0.13038E-02   0.63446E-08 
c  VelocityY    0.68431E+03       2   0.13038E-02   0.21194E-10 
c  VelocityZ    0.68431E+03       2   0.13038E-02   0.23715E-34 
c  TurbEner     0.20528E-01       2   0.22516E-03   0.47660E-17 
c  omega        0.39489E+02      14   0.28095E-01   0.61588E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.14453E-01   0.18658E-01         --         -- 
v  VelocityX   -0.32270E-01   0.92951E-01         --         -- 
v  VelocityY   -0.80661E-01   0.61463E-01         --         -- 
v  VelocityZ   -0.55421E-14   0.43016E-14         --         -- 
v  TurbEner     0.16212E-12   0.13246E-04        143          0 
v  omega        0.29109E-03   0.88608E+03         28          0 
v  TurbVisc     0.69036E-15   0.60954E-02          0          0 
v  CourantNb    0.00000E+00   0.40579E+01          0          0 
v  FourierNb    0.54075E-04   0.12865E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.14159E-07   0.13630E-04        143          0 
a  omega       -0.12252E+03   0.88701E+03         28          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.28160E+02  0.10987E+01  0.50000E+00  
Courant max  0.40579E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.12865E+01  0.16509E+01  0.40330E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.43763E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               14:        0.18292E+00

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


 INSTANT    0.450000000E+01   TIME STEP NUMBER              15
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.681332127E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375189E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68896E-01 0.16688E-01
   Friction velocity        uet   :  0.28688E-06 0.14187E-01
   Friction velocity        uk    :  0.00000E+00 0.94107E-02
   Dimensionless distance   yplus :  0.80660E-04 0.12925E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        443
   Nb of faces within the viscous sub-layer     :       1300
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.15089E-01      45   0.16101E-01   0.80381E-01 
c  VelocityX    0.68435E+03       2   0.11794E-02   0.52966E-08 
c  VelocityY    0.68435E+03       2   0.11794E-02   0.22402E-10 
c  VelocityZ    0.68435E+03       2   0.11794E-02   0.23147E-34 
c  TurbEner     0.20527E-01       2   0.22510E-03   0.46531E-17 
c  omega        0.39430E+02      14   0.27616E-01   0.75745E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.13664E-01   0.17395E-01         --         -- 
v  VelocityX   -0.32017E-01   0.92598E-01         --         -- 
v  VelocityY   -0.81008E-01   0.61018E-01         --         -- 
v  VelocityZ   -0.54979E-14   0.42667E-14         --         -- 
v  TurbEner     0.53458E-13   0.14059E-04        108          0 
v  omega        0.29209E-03   0.88820E+03         28          0 
v  TurbVisc     0.22766E-15   0.60913E-02          0          0 
v  CourantNb    0.00000E+00   0.40683E+01          0          0 
v  FourierNb    0.54075E-04   0.11634E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.95157E-08   0.14408E-04        108          0 
a  omega       -0.11972E+03   0.88910E+03         28          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.40683E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.11634E+01  0.28669E+02  0.24086E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.43866E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               15:        0.18036E+00

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


 INSTANT    0.480000000E+01   TIME STEP NUMBER              16
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.405622903E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375108E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68435E-01 0.16667E-01
   Friction velocity        uet   :  0.10854E-05 0.14280E-01
   Friction velocity        uk    :  0.00000E+00 0.93944E-02
   Dimensionless distance   yplus :  0.30519E-03 0.12894E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        438
   Nb of faces within the viscous sub-layer     :       1301
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13377E-01      41   0.15170E-01   0.75779E-01 
c  VelocityX    0.68439E+03       2   0.10770E-02   0.44888E-08 
c  VelocityY    0.68439E+03       2   0.10770E-02   0.24172E-10 
c  VelocityZ    0.68439E+03       2   0.10770E-02   0.22633E-34 
c  TurbEner     0.20527E-01       2   0.22500E-03   0.45853E-17 
c  omega        0.39389E+02      14   0.27277E-01   0.65667E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.12970E-01   0.16189E-01         --         -- 
v  VelocityX   -0.31780E-01   0.92251E-01         --         -- 
v  VelocityY   -0.79607E-01   0.61053E-01         --         -- 
v  VelocityZ   -0.54551E-14   0.42321E-14         --         -- 
v  TurbEner     0.17634E-13   0.14932E-04         90          0 
v  omega        0.29304E-03   0.89012E+03         30          0 
v  TurbVisc     0.75071E-16   0.60873E-02          0          0 
v  CourantNb    0.00000E+00   0.40326E+01          0          0 
v  FourierNb    0.54075E-04   0.11509E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.57255E-08   0.15463E-04         90          0 
a  omega       -0.12254E+03   0.89094E+03         30          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.26119E+02  0.11509E+01  0.50000E+00  
Courant max  0.40326E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.11509E+01  0.28669E+02  0.24086E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.43510E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               16:        0.17932E+00

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


 INSTANT    0.510000000E+01   TIME STEP NUMBER              17
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.331719278E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375015E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68069E-01 0.16695E-01
   Friction velocity        uet   :  0.23679E-06 0.14143E-01
   Friction velocity        uk    :  0.00000E+00 0.93533E-02
   Dimensionless distance   yplus :  0.64533E-04 0.12869E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        433
   Nb of faces within the viscous sub-layer     :       1301
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.12020E-01      45   0.14506E-01   0.72278E-01 
c  VelocityX    0.68442E+03       2   0.98905E-03   0.38339E-08 
c  VelocityY    0.68442E+03       2   0.98905E-03   0.26757E-10 
c  VelocityZ    0.68442E+03       2   0.98905E-03   0.22204E-34 
c  TurbEner     0.20526E-01       2   0.22487E-03   0.44815E-17 
c  omega        0.39354E+02      14   0.23675E-01   0.26413E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.12187E-01   0.15195E-01         --         -- 
v  VelocityX   -0.31628E-01   0.91949E-01         --         -- 
v  VelocityY   -0.79049E-01   0.60861E-01         --         -- 
v  VelocityZ   -0.54121E-14   0.41978E-14         --         -- 
v  TurbEner     0.58244E-14   0.16149E-04         72          0 
v  omega        0.29396E-03   0.89175E+03         33          0 
v  TurbVisc     0.24763E-16   0.60834E-02          0          0 
v  CourantNb    0.00000E+00   0.40368E+01          0          0 
v  FourierNb    0.54075E-04   0.15833E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.36015E-08   0.16671E-04         72          0 
a  omega       -0.11839E+03   0.89245E+03         33          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.40368E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.15833E+01 -0.25857E+02 -0.44507E+00  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.43552E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               17:        0.18105E+00

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


 INSTANT    0.540000000E+01   TIME STEP NUMBER              18
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.650402189E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374927E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67407E-01 0.16727E-01
   Friction velocity        uet   :  0.51390E-06 0.14240E-01
   Friction velocity        uk    :  0.00000E+00 0.93386E-02
   Dimensionless distance   yplus :  0.81744E-04 0.12823E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        428
   Nb of faces within the viscous sub-layer     :       1303
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.10873E-01      41   0.13883E-01   0.69275E-01 
c  VelocityX    0.68446E+03       2   0.91407E-03   0.32964E-08 
c  VelocityY    0.68446E+03       2   0.91407E-03   0.28796E-10 
c  VelocityZ    0.68446E+03       2   0.91407E-03   0.21742E-34 
c  TurbEner     0.20526E-01       2   0.22472E-03   0.43779E-17 
c  omega        0.39325E+02      14   0.23284E-01   0.36922E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.11504E-01   0.14175E-01         --         -- 
v  VelocityX   -0.31440E-01   0.91615E-01         --         -- 
v  VelocityY   -0.77873E-01   0.60866E-01         --         -- 
v  VelocityZ   -0.53702E-14   0.41638E-14         --         -- 
v  TurbEner     0.19289E-14   0.17358E-04         62          0 
v  omega        0.29483E-03   0.89328E+03         33          0 
v  TurbVisc     0.81792E-17   0.60796E-02          0          0 
v  CourantNb    0.00000E+00   0.40030E+01          0          0 
v  FourierNb    0.54075E-04   0.17382E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.19093E-08   0.17876E-04         62          0 
a  omega       -0.12301E+03   0.89393E+03         33          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.28160E+02  0.10987E+01  0.50000E+00  
Courant max  0.40030E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.17382E+01 -0.25857E+02 -0.44507E+00  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.43214E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               18:        0.18029E+00

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


 INSTANT    0.570000000E+01   TIME STEP NUMBER              19
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.254043710E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374875E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66831E-01 0.16755E-01
   Friction velocity        uet   :  0.83344E-06 0.14108E-01
   Friction velocity        uk    :  0.00000E+00 0.93008E-02
   Dimensionless distance   yplus :  0.13257E-03 0.12784E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        426
   Nb of faces within the viscous sub-layer     :       1305
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.99006E-02      42   0.13361E-01   0.66731E-01 
c  VelocityX    0.68449E+03       2   0.84727E-03   0.28528E-08 
c  VelocityY    0.68449E+03       2   0.84727E-03   0.30334E-10 
c  VelocityZ    0.68449E+03       2   0.84727E-03   0.21275E-34 
c  TurbEner     0.20525E-01       2   0.22455E-03   0.43369E-17 
c  omega        0.39302E+02      14   0.23261E-01   0.32812E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.10897E-01   0.13232E-01         --         -- 
v  VelocityX   -0.31311E-01   0.91309E-01         --         -- 
v  VelocityY   -0.77436E-01   0.60370E-01         --         -- 
v  VelocityZ   -0.53285E-14   0.41300E-14         --         -- 
v  TurbEner     0.64186E-15   0.18568E-04         57          0 
v  omega        0.29567E-03   0.89435E+03         33          0 
v  TurbVisc     0.27087E-17   0.60759E-02          0          0 
v  CourantNb    0.00000E+00   0.40131E+01          0          0 
v  FourierNb    0.54075E-04   0.18239E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.80482E-09   0.19175E-04         57          0 
a  omega       -0.11812E+03   0.89480E+03         33          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.27217E+02  0.11224E+01  0.50000E+00  
Courant max  0.40131E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.18239E+01 -0.25857E+02 -0.44507E+00  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.43315E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               19:        0.18091E+00

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


 INSTANT    0.600000000E+01   TIME STEP NUMBER              20
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.221155009E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374878E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66385E-01 0.16779E-01
   Friction velocity        uet   :  0.32859E-06 0.14197E-01
   Friction velocity        uk    :  0.00000E+00 0.92981E-02
   Dimensionless distance   yplus :  0.92387E-04 0.12753E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        422
   Nb of faces within the viscous sub-layer     :       1307
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.90662E-02      42   0.12926E-01   0.64553E-01 
c  VelocityX    0.68452E+03       2   0.78732E-03   0.24815E-08 
c  VelocityY    0.68452E+03       2   0.78732E-03   0.31459E-10 
c  VelocityZ    0.68452E+03       2   0.78732E-03   0.20882E-34 
c  TurbEner     0.20524E-01       2   0.22437E-03   0.42786E-17 
c  omega        0.39288E+02      14   0.24738E-01   0.58033E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.10345E-01   0.12351E-01         --         -- 
v  VelocityX   -0.31057E-01   0.91019E-01         --         -- 
v  VelocityY   -0.76558E-01   0.60573E-01         --         -- 
v  VelocityZ   -0.52871E-14   0.40965E-14         --         -- 
v  TurbEner     0.21529E-15   0.19997E-04         50          0 
v  omega        0.29648E-03   0.89503E+03         32          0 
v  TurbVisc     0.90135E-18   0.60541E-02          0          0 
v  CourantNb    0.00000E+00   0.39746E+01          0          0 
v  FourierNb    0.54075E-04   0.17955E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.93973E-09   0.20610E-04         50          0 
a  omega       -0.12263E+03   0.89532E+03         32          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.39746E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.17955E+01 -0.25857E+02 -0.44507E+00  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.42930E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               20:        0.18178E+00

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


 INSTANT    0.630000000E+01   TIME STEP NUMBER              21
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.101389844E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374911E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66017E-01 0.16798E-01
   Friction velocity        uet   :  0.66384E-06 0.14078E-01
   Friction velocity        uk    :  0.00000E+00 0.92515E-02
   Dimensionless distance   yplus :  0.16240E-03 0.12727E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        419
   Nb of faces within the viscous sub-layer     :       1306
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.83394E-02      42   0.12545E-01   0.62648E-01 
c  VelocityX    0.68455E+03       2   0.73346E-03   0.21657E-08 
c  VelocityY    0.68455E+03       2   0.73346E-03   0.32361E-10 
c  VelocityZ    0.68455E+03       2   0.73346E-03   0.20436E-34 
c  TurbEner     0.20524E-01       2   0.22418E-03   0.42641E-17 
c  omega        0.39272E+02      14   0.21385E-01   0.14584E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.98607E-02   0.11531E-01         --         -- 
v  VelocityX   -0.30729E-01   0.90737E-01         --         -- 
v  VelocityY   -0.76206E-01   0.60206E-01         --         -- 
v  VelocityZ   -0.52467E-14   0.40633E-14         --         -- 
v  TurbEner     0.73136E-16   0.21381E-04         44          0 
v  omega        0.29726E-03   0.89559E+03         32          0 
v  TurbVisc     0.30233E-18   0.60504E-02          0          0 
v  CourantNb    0.00000E+00   0.39885E+01          0          0 
v  FourierNb    0.54075E-04   0.18160E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.73097E-09   0.21974E-04         44          0 
a  omega       -0.11814E+03   0.89584E+03         32          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.39885E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.18160E+01 -0.25857E+02 -0.44507E+00  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.43069E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               21:        0.18284E+00

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


 INSTANT    0.660000000E+01   TIME STEP NUMBER              22
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.406205238E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374946E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65735E-01 0.16814E-01
   Friction velocity        uet   :  0.70879E-06 0.14161E-01
   Friction velocity        uk    :  0.00000E+00 0.92580E-02
   Dimensionless distance   yplus :  0.19929E-03 0.12708E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        413
   Nb of faces within the viscous sub-layer     :       1308
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.77011E-02      42   0.12209E-01   0.60967E-01 
c  VelocityX    0.68457E+03       2   0.68487E-03   0.18971E-08 
c  VelocityY    0.68457E+03       2   0.68487E-03   0.33193E-10 
c  VelocityZ    0.68457E+03       2   0.68487E-03   0.20085E-34 
c  TurbEner     0.20523E-01       2   0.22398E-03   0.41491E-17 
c  omega        0.39259E+02      13   0.20824E-01   0.13039E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.93933E-02   0.10794E-01         --         -- 
v  VelocityX   -0.30452E-01   0.90424E-01         --         -- 
v  VelocityY   -0.76002E-01   0.60212E-01         --         -- 
v  VelocityZ   -0.52063E-14   0.40304E-14         --         -- 
v  TurbEner     0.25336E-16   0.22749E-04         44          0 
v  omega        0.29800E-03   0.89591E+03         31          0 
v  TurbVisc     0.10270E-18   0.60487E-02          0          0 
v  CourantNb    0.00000E+00   0.39532E+01          0          0 
v  FourierNb    0.54075E-04   0.18157E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.14988E-08   0.23335E-04         44          0 
a  omega       -0.12224E+03   0.89605E+03         31          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.39532E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.18157E+01 -0.25857E+02 -0.44507E+00  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.42716E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               22:        0.18204E+00

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


 INSTANT    0.690000000E+01   TIME STEP NUMBER              23
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.115011192E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374969E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65163E-01 0.16827E-01
   Friction velocity        uet   :  0.12508E-06 0.14038E-01
   Friction velocity        uk    :  0.00000E+00 0.92045E-02
   Dimensionless distance   yplus :  0.34089E-04 0.12668E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        408
   Nb of faces within the viscous sub-layer     :       1310
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.71241E-02      41   0.11889E-01   0.59370E-01 
c  VelocityX    0.68460E+03       2   0.64097E-03   0.16700E-08 
c  VelocityY    0.68460E+03       2   0.64097E-03   0.33311E-10 
c  VelocityZ    0.68460E+03       2   0.64097E-03   0.19642E-34 
c  TurbEner     0.20523E-01       2   0.22377E-03   0.40801E-17 
c  omega        0.39245E+02      14   0.21228E-01   0.25312E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.89401E-02   0.10126E-01         --         -- 
v  VelocityX   -0.34906E-01   0.90143E-01         --         -- 
v  VelocityY   -0.76101E-01   0.59795E-01         --         -- 
v  VelocityZ   -0.51668E-14   0.39978E-14         --         -- 
v  TurbEner     0.90332E-17   0.24034E-04         31          0 
v  omega        0.29872E-03   0.89616E+03         30          0 
v  TurbVisc     0.35579E-19   0.60469E-02          0          0 
v  CourantNb    0.00000E+00   0.39613E+01          0          0 
v  FourierNb    0.54075E-04   0.18128E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.50554E-10   0.24585E-04         31          0 
a  omega       -0.11796E+03   0.89627E+03         30          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.26119E+02  0.11509E+01  0.50000E+00  
Courant max  0.39613E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.18128E+01 -0.25857E+02 -0.44507E+00  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.42797E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               23:        0.17422E+00

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


 INSTANT    0.720000000E+01   TIME STEP NUMBER              24
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.649621331E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374978E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64670E-01 0.16837E-01
   Friction velocity        uet   :  0.74294E-06 0.14133E-01
   Friction velocity        uk    :  0.00000E+00 0.92254E-02
   Dimensionless distance   yplus :  0.11818E-03 0.12633E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        403
   Nb of faces within the viscous sub-layer     :       1317
   Total number of wall faces                   :       2254
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         24, Physical time    0.72000E+01


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

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

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

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


 Time for restart files:    0.10010E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.66159E-02      42   0.11611E-01   0.57981E-01 
c  VelocityX    0.68462E+03       2   0.60112E-03   0.14755E-08 
c  VelocityY    0.68462E+03       2   0.60112E-03   0.33367E-10 
c  VelocityZ    0.68462E+03       2   0.60112E-03   0.19316E-34 
c  TurbEner     0.20522E-01       2   0.22357E-03   0.41271E-17 
c  omega        0.39241E+02      13   0.24757E-01   0.63917E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.85188E-02   0.95002E-02         --         -- 
v  VelocityX   -0.38477E-01   0.89873E-01         --         -- 
v  VelocityY   -0.74919E-01   0.60014E-01         --         -- 
v  VelocityZ   -0.51273E-14   0.39654E-14         --         -- 
v  TurbEner     0.33515E-17   0.25271E-04         32          0 
v  omega        0.29926E-03   0.89632E+03         30          0 
v  TurbVisc     0.12685E-19   0.60452E-02          0          0 
v  CourantNb    0.00000E+00   0.39301E+01          0          0 
v  FourierNb    0.54075E-04   0.18113E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.26954E-10   0.25802E-04         32          0 
a  omega       -0.12215E+03   0.89639E+03         30          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.39301E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.18113E+01 -0.25857E+02 -0.44507E+00  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.42484E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               24:        0.28011E+00

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


 INSTANT    0.750000000E+01   TIME STEP NUMBER              25
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.141745670E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374978E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64313E-01 0.16845E-01
   Friction velocity        uet   :  0.10939E-06 0.14009E-01
   Friction velocity        uk    :  0.00000E+00 0.91747E-02
   Dimensionless distance   yplus :  0.30756E-04 0.12608E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        398
   Nb of faces within the viscous sub-layer     :       1319
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61612E-02      42   0.11362E-01   0.56732E-01 
c  VelocityX    0.68464E+03       2   0.56475E-03   0.13084E-08 
c  VelocityY    0.68464E+03       2   0.56475E-03   0.33202E-10 
c  VelocityZ    0.68464E+03       2   0.56475E-03   0.18932E-34 
c  TurbEner     0.20521E-01       2   0.22336E-03   0.41734E-17 
c  omega        0.39231E+02      13   0.24159E-01   0.42468E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.81293E-02   0.89173E-02         --         -- 
v  VelocityX   -0.41214E-01   0.89626E-01         --         -- 
v  VelocityY   -0.74173E-01   0.59418E-01         --         -- 
v  VelocityZ   -0.50884E-14   0.39333E-14         --         -- 
v  TurbEner     0.13084E-17   0.26426E-04         31          0 
v  omega        0.29947E-03   0.89644E+03         30          0 
v  TurbVisc     0.47065E-20   0.60434E-02          0          0 
v  CourantNb    0.00000E+00   0.39427E+01          0          0 
v  FourierNb    0.54075E-04   0.19061E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.83953E-09   0.26921E-04         31          0 
a  omega       -0.11763E+03   0.89649E+03         30          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.39427E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.19061E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.42611E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               25:        0.18340E+00

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


 INSTANT    0.780000000E+01   TIME STEP NUMBER              26
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.407846364E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374973E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63988E-01 0.16918E-01
   Friction velocity        uet   :  0.50301E-06 0.14095E-01
   Friction velocity        uk    :  0.00000E+00 0.91932E-02
   Dimensionless distance   yplus :  0.14143E-03 0.12585E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        396
   Nb of faces within the viscous sub-layer     :       1320
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.57540E-02      42   0.11139E-01   0.55618E-01 
c  VelocityX    0.68466E+03       2   0.53148E-03   0.11645E-08 
c  VelocityY    0.68466E+03       2   0.53148E-03   0.33020E-10 
c  VelocityZ    0.68466E+03       2   0.53148E-03   0.18540E-34 
c  TurbEner     0.20521E-01       2   0.22314E-03   0.42136E-17 
c  omega        0.39226E+02      13   0.20968E-01   0.23038E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.77650E-02   0.83784E-02         --         -- 
v  VelocityX   -0.43230E-01   0.89341E-01         --         -- 
v  VelocityY   -0.73129E-01   0.59726E-01         --         -- 
v  VelocityZ   -0.50502E-14   0.39014E-14         --         -- 
v  TurbEner     0.54179E-18   0.27530E-04         26          0 
v  omega        0.29969E-03   0.89620E+03         28          0 
v  TurbVisc     0.18374E-20   0.60416E-02          0          0 
v  CourantNb    0.00000E+00   0.39068E+01          0          0 
v  FourierNb    0.54075E-04   0.20953E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.27901E-10   0.28003E-04         26          0 
a  omega       -0.12197E+03   0.89610E+03         28          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.39068E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.20953E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.42252E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               26:        0.18046E+00

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


 INSTANT    0.810000000E+01   TIME STEP NUMBER              27
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.281539193E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374966E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63753E-01 0.16965E-01
   Friction velocity        uet   :  0.38597E-06 0.13985E-01
   Friction velocity        uk    :  0.00000E+00 0.91478E-02
   Dimensionless distance   yplus :  0.61395E-04 0.12568E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        391
   Nb of faces within the viscous sub-layer     :       1323
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.53731E-02      42   0.10911E-01   0.54477E-01 
c  VelocityX    0.68468E+03       2   0.50097E-03   0.10379E-08 
c  VelocityY    0.68468E+03       2   0.50097E-03   0.32494E-10 
c  VelocityZ    0.68468E+03       2   0.50097E-03   0.18178E-34 
c  TurbEner     0.20520E-01       2   0.22293E-03   0.41895E-17 
c  omega        0.39219E+02      13   0.20626E-01   0.15846E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.74200E-02   0.78813E-02         --         -- 
v  VelocityX   -0.44754E-01   0.89080E-01         --         -- 
v  VelocityY   -0.72547E-01   0.59312E-01         --         -- 
v  VelocityZ   -0.50119E-14   0.38698E-14         --         -- 
v  TurbEner     0.23845E-18   0.28564E-04         24          0 
v  omega        0.29993E-03   0.89635E+03         25          0 
v  TurbVisc     0.76083E-21   0.60399E-02          0          0 
v  CourantNb    0.00000E+00   0.39230E+01          0          0 
v  FourierNb    0.54075E-04   0.21949E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.92712E-11   0.29007E-04         24          0 
a  omega       -0.11764E+03   0.89641E+03         25          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.39230E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.21949E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.42414E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               27:        0.18056E+00

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


 INSTANT    0.840000000E+01   TIME STEP NUMBER              28
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.323063660E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374961E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63259E-01 0.16927E-01
   Friction velocity        uet   :  0.43297E-06 0.14066E-01
   Friction velocity        uk    :  0.00000E+00 0.91725E-02
   Dimensionless distance   yplus :  0.12174E-03 0.12533E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        386
   Nb of faces within the viscous sub-layer     :       1327
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.50328E-02      42   0.10710E-01   0.53481E-01 
c  VelocityX    0.68470E+03       2   0.47292E-03   0.92865E-09 
c  VelocityY    0.68470E+03       2   0.47292E-03   0.31733E-10 
c  VelocityZ    0.68470E+03       2   0.47292E-03   0.17867E-34 
c  TurbEner     0.20520E-01       2   0.22270E-03   0.41121E-17 
c  omega        0.39220E+02      13   0.24092E-01   0.66358E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.70927E-02   0.74236E-02         --         -- 
v  VelocityX   -0.46199E-01   0.88826E-01         --         -- 
v  VelocityY   -0.73051E-01   0.59378E-01         --         -- 
v  VelocityZ   -0.49742E-14   0.38385E-14         --         -- 
v  TurbEner     0.11103E-18   0.29549E-04         27          0 
v  omega        0.30017E-03   0.89638E+03         24          0 
v  TurbVisc     0.33486E-21   0.60391E-02          0          0 
v  CourantNb    0.00000E+00   0.38904E+01          0          0 
v  FourierNb    0.54075E-04   0.22352E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.30940E-10   0.29971E-04         27          0 
a  omega       -0.12157E+03   0.89639E+03         24          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.28666E+02  0.10859E+01  0.50000E+00  
Courant max  0.38904E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22352E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.42088E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               28:        0.18259E+00

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


 INSTANT    0.870000000E+01   TIME STEP NUMBER              29
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.843168359E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374960E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62844E-01 0.16916E-01
   Friction velocity        uet   :  0.24745E-06 0.13946E-01
   Friction velocity        uk    :  0.00000E+00 0.91217E-02
   Dimensionless distance   yplus :  0.69575E-04 0.12504E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        382
   Nb of faces within the viscous sub-layer     :       1327
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.47192E-02      42   0.10517E-01   0.52521E-01 
c  VelocityX    0.68472E+03       2   0.44704E-03   0.83239E-09 
c  VelocityY    0.68472E+03       2   0.44704E-03   0.30886E-10 
c  VelocityZ    0.68472E+03       2   0.44704E-03   0.17504E-34 
c  TurbEner     0.20519E-01       2   0.22249E-03   0.42066E-17 
c  omega        0.39217E+02      13   0.20581E-01   0.17111E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.67841E-02   0.71194E-02         --         -- 
v  VelocityX   -0.46387E-01   0.88585E-01         --         -- 
v  VelocityY   -0.72036E-01   0.58943E-01         --         -- 
v  VelocityZ   -0.49368E-14   0.38074E-14         --         -- 
v  TurbEner     0.54193E-19   0.30462E-04         26          0 
v  omega        0.30042E-03   0.89617E+03         22          0 
v  TurbVisc     0.15592E-21   0.60382E-02          0          0 
v  CourantNb    0.00000E+00   0.38981E+01          0          0 
v  FourierNb    0.54075E-04   0.27789E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.14893E-10   0.30854E-04         26          0 
a  omega       -0.11740E+03   0.89608E+03         22          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.38981E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.27789E+01 -0.25942E+02 -0.45976E+00  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.42165E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               29:        0.18239E+00

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


 INSTANT    0.900000000E+01   TIME STEP NUMBER              30
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.729507126E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374964E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62520E-01 0.16940E-01
   Friction velocity        uet   :  0.27338E-06 0.14032E-01
   Friction velocity        uk    :  0.00000E+00 0.91438E-02
   Dimensionless distance   yplus :  0.43486E-04 0.12481E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        378
   Nb of faces within the viscous sub-layer     :       1331
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.44317E-02      42   0.10338E-01   0.51617E-01 
c  VelocityX    0.68473E+03       2   0.42319E-03   0.74821E-09 
c  VelocityY    0.68473E+03       2   0.42319E-03   0.30318E-10 
c  VelocityZ    0.68473E+03       2   0.42319E-03   0.17229E-34 
c  TurbEner     0.20519E-01       2   0.22225E-03   0.40550E-17 
c  omega        0.39213E+02      13   0.20504E-01   0.29955E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.64923E-02   0.68577E-02         --         -- 
v  VelocityX   -0.46329E-01   0.88341E-01         --         -- 
v  VelocityY   -0.71461E-01   0.59188E-01         --         -- 
v  VelocityZ   -0.48997E-14   0.37765E-14         --         -- 
v  TurbEner     0.27429E-19   0.31353E-04         19          0 
v  omega        0.30068E-03   0.89629E+03         20          0 
v  TurbVisc     0.76103E-22   0.60372E-02          0          0 
v  CourantNb    0.00000E+00   0.38662E+01          0          0 
v  FourierNb    0.54075E-04   0.27178E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.21632E-11   0.31734E-04         19          0 
a  omega       -0.12140E+03   0.89635E+03         20          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.38662E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.27178E+01 -0.25942E+02 -0.45976E+00  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.41846E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               30:        0.18086E+00

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


 INSTANT    0.930000000E+01   TIME STEP NUMBER              31
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.210778855E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374970E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62253E-01 0.16959E-01
   Friction velocity        uet   :  0.21998E-06 0.13914E-01
   Friction velocity        uk    :  0.00000E+00 0.90965E-02
   Dimensionless distance   yplus :  0.61850E-04 0.12462E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        375
   Nb of faces within the viscous sub-layer     :       1334
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.41685E-02      42   0.10169E-01   0.50778E-01 
c  VelocityX    0.68475E+03       2   0.40111E-03   0.67460E-09 
c  VelocityY    0.68475E+03       2   0.40111E-03   0.29474E-10 
c  VelocityZ    0.68475E+03       2   0.40111E-03   0.16875E-34 
c  TurbEner     0.20518E-01       2   0.22203E-03   0.41525E-17 
c  omega        0.39213E+02      13   0.22304E-01   0.37278E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.62213E-02   0.66054E-02         --         -- 
v  VelocityX   -0.46070E-01   0.88118E-01         --         -- 
v  VelocityY   -0.72432E-01   0.58660E-01         --         -- 
v  VelocityZ   -0.48628E-14   0.37459E-14         --         -- 
v  TurbEner     0.14260E-19   0.32169E-04         22          0 
v  omega        0.30094E-03   0.89628E+03         20          0 
v  TurbVisc     0.38519E-22   0.60361E-02          0          0 
v  CourantNb    0.00000E+00   0.38777E+01          0          0 
v  FourierNb    0.54075E-04   0.25770E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.15139E-10   0.32518E-04         22          0 
a  omega       -0.11707E+03   0.89628E+03         20          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.38777E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.25770E+01 -0.25942E+02 -0.45976E+00  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.41961E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               31:        0.18226E+00

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


 INSTANT    0.960000000E+01   TIME STEP NUMBER              32
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.275418057E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374976E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62002E-01 0.16975E-01
   Friction velocity        uet   :  0.39787E-06 0.14001E-01
   Friction velocity        uk    :  0.00000E+00 0.91219E-02
   Dimensionless distance   yplus :  0.11187E-03 0.12444E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        371
   Nb of faces within the viscous sub-layer     :       1336
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.39245E-02      44   0.10004E-01   0.49964E-01 
c  VelocityX    0.68476E+03       2   0.38070E-03   0.60966E-09 
c  VelocityY    0.68476E+03       2   0.38070E-03   0.28705E-10 
c  VelocityZ    0.68476E+03       2   0.38070E-03   0.16583E-34 
c  TurbEner     0.20517E-01       2   0.22181E-03   0.41086E-17 
c  omega        0.39215E+02      13   0.20067E-01   0.27208E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.61719E-02   0.63606E-02         --         -- 
v  VelocityX   -0.45679E-01   0.87893E-01         --         -- 
v  VelocityY   -0.71008E-01   0.58889E-01         --         -- 
v  VelocityZ   -0.48262E-14   0.37156E-14         --         -- 
v  TurbEner     0.75591E-20   0.32950E-04         17          0 
v  omega        0.30121E-03   0.89631E+03         20          0 
v  TurbVisc     0.20025E-22   0.60350E-02          0          0 
v  CourantNb    0.00000E+00   0.38450E+01          0          0 
v  FourierNb    0.54075E-04   0.22323E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.76548E-10   0.33285E-04         17          0 
a  omega       -0.12130E+03   0.89632E+03         20          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.38450E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.54075E-04  0.49652E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22323E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.41634E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               32:        0.19847E+00

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


 INSTANT    0.990000000E+01   TIME STEP NUMBER              33
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.875150471E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374982E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61838E-01 0.16987E-01
   Friction velocity        uet   :  0.65134E-06 0.13891E-01
   Friction velocity        uk    :  0.00000E+00 0.90768E-02
   Dimensionless distance   yplus :  0.10361E-03 0.12432E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        364
   Nb of faces within the viscous sub-layer     :       1336
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.37004E-02      43   0.98539E-02   0.49208E-01 
c  VelocityX    0.68478E+03       2   0.36175E-03   0.55191E-09 
c  VelocityY    0.68478E+03       2   0.36175E-03   0.27746E-10 
c  VelocityZ    0.68478E+03       2   0.36175E-03   0.16272E-34 
c  TurbEner     0.20517E-01       2   0.22158E-03   0.41491E-17 
c  omega        0.39210E+02      13   0.19157E-01   0.10078E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.61281E-02   0.61288E-02         --         -- 
v  VelocityX   -0.45115E-01   0.87675E-01         --         -- 
v  VelocityY   -0.70358E-01   0.58597E-01         --         -- 
v  VelocityZ   -0.47903E-14   0.36855E-14         --         -- 
v  TurbEner     0.40661E-20   0.33684E-04         18          0 
v  omega        0.30149E-03   0.89616E+03         18          0 
v  TurbVisc     0.10615E-22   0.60338E-02          0          0 
v  CourantNb    0.00000E+00   0.38588E+01          0          0 
v  FourierNb    0.53812E-04   0.22347E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.76913E-09   0.33998E-04         18          0 
a  omega       -0.11701E+03   0.89610E+03         18          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.38588E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.53812E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22347E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.41772E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               33:        0.21215E+00

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


 INSTANT    0.102000000E+02   TIME STEP NUMBER              34
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.823448374E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374990E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61411E-01 0.16994E-01
   Friction velocity        uet   :  0.28338E-06 0.13965E-01
   Friction velocity        uk    :  0.00000E+00 0.91015E-02
   Dimensionless distance   yplus :  0.45077E-04 0.12401E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        359
   Nb of faces within the viscous sub-layer     :       1340
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.34939E-02      43   0.97128E-02   0.48501E-01 
c  VelocityX    0.68479E+03       2   0.34413E-03   0.50110E-09 
c  VelocityY    0.68479E+03       2   0.34413E-03   0.26922E-10 
c  VelocityZ    0.68479E+03       2   0.34413E-03   0.15988E-34 
c  TurbEner     0.20516E-01       2   0.22135E-03   0.40176E-17 
c  omega        0.39211E+02      13   0.20712E-01   0.39509E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.61377E-02   0.59058E-02         --         -- 
v  VelocityX   -0.44370E-01   0.87455E-01         --         -- 
v  VelocityY   -0.71115E-01   0.58590E-01         --         -- 
v  VelocityZ   -0.47544E-14   0.36557E-14         --         -- 
v  TurbEner     0.22423E-20   0.34388E-04         16          0 
v  omega        0.30178E-03   0.89620E+03         19          0 
v  TurbVisc     0.57100E-23   0.60326E-02          0          0 
v  CourantNb    0.00000E+00   0.38254E+01          0          0 
v  FourierNb    0.53345E-04   0.22362E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.53265E-09   0.34690E-04         16          0 
a  omega       -0.12084E+03   0.89622E+03         19          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25896E+02  0.11575E+01  0.50000E+00  
Courant max  0.38254E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.53345E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22362E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.41438E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               34:        0.20894E+00

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


 INSTANT    0.105000000E+02   TIME STEP NUMBER              35
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.817148566E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214374997E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61053E-01 0.16997E-01
   Friction velocity        uet   :  0.23521E-06 0.13858E-01
   Friction velocity        uk    :  0.00000E+00 0.90538E-02
   Dimensionless distance   yplus :  0.63820E-04 0.12376E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        355
   Nb of faces within the viscous sub-layer     :       1342
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.32999E-02      43   0.95666E-02   0.47789E-01 
c  VelocityX    0.68480E+03       2   0.32776E-03   0.45577E-09 
c  VelocityY    0.68480E+03       2   0.32776E-03   0.26057E-10 
c  VelocityZ    0.68480E+03       2   0.32776E-03   0.15696E-34 
c  TurbEner     0.20516E-01       2   0.22113E-03   0.41839E-17 
c  omega        0.39213E+02      13   0.21812E-01   0.35577E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.61105E-02   0.56898E-02         --         -- 
v  VelocityX   -0.43416E-01   0.87240E-01         --         -- 
v  VelocityY   -0.69653E-01   0.58277E-01         --         -- 
v  VelocityZ   -0.47188E-14   0.36261E-14         --         -- 
v  TurbEner     0.12732E-20   0.35032E-04         16          0 
v  omega        0.30194E-03   0.89624E+03         17          0 
v  TurbVisc     0.31489E-23   0.60313E-02          0          0 
v  CourantNb    0.00000E+00   0.38368E+01          0          0 
v  FourierNb    0.52888E-04   0.22399E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.40969E-11   0.35309E-04         16          0 
a  omega       -0.11694E+03   0.89626E+03         17          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.38368E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.52888E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22399E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.41552E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               35:        0.19617E+00

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


 INSTANT    0.108000000E+02   TIME STEP NUMBER              36
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.171537407E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375006E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60779E-01 0.16998E-01
   Friction velocity        uet   :  0.52290E-06 0.13940E-01
   Friction velocity        uk    :  0.00000E+00 0.90780E-02
   Dimensionless distance   yplus :  0.10518E-03 0.12356E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        353
   Nb of faces within the viscous sub-layer     :       1342
   Total number of wall faces                   :       2254
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         36, Physical time    0.10800E+02


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

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

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

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


 Time for restart files:    0.98951E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.31197E-02      43   0.94312E-02   0.47103E-01 
c  VelocityX    0.68481E+03       2   0.31252E-03   0.41629E-09 
c  VelocityY    0.68481E+03       2   0.31252E-03   0.25017E-10 
c  VelocityZ    0.68481E+03       2   0.31252E-03   0.15380E-34 
c  TurbEner     0.20515E-01       2   0.22090E-03   0.41167E-17 
c  omega        0.39216E+02      13   0.19510E-01   0.25850E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.61173E-02   0.54818E-02         --         -- 
v  VelocityX   -0.42622E-01   0.87021E-01         --         -- 
v  VelocityY   -0.70158E-01   0.58344E-01         --         -- 
v  VelocityZ   -0.46835E-14   0.35967E-14         --         -- 
v  TurbEner     0.73511E-21   0.35668E-04         13          0 
v  omega        0.30206E-03   0.89626E+03         18          0 
v  TurbVisc     0.17880E-23   0.60300E-02          0          0 
v  CourantNb    0.00000E+00   0.38054E+01          0          0 
v  FourierNb    0.52439E-04   0.22423E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.24579E-11   0.35940E-04         13          0 
a  omega       -0.12075E+03   0.89627E+03         18          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.38054E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.52439E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22423E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.41238E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               36:        0.28305E+00

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


 INSTANT    0.111000000E+02   TIME STEP NUMBER              37
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.773195497E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375014E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60522E-01 0.16995E-01
   Friction velocity        uet   :  0.43149E-06 0.13828E-01
   Friction velocity        uk    :  0.00000E+00 0.90342E-02
   Dimensionless distance   yplus :  0.12132E-03 0.12337E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        348
   Nb of faces within the viscous sub-layer     :       1344
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.29511E-02      43   0.92947E-02   0.46431E-01 
c  VelocityX    0.68482E+03       2   0.29831E-03   0.38019E-09 
c  VelocityY    0.68482E+03       2   0.29831E-03   0.23985E-10 
c  VelocityZ    0.68482E+03       2   0.29831E-03   0.15126E-34 
c  TurbEner     0.20514E-01       2   0.22067E-03   0.42139E-17 
c  omega        0.39215E+02      13   0.19031E-01   0.15293E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.60757E-02   0.52813E-02         --         -- 
v  VelocityX   -0.42113E-01   0.86812E-01         --         -- 
v  VelocityY   -0.68838E-01   0.58019E-01         --         -- 
v  VelocityZ   -0.46486E-14   0.35676E-14         --         -- 
v  TurbEner     0.42896E-21   0.36244E-04         13          0 
v  omega        0.30218E-03   0.89628E+03         17          0 
v  TurbVisc     0.10323E-23   0.60288E-02          0          0 
v  CourantNb    0.00000E+00   0.38181E+01          0          0 
v  FourierNb    0.51998E-04   0.22495E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.35620E-11   0.36492E-04         13          0 
a  omega       -0.11657E+03   0.89628E+03         17          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.38181E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.51998E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22495E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.41365E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               37:        0.19845E+00

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


 INSTANT    0.114000000E+02   TIME STEP NUMBER              38
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.127743156E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375022E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60272E-01 0.16990E-01
   Friction velocity        uet   :  0.59684E-06 0.13901E-01
   Friction velocity        uk    :  0.00000E+00 0.90573E-02
   Dimensionless distance   yplus :  0.11107E-03 0.12319E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        344
   Nb of faces within the viscous sub-layer     :       1345
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.27986E-02      55   0.91787E-02   0.45856E-01 
c  VelocityX    0.68483E+03       2   0.28505E-03   0.34794E-09 
c  VelocityY    0.68483E+03       2   0.28505E-03   0.23112E-10 
c  VelocityZ    0.68483E+03       2   0.28505E-03   0.14889E-34 
c  TurbEner     0.20514E-01       2   0.22044E-03   0.41742E-17 
c  omega        0.39220E+02      13   0.22186E-01   0.50602E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.61012E-02   0.50854E-02         --         -- 
v  VelocityX   -0.41550E-01   0.86602E-01         --         -- 
v  VelocityY   -0.68982E-01   0.58087E-01         --         -- 
v  VelocityZ   -0.46138E-14   0.35387E-14         --         -- 
v  TurbEner     0.25251E-21   0.36799E-04         10          0 
v  omega        0.30230E-03   0.89615E+03         17          0 
v  TurbVisc     0.60239E-24   0.60275E-02          0          0 
v  CourantNb    0.00000E+00   0.37825E+01          0          0 
v  FourierNb    0.51565E-04   0.22619E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.29433E-11   0.37037E-04         10          0 
a  omega       -0.12053E+03   0.89610E+03         17          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.37825E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.51565E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22619E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.41009E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               38:        0.18347E+00

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


 INSTANT    0.117000000E+02   TIME STEP NUMBER              39
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.878240817E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375026E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60104E-01 0.16981E-01
   Friction velocity        uet   :  0.12032E-05 0.13805E-01
   Friction velocity        uk    :  0.00000E+00 0.90151E-02
   Dimensionless distance   yplus :  0.26905E-03 0.12307E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        341
   Nb of faces within the viscous sub-layer     :       1349
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26529E-02      42   0.90550E-02   0.45248E-01 
c  VelocityX    0.68484E+03       2   0.27267E-03   0.31935E-09 
c  VelocityY    0.68484E+03       2   0.27267E-03   0.22196E-10 
c  VelocityZ    0.68484E+03       2   0.27267E-03   0.14578E-34 
c  TurbEner     0.20513E-01       2   0.22022E-03   0.43439E-17 
c  omega        0.39224E+02      13   0.19611E-01   0.28100E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.60598E-02   0.48999E-02         --         -- 
v  VelocityX   -0.41069E-01   0.86397E-01         --         -- 
v  VelocityY   -0.67652E-01   0.57960E-01         --         -- 
v  VelocityZ   -0.45793E-14   0.35100E-14         --         -- 
v  TurbEner     0.14726E-21   0.37317E-04         14          0 
v  omega        0.30241E-03   0.89618E+03         19          0 
v  TurbVisc     0.35460E-24   0.60262E-02          0          0 
v  CourantNb    0.00000E+00   0.37998E+01          0          0 
v  FourierNb    0.51140E-04   0.22780E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.24043E-11   0.37539E-04         14          0 
a  omega       -0.11651E+03   0.89619E+03         19          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.28160E+02  0.10987E+01  0.50000E+00  
Courant max  0.37998E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.51140E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22780E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.41182E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               39:        0.18134E+00

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


 INSTANT    0.120000000E+02   TIME STEP NUMBER              40
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.567882652E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375030E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59684E-01 0.16970E-01
   Friction velocity        uet   :  0.81654E-06 0.13871E-01
   Friction velocity        uk    :  0.00000E+00 0.90395E-02
   Dimensionless distance   yplus :  0.19047E-03 0.12276E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        338
   Nb of faces within the viscous sub-layer     :       1354
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25169E-02      56   0.89386E-02   0.44659E-01 
c  VelocityX    0.68485E+03       2   0.26109E-03   0.29353E-09 
c  VelocityY    0.68485E+03       2   0.26109E-03   0.21215E-10 
c  VelocityZ    0.68485E+03       2   0.26109E-03   0.14334E-34 
c  TurbEner     0.20513E-01       2   0.21999E-03   0.44288E-17 
c  omega        0.39228E+02      13   0.21091E-01   0.54437E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.60759E-02   0.47198E-02         --         -- 
v  VelocityX   -0.40575E-01   0.86199E-01         --         -- 
v  VelocityY   -0.68090E-01   0.57791E-01         --         -- 
v  VelocityZ   -0.45452E-14   0.34816E-14         --         -- 
v  TurbEner     0.85737E-22   0.37822E-04          6          0 
v  omega        0.30254E-03   0.89613E+03         21          0 
v  TurbVisc     0.20679E-24   0.60250E-02          0          0 
v  CourantNb    0.00000E+00   0.37648E+01          0          0 
v  FourierNb    0.50723E-04   0.22159E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.11695E-11   0.38039E-04          6          0 
a  omega       -0.12009E+03   0.89612E+03         21          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.28160E+02  0.10987E+01  0.50000E+00  
Courant max  0.37648E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.50723E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22159E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.40832E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               40:        0.18802E+00

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


 INSTANT    0.123000000E+02   TIME STEP NUMBER              41
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.133111228E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375025E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59330E-01 0.16962E-01
   Friction velocity        uet   :  0.18006E-05 0.13767E-01
   Friction velocity        uk    :  0.00000E+00 0.89973E-02
   Dimensionless distance   yplus :  0.36130E-03 0.12250E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        334
   Nb of faces within the viscous sub-layer     :       1359
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23887E-02      43   0.88206E-02   0.44072E-01 
c  VelocityX    0.68486E+03       2   0.25026E-03   0.27051E-09 
c  VelocityY    0.68486E+03       2   0.25026E-03   0.20463E-10 
c  VelocityZ    0.68486E+03       2   0.25026E-03   0.14091E-34 
c  TurbEner     0.20512E-01       2   0.21978E-03   0.49445E-17 
c  omega        0.39235E+02      13   0.23554E-01   0.75711E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.60487E-02   0.45502E-02         --         -- 
v  VelocityX   -0.39862E-01   0.86013E-01         --         -- 
v  VelocityY   -0.66560E-01   0.57647E-01         --         -- 
v  VelocityZ   -0.45112E-14   0.34534E-14         --         -- 
v  TurbEner     0.50275E-22   0.38272E-04         13          0 
v  omega        0.30259E-03   0.89604E+03         21          0 
v  TurbVisc     0.12040E-24   0.60238E-02          0          0 
v  CourantNb    0.00000E+00   0.37743E+01          0          0 
v  FourierNb    0.50314E-04   0.22614E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.19445E-11   0.38464E-04         13          0 
a  omega       -0.11615E+03   0.89600E+03         21          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.37743E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.50314E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22614E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.40927E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               41:        0.18519E+00

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


 INSTANT    0.126000000E+02   TIME STEP NUMBER              42
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.560074067E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375022E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59042E-01 0.16965E-01
   Friction velocity        uet   :  0.43378E-06 0.13844E-01
   Friction velocity        uk    :  0.00000E+00 0.90246E-02
   Dimensionless distance   yplus :  0.12196E-03 0.12229E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        331
   Nb of faces within the viscous sub-layer     :       1361
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.22687E-02      56   0.87100E-02   0.43498E-01 
c  VelocityX    0.68487E+03       2   0.24012E-03   0.24970E-09 
c  VelocityY    0.68487E+03       2   0.24012E-03   0.19529E-10 
c  VelocityZ    0.68487E+03       2   0.24012E-03   0.13854E-34 
c  TurbEner     0.20512E-01       2   0.21957E-03   0.50761E-17 
c  omega        0.39242E+02      12   0.18891E-01   0.18971E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.60585E-02   0.43865E-02         --         -- 
v  VelocityX   -0.38873E-01   0.85824E-01         --         -- 
v  VelocityY   -0.67073E-01   0.57539E-01         --         -- 
v  VelocityZ   -0.44774E-14   0.34262E-14         --         -- 
v  TurbEner     0.29887E-22   0.38728E-04         12          0 
v  omega        0.30265E-03   0.89593E+03         22          0 
v  TurbVisc     0.70601E-25   0.60226E-02          0          0 
v  CourantNb    0.00000E+00   0.37378E+01          0          0 
v  FourierNb    0.49911E-04   0.22397E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.12144E-11   0.38924E-04         12          0 
a  omega       -0.12008E+03   0.89588E+03         22          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.37378E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.49911E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22397E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.40562E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               42:        0.19218E+00

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


 INSTANT    0.129000000E+02   TIME STEP NUMBER              43
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.469917997E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375019E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58786E-01 0.16955E-01
   Friction velocity        uet   :  0.20247E-06 0.13752E-01
   Friction velocity        uk    :  0.00000E+00 0.89830E-02
   Dimensionless distance   yplus :  0.50672E-04 0.12211E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        325
   Nb of faces within the viscous sub-layer     :       1363
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.21588E-02      56   0.86046E-02   0.42994E-01 
c  VelocityX    0.68488E+03       2   0.23061E-03   0.23097E-09 
c  VelocityY    0.68488E+03       2   0.23061E-03   0.18842E-10 
c  VelocityZ    0.68488E+03       2   0.23061E-03   0.13588E-34 
c  TurbEner     0.20511E-01       2   0.21933E-03   0.49754E-17 
c  omega        0.39246E+02      13   0.21617E-01   0.42090E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.60233E-02   0.42294E-02         --         -- 
v  VelocityX   -0.37761E-01   0.85629E-01         --         -- 
v  VelocityY   -0.65596E-01   0.57388E-01         --         -- 
v  VelocityZ   -0.44443E-14   0.34001E-14         --         -- 
v  TurbEner     0.18113E-22   0.39135E-04          7          0 
v  omega        0.30271E-03   0.89571E+03         22          0 
v  TurbVisc     0.41970E-25   0.60214E-02          0          0 
v  CourantNb    0.00000E+00   0.37598E+01          0          0 
v  FourierNb    0.49516E-04   0.22190E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.11984E-11   0.39310E-04          7          0 
a  omega       -0.11610E+03   0.89562E+03         22          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.37598E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.49516E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22190E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.40782E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               43:        0.20390E+00

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


 INSTANT    0.132000000E+02   TIME STEP NUMBER              44
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.253368730E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375018E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58547E-01 0.16917E-01
   Friction velocity        uet   :  0.42953E-06 0.13819E-01
   Friction velocity        uk    :  0.00000E+00 0.90093E-02
   Dimensionless distance   yplus :  0.17756E-03 0.12193E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        321
   Nb of faces within the viscous sub-layer     :       1364
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.20569E-02      57   0.85098E-02   0.42528E-01 
c  VelocityX    0.68488E+03       2   0.22169E-03   0.21417E-09 
c  VelocityY    0.68488E+03       2   0.22169E-03   0.18085E-10 
c  VelocityZ    0.68488E+03       2   0.22169E-03   0.13352E-34 
c  TurbEner     0.20510E-01       2   0.21910E-03   0.47814E-17 
c  omega        0.39245E+02      12   0.20841E-01   0.15637E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.60500E-02   0.40780E-02         --         -- 
v  VelocityX   -0.37132E-01   0.85431E-01         --         -- 
v  VelocityY   -0.66223E-01   0.57452E-01         --         -- 
v  VelocityZ   -0.44110E-14   0.33742E-14         --         -- 
v  TurbEner     0.11247E-22   0.39535E-04          8          0 
v  omega        0.30279E-03   0.89552E+03         22          0 
v  TurbVisc     0.25436E-25   0.60202E-02          0          0 
v  CourantNb    0.00000E+00   0.37268E+01          0          0 
v  FourierNb    0.49128E-04   0.22035E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.95586E-12   0.39706E-04          8          0 
a  omega       -0.11966E+03   0.89543E+03         22          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.28160E+02  0.10987E+01  0.50000E+00  
Courant max  0.37268E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.49128E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22035E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.40452E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               44:        0.18848E+00

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


 INSTANT    0.135000000E+02   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.232709067E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375018E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58384E-01 0.16882E-01
   Friction velocity        uet   :  0.88227E-06 0.13712E-01
   Friction velocity        uk    :  0.00000E+00 0.89702E-02
   Dimensionless distance   yplus :  0.21425E-03 0.12181E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        317
   Nb of faces within the viscous sub-layer     :       1365
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.19562E-02      57   0.84028E-02   0.41971E-01 
c  VelocityX    0.68489E+03       2   0.21331E-03   0.19880E-09 
c  VelocityY    0.68489E+03       2   0.21331E-03   0.17303E-10 
c  VelocityZ    0.68489E+03       2   0.21331E-03   0.13139E-34 
c  TurbEner     0.20510E-01       2   0.21883E-03   0.43201E-17 
c  omega        0.39246E+02      12   0.21326E-01   0.37745E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.60110E-02   0.39328E-02         --         -- 
v  VelocityX   -0.36488E-01   0.85227E-01         --         -- 
v  VelocityY   -0.64793E-01   0.57320E-01         --         -- 
v  VelocityZ   -0.43780E-14   0.33486E-14         --         -- 
v  TurbEner     0.71890E-23   0.39906E-04         12          0 
v  omega        0.30286E-03   0.89531E+03         22          0 
v  TurbVisc     0.15794E-25   0.60191E-02          0          0 
v  CourantNb    0.00000E+00   0.37377E+01          0          0 
v  FourierNb    0.48746E-04   0.21986E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.27024E-08   0.40065E-04         12          0 
a  omega       -0.11567E+03   0.89522E+03         22          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.28160E+02  0.10987E+01  0.50000E+00  
Courant max  0.37377E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.48746E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.21986E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.40561E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               45:        0.18814E+00

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


 INSTANT    0.138000000E+02   TIME STEP NUMBER              46
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.144637659E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375019E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57974E-01 0.16861E-01
   Friction velocity        uet   :  0.25099E-06 0.13790E-01
   Friction velocity        uk    :  0.00000E+00 0.89968E-02
   Dimensionless distance   yplus :  0.70570E-04 0.12151E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        312
   Nb of faces within the viscous sub-layer     :       1370
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.18645E-02      56   0.83068E-02   0.41488E-01 
c  VelocityX    0.68490E+03       2   0.20544E-03   0.18518E-09 
c  VelocityY    0.68490E+03       2   0.20544E-03   0.16539E-10 
c  VelocityZ    0.68490E+03       2   0.20544E-03   0.12917E-34 
c  TurbEner     0.20509E-01       2   0.21862E-03   0.43489E-17 
c  omega        0.39252E+02      12   0.19100E-01   0.21209E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.60270E-02   0.37928E-02         --         -- 
v  VelocityX   -0.35773E-01   0.85025E-01         --         -- 
v  VelocityY   -0.65452E-01   0.57176E-01         --         -- 
v  VelocityZ   -0.43452E-14   0.33231E-14         --         -- 
v  TurbEner     0.47485E-23   0.40269E-04          9          0 
v  omega        0.30295E-03   0.89508E+03         22          0 
v  TurbVisc     0.10095E-25   0.60184E-02          0          0 
v  CourantNb    0.00000E+00   0.37013E+01          0          0 
v  FourierNb    0.48371E-04   0.22035E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.29886E-08   0.40425E-04          9          0 
a  omega       -0.11960E+03   0.89499E+03         22          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.28160E+02  0.10987E+01  0.50000E+00  
Courant max  0.37013E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.48371E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22035E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.40197E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               46:        0.18859E+00

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


 INSTANT    0.141000000E+02   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.631165277E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375020E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57634E-01 0.16840E-01
   Friction velocity        uet   :  0.37346E-06 0.13693E-01
   Friction velocity        uk    :  0.00000E+00 0.89542E-02
   Dimensionless distance   yplus :  0.15072E-03 0.12125E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        309
   Nb of faces within the viscous sub-layer     :       1372
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.17794E-02      57   0.82171E-02   0.41047E-01 
c  VelocityX    0.68490E+03       2   0.19805E-03   0.17274E-09 
c  VelocityY    0.68490E+03       2   0.19805E-03   0.15811E-10 
c  VelocityZ    0.68490E+03       2   0.19805E-03   0.12695E-34 
c  TurbEner     0.20509E-01       2   0.21837E-03   0.43118E-17 
c  omega        0.39256E+02      12   0.21277E-01   0.38417E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.60049E-02   0.36582E-02         --         -- 
v  VelocityX   -0.36136E-01   0.84812E-01         --         -- 
v  VelocityY   -0.64113E-01   0.57013E-01         --         -- 
v  VelocityZ   -0.43127E-14   0.32977E-14         --         -- 
v  TurbEner     0.32502E-23   0.40586E-04          9          0 
v  omega        0.30303E-03   0.89486E+03         22          0 
v  TurbVisc     0.66683E-26   0.60177E-02          0          0 
v  CourantNb    0.00000E+00   0.37219E+01          0          0 
v  FourierNb    0.48002E-04   0.22099E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.50925E-08   0.40722E-04          9          0 
a  omega       -0.11555E+03   0.89476E+03         22          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25952E+02  0.10988E+01  0.50000E+00  
Courant max  0.37219E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.48002E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22099E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.40403E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               47:        0.20496E+00

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


 INSTANT    0.144000000E+02   TIME STEP NUMBER              48
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.576528343E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375019E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57361E-01 0.16817E-01
   Friction velocity        uet   :  0.57321E-06 0.13759E-01
   Friction velocity        uk    :  0.00000E+00 0.89814E-02
   Dimensionless distance   yplus :  0.16117E-03 0.12105E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        306
   Nb of faces within the viscous sub-layer     :       1371
   Total number of wall faces                   :       2254
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration         48, Physical time    0.14400E+02


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

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

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

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


 Time for restart files:    0.98830E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.17028E-02      57   0.81542E-02   0.40697E-01 
c  VelocityX    0.68491E+03       2   0.19110E-03   0.16133E-09 
c  VelocityY    0.68491E+03       2   0.19110E-03   0.15181E-10 
c  VelocityZ    0.68491E+03       2   0.19110E-03   0.12451E-34 
c  TurbEner     0.20508E-01       2   0.21816E-03   0.43924E-17 
c  omega        0.39263E+02      12   0.20542E-01   0.34500E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.60172E-02   0.35294E-02         --         -- 
v  VelocityX   -0.37018E-01   0.84602E-01         --         -- 
v  VelocityY   -0.64778E-01   0.56878E-01         --         -- 
v  VelocityZ   -0.42804E-14   0.32726E-14         --         -- 
v  TurbEner     0.23081E-23   0.40917E-04         11          0 
v  omega        0.30312E-03   0.89464E+03         23          0 
v  TurbVisc     0.45643E-26   0.60171E-02          0          0 
v  CourantNb    0.00000E+00   0.36865E+01          0          0 
v  FourierNb    0.47639E-04   0.22173E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.37151E-09   0.41059E-04         11          0 
a  omega       -0.11914E+03   0.89455E+03         23          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.36865E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.47639E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.22173E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.40049E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               48:        0.29670E+00

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


 INSTANT    0.147000000E+02   TIME STEP NUMBER              49
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254         0.478573615E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375017E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57079E-01 0.16815E-01
   Friction velocity        uet   :  0.64234E-07 0.13655E-01
   Friction velocity        uk    :  0.00000E+00 0.89414E-02
   Dimensionless distance   yplus :  0.24394E-04 0.12084E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        302
   Nb of faces within the viscous sub-layer     :       1374
   Total number of wall faces                   :       2254
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.16191E-02      58   0.80228E-02   0.40076E-01 
c  VelocityX    0.68491E+03       2   0.18455E-03   0.15089E-09 
c  VelocityY    0.68491E+03       2   0.18455E-03   0.14452E-10 
c  VelocityZ    0.68491E+03       2   0.18455E-03   0.12220E-34 
c  TurbEner     0.20508E-01       2   0.21791E-03   0.41860E-17 
c  omega        0.39270E+02      12   0.21693E-01   0.48323E-04 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.59833E-02   0.34061E-02         --         -- 
v  VelocityX   -0.37126E-01   0.84425E-01         --         -- 
v  VelocityY   -0.63558E-01   0.56749E-01         --         -- 
v  VelocityZ   -0.42485E-14   0.32478E-14         --         -- 
v  TurbEner     0.16993E-23   0.41201E-04         11          0 
v  omega        0.30322E-03   0.89440E+03         23          0 
v  TurbVisc     0.32413E-26   0.60164E-02          0          0 
v  CourantNb    0.00000E+00   0.36992E+01          0          0 
v  FourierNb    0.47282E-04   0.20539E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.44362E-08   0.41323E-04         11          0 
a  omega       -0.11519E+03   0.89429E+03         23          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00 -0.25871E+02  0.11575E+01  0.50000E+00  
Courant max  0.36992E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.47282E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.20539E+01 -0.15554E+00  0.40852E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.40177E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               49:        0.18994E+00

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


 INSTANT    0.150000000E+02   TIME STEP NUMBER              50
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          41        -0.214375000E+02
Smooth wall               5        2254        -0.203287907E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      149526         0.000000000E+00
Free outlet               3          41         0.214375015E+02
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56809E-01 0.16818E-01
   Friction velocity        uet   :  0.37864E-06 0.13734E-01
   Friction velocity        uk    :  0.00000E+00 0.89681E-02
   Dimensionless distance   yplus :  0.17643E-03 0.12064E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        299
   Nb of faces within the viscous sub-layer     :       1374
   Total number of wall faces                   :       2254
------------------------------------------------------------




 Write final restart files
   checkpoint at iteration         50, Physical time    0.15000E+02


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

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

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

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


 Time for restart files:    0.98725E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.15489E-02      58   0.79411E-02   0.39679E-01 
c  VelocityX    0.68492E+03       2   0.17839E-03   0.14153E-09 
c  VelocityY    0.68492E+03       2   0.17839E-03   0.13889E-10 
c  VelocityZ    0.68492E+03       2   0.17839E-03   0.12048E-34 
c  TurbEner     0.20507E-01       2   0.21770E-03   0.43392E-17 
c  omega        0.39275E+02      12   0.17826E-01   0.92090E-05 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.60095E-02   0.32882E-02         --         -- 
v  VelocityX   -0.37985E-01   0.84188E-01         --         -- 
v  VelocityY   -0.64215E-01   0.56808E-01         --         -- 
v  VelocityZ   -0.42167E-14   0.32230E-14         --         -- 
v  TurbEner     0.12940E-23   0.41483E-04         12          0 
v  omega        0.30332E-03   0.89409E+03         22          0 
v  TurbVisc     0.23863E-26   0.60158E-02          0          0 
v  CourantNb    0.00000E+00   0.36609E+01          0          0 
v  FourierNb    0.46931E-04   0.20143E+01          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.50905E-08   0.41604E-04         12          0 
a  omega       -0.11911E+03   0.89396E+03         22          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.25920E+02  0.11229E+01  0.50000E+00  
Courant max  0.36609E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
Fourier min  0.46931E-04 -0.24540E+03 -0.17105E+03  0.50000E+00  
Fourier max  0.20143E+01 -0.86666E-01  0.40912E+01  0.50000E+00  
Cou_Fou min  0.15801E-02  0.20525E+03 -0.17105E+03  0.50000E+00  
Cou_Fou max  0.39793E+01 -0.28861E+02  0.11032E+01  0.50000E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               50:        0.50019E+00

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.23000E-04
      -----------------------                                



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




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


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

 Destruction des structures et clôture du calcul

Time elapsed defining values using MEI:      0.00327


Bilan des temps de calcul :

  Temps CPU utilisateur :       12.360 s
  Temps CPU système :            0.220 s
  Temps CPU cumulé :           102.060 s

  Temps écoulé :                12.764 s
  Temps CPU / écoulé             0.986

Bilan de l'occupation mémoire :

  Consommation mémoire totale mesurée :             1.980 Gio
                             minimum local :      252.457 Mio  (rang 6)
                             maximum local :      257.293 Mio  (rang 0)
  Mémoire dynamique instrumentée théorique :      110.773 Mio
                             minimum local :       11.167 Mio  (rang 2)
                             maximum local :       30.167 Mio  (rang 0)
