command: 
 ./cs_solver --param Calc --mpi

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

                                  (R)
                      Code_Saturne

                      Version 3.2.1


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

  build Mi 08 Jan 2014 16:51:01 CET
  MPI version 2.2 (MPICH2 1.4.1)


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

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

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


Local case configuration:

  Date:                So 12 Jan 2014 14:31:14 CET
  System:              Linux 3.8.0-34-generic
  Machine:             caelinux-GA-78LMT-USB3
  Processor:           model name	: AMD FX(tm)-4300 Quad-Core Processor
  Memory:              3432 MB
  User:                caelinux (caelinux)
  Directory:           /home/caelinux/opt/code_saturne-3.2.1/arch/Linux_x86_64/bin/RPMFine/Case1/RESU/20140112-1431
  MPI ranks:           4 (appnum attribute: 0)
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

  External libraries for partitioning:
    ParMETIS 4.0.3

 Reading metadata from file: "mesh_input/mesh_01"
 Reading metadata from file: "mesh_input/mesh_02"

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

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


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




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


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

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

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


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

 --- 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          )


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


 ** 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    =    0.10350E+04 (Reference density           )
       VISCL0 =    0.35000E-02 (Ref. molecular dyn. visc.   )
       CP0    =    0.10172E+04 (Ref. specific heat          )
       ICP    =              0 (> 0: variable CP (usphyv)   )
       P0     =    0.10132E+06 (Ref. total pressure         )
       PRED0  =    0.00000E+00 (Ref. reduced pressure       )
       T0     =    0.29315E+03 (Ref. temperature            )

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

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

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


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

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


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

 --- Continuous phase:

   - Commons
       ITURB  =             60 (Turbulence model            )
       IDEUCH =              1 (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)     )

   - k-omega SST         (ITURB = 60)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       IKECOU =              0 (k-epsilon coupling mode     )
       IGRAKE =              1 (Account for gravity         )
       RELAXV =    0.10000E+01 for k      (Relaxation)
       RELAXV =    0.10000E+01 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:
       IVISSE =              1 (1: accounted for            )


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

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

       With a non-constant time step (IDTVAR = 1 or 2),
         when the value of COUMAX or FOUMAX is negative
         or zero, the associated time step limitation (for
         CFL and Fourier respectively) is ignored.

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

------------------------------------
 Variable          ISTAT      CDTVAR
------------------------------------
 Pressure              0  0.1000E+01
 VelocityX             1  0.1000E+01
 VelocityY             1  0.1000E+01
 VelocityZ             1  0.1000E+01
 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      1      0 0.10E+01 0.10E+01
 VelocityY             1      1      1      1      0 0.10E+01 0.10E+01
 VelocityZ             1      1      1      1      0 0.10E+01 0.10E+01
 TurbEner              1      1      1      1      0 0.00E+00 0.10E+01
 omega                 1      1      1      1      0 0.00E+00 0.10E+01
-------------------------------------------------------------

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


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


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

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

       RELAXV =    0.10000E+01 for pressure (relaxation)
       ARAK   =    0.10000E+01 (Arakawa factor              )

       ISTMPF =              1 (time scheme for flow
                               (0: explicit (THETFL = 0     )
                               (1: std scheme (Saturne 1.0  )
                               (2: 2nd-order (THETFL = 0.5  )
       THETFL =   -0.99900E+03 (theta for mass flow         )
       IROEXT =              0 (density extrapolation
                               (0: explicit
                               (1: n+thetro with thetro=1/2
                               (2: n+thetro with thetro=1
       THETRO =    0.00000E+00 (theta for density
                               ((1+theta).new-theta.old
       IVIEXT =              0 (total viscosity extrapolation
                               (0: explicit
                               (1: n+thetvi with thetro=1/2
                               (2: n+thetvi with thetro=1
       THETVI =    0.00000E+00 (theta for total viscosity
                               ((1+theta).new-theta.old
       ICPEXT =              0 (specific heat extrapolation
                               (0: explicit
                               (1: n+thetcp with thetro=1/2
                               (2: n+thetcp with thetro=1
       THETCP =    0.00000E+00 (specific heat theta-scheme
                               ((1+theta).new-theta.old
       THETSN =    0.00000E+00 (Nav-Stokes S.T. theta scheme)
                               ((1+theta).new-theta.old
       THETST =    0.00000E+00 (Turbulence S.T. theta-scheme)
                               ((1+theta).new-theta.old
       EPSUP  =    0.10000E-04 (Velocity/pressure coupling
                                stop test                   )


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


 ** GRADIENTS CALCULATION
    ---------------------

       IMRGRA =              0 (Reconstruction mode         )
       ANOMAX =    0.78540E+00 (Non-ortho angle: limit for  )
                               (least squares ext. neighbors)

-------------------------------------------------------------------
 Variable         NSWRGR NSWRSM      EPSRGR      EPSRSM      EXTRAG
-------------------------------------------------------------------
 Pressure            100      2  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityX           100      1  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityY           100      1  0.1000E-04  0.1000E-06  0.0000E+00
 VelocityZ           100      1  0.1000E-04  0.1000E-06  0.0000E+00
 TurbEner            100      1  0.1000E-04  0.1000E-06  0.0000E+00
 omega               100      1  0.1000E-04  0.1000E-06  0.0000E+00
-----------------------------------------------------------

-------------------------------------------
 Variable         IRCFLU IMLIGR      CLIMGR
-------------------------------------------
 Pressure              1     -1  0.1500E+01
 VelocityX             1     -1  0.1500E+01
 VelocityY             1     -1  0.1500E+01
 VelocityZ             1     -1  0.1500E+01
 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 =    0.10000E-04 (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  10000  0.1000E-07      1
 VelocityX            -1  10000  0.1000E-07      1
 VelocityY            -1  10000  0.1000E-07      1
 VelocityZ            -1  10000  0.1000E-07      1
 TurbEner             -1  10000  0.1000E-07      1
 omega                -1  10000  0.1000E-07      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)


  Multigrid rank merge parameters:
    mean  coarse cells merge threshold: 300
    total coarse cells merge threshold: 500
    minimum ranks merge threshold:      1
    merge stride:                       1

  Multigrid coarsening type: algebraic, face traveral by criteria

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


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

 --- Restarted calculation
       ISUITE =              0 (1: restarted calculation    )
       ILEAUX =              1 (1: read  restart/auxiliary  )
       IECAUX =              1 (1: write checkpoint/auxiliary)


 --- Calculation time
     The numbering of time steps and the measure of simulated
       physical time are absolute values, and not values
       relative to the current calculation.

       INPDT0 =              0 (1: 0 time step calcuation   )
       NTMABS =             20 (Final time step required    )

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


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


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

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

 --- Post-processed variables

       Number Name
         2 Pressure        
         3 VelocityX       
         4 VelocityY       
         5 VelocityZ       
         6 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  =              3 (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)


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


Postprocessing output writers:
------------------------------

  -1: name: results
      directory: postprocessing
      format: EnSight Gold
      options: binary
      time dependency: fixed mesh
      output: at calculation end


 Reading file:        mesh_input/mesh_01
 Finished reading:    mesh_input/mesh_01

 Reading file:        mesh_input/mesh_02
 Finished reading:    mesh_input/mesh_02
 No "partition_input/domain_number_4" file available;

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

 Partitioning 1629817 cells to 4 domains on 4 ranks
   (ParMETIS_V3_PartKway).

  Total number of faces on parallel boundaries: 2808
  wall-clock time: 2.801099 s

  Number of cells per domain (histogramm):
    [     402098 ;     403224 [ =          2
    [     403224 ;     404351 [ =          0
    [     404351 ;     405478 [ =          0
    [     405478 ;     406605 [ =          0
    [     406605 ;     407732 [ =          0
    [     407732 ;     408859 [ =          0
    [     408859 ;     409986 [ =          0
    [     409986 ;     411113 [ =          0
    [     411113 ;     412240 [ =          1
    [     412240 ;     413367 ] =          1

 Writing file:        partition_output/domain_number_4
 Finished writing:    partition_output/domain_number_4

 Partitioning finished (3.59 s)


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

 Halo construction with standard neighborhood
 ============================================

 Face interfaces creation
 Vertex interfaces creation
 Halo creation
 Halo definition
    Local halo definition
    Distant halo creation
    Updating the faces -> cells connectivity

 Histogram of the number of cells per rank:

    minimum value =             402098
    maximum value =             413367

      1 : [     402098 ;     404351 [ =          2
      2 : [     404351 ;     406605 [ =          0
      3 : [     406605 ;     408859 [ =          0
      4 : [     408859 ;     411113 [ =          0
      5 : [     411113 ;     413367 ] =          2

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

 Histogram of the number of standard + halo cells per rank:

    minimum value =             403313
    maximum value =             414731

      1 : [     403313 ;     405596 [ =          2
      2 : [     405596 ;     407880 [ =          0
      3 : [     407880 ;     410163 [ =          0
      4 : [     410163 ;     412447 [ =          0
      5 : [     412447 ;     414731 ] =          2

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

 Histogram of the number of ghost cells per rank:

    minimum value =                946
    maximum value =               1746

      1 : [        946 ;       1106 [ =          1
      2 : [       1106 ;       1266 [ =          1
      3 : [       1266 ;       1426 [ =          1
      4 : [       1426 ;       1586 [ =          0
      5 : [       1586 ;       1746 ] =          1

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

 Histogram of the number of interior faces per rank:

    minimum value =             784437
    maximum value =             797351

      1 : [     784437 ;     787019 [ =          1
      2 : [     787019 ;     789602 [ =          0
      3 : [     789602 ;     792185 [ =          1
      4 : [     792185 ;     794768 [ =          0
      5 : [     794768 ;     797351 ] =          2

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

 Histogram of the number of boundary faces per rank:

    minimum value =              29450
    maximum value =              60268

      1 : [      29450 ;      35613 [ =          1
      2 : [      35613 ;      41777 [ =          1
      3 : [      41777 ;      47940 [ =          0
      4 : [      47940 ;      54104 [ =          0
      5 : [      54104 ;      60268 ] =          2

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =        558
      2 : [          3 ;          4 ] =    1629259

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  1
    maximum value =                  3

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

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

 Global definition of the number of elements (cells, vertices, faces...)
Synchronizing cell families

 Writing file:        mesh_output
 Finished writing:    mesh_output

 Renumbering mesh:

Checking mesh renumbering for threads:
-------------------------------------


 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =             402261
    maximum value =             414049

      1 : [     402261 ;     404618 [ =          2
      2 : [     404618 ;     406976 [ =          0
      3 : [     406976 ;     409333 [ =          0
      4 : [     409333 ;     411691 [ =          0
      5 : [     411691 ;     414049 ] =          2

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =               1241
    maximum value =               7318

      1 : [       1241 ;       2456 [ =          1
      2 : [       2456 ;       3671 [ =          1
      3 : [       3671 ;       4887 [ =          1
      4 : [       4887 ;       6102 [ =          0
      5 : [       6102 ;       7318 ] =          1

 Mesh coordinates:               minimum    and maximum
                       X : -2.9999624e+01  6.1540000e+01
                       Y : -3.3797720e+01  2.9999972e+01
                       Z :  0.0000000e+00  2.9000000e+01
 Mesh
     Number of cells:          1629817
     Number of interior faces: 3166344
     Number of boundary faces: 186580
     Number of vertices:       324245

 Groups:
    "Inlet"
       boundary faces:           46
    "Outlet"
       boundary faces:           58
    "boundary"
       boundary faces:        24811
    "cells"
       cells:                925211
    "wall"
       boundary faces:       161665

 --- Information on the volumes
       Minimum control volume      =  6.1486888e-09
       Maximum control volume      =  9.9096864e+00
       Total volume for the domain =  2.1709497e+04

  Criterion 1: Orthogonality:
    Number of bad cells detected: 3 -->   0 %

  Criterion 2: Offset:
    Number of bad cells detected: 0 -->   0 %

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 36600 -->   2 %

  Criterion 4: Cells Volume Ratio:
    Number of bad cells detected: 7 -->   0 %

  Criterion 5: Guilt by Association:
    Number of bad cells detected: 0 -->   0 %

 Warning:
 --------
    Mesh quality issue has been detected

    The mesh should be re-considered using the listed criteria.

    The calculation will run but the solution quality may be degraded...

 Computing geometric quantities (1.79 s)
                                                             
       ALMAX  =    0.27804E+02 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.

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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Pressure          0.0000E+00  0.0000E+00
  VelocityX         0.0000E+00  0.0000E+00
  VelocityY         0.0000E+00  0.0000E+00
  VelocityZ         0.0000E+00  0.0000E+00
  TurbEner          0.6000E-03  0.6000E-03
  omega             0.8810E-03  0.8810E-03
 ---------------------------------

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



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

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



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



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


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




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


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


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1035E+04  0.1035E+04
  LamVisc           0.3500E-02  0.3500E-02
  TurbVisc          0.7049E+03  0.7049E+03
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2          46
Smooth wall               5      161665
Rough wall                6           0
Symmetry                  4       24811
Free outlet               3          58
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.61540E+02  -0.22826E+02   0.48947E+01



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46         0.000000000E+00
Smooth wall               5      161665         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.00000E+00 0.00000E+00
   Friction velocity        uk    :  0.78857E-02 0.13416E-01
   Dimensionless distance   yplus :  0.15009E+01 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         17
   Total number of wall faces                   :     161665
------------------------------------------------------------


@                                                            
@ @@ WARNING: Wall distance calculation                      
@    =========                                               
@  The laplacian solution does not respect the maximum       
@  principle. We recompute the laplacien without             
@  reconstructions.                                          

                                                             
 ** WALL DISTANCE                                            
    -------------                                            
                                                             
  Min distance =    0.52002E-03 Max distance =    0.41082E+01
                                                             
     (Distance calculation done in        973 iterations)

 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61724E-02    1937   0.33955E+01   0.94916E+00 
c  VelocityX    0.84876E-02       5   0.90948E-03   0.10854E-09 
c  VelocityY    0.84876E-02       5   0.90948E-03   0.29312E-10 
c  VelocityZ    0.84876E-02       5   0.90948E-03   0.30790E-10 
c  TurbEner     0.90869E+05      80   0.43838E-06   0.77155E-11 
c  omega        0.29668E+07    1231   0.33643E+00   0.86596E+04 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega           -0.21715                          1472


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                     0           95.47          22.054          24.882
v  Velocity[x]        -1.1709e-05      1.8586e-05      5.1132e-07      1.1346e-07
v  Velocity[y]        -2.2146e-05      9.4142e-07     -5.4902e-07     -4.4169e-08
v  Velocity[z]        -9.1009e-06      9.9758e-06      7.8478e-08     -4.1127e-08
v  TurbEner             0.0001247      0.00060031      0.00059783          0.0006
v  omega               6.3598e-09      4.9664e+05          69.044        0.014897
v  TurbVisc                704.89          704.89          704.89          704.89
v  CourantNb                    0               0               0               0
v  FourierNb            0.0015558          1587.9          13.476        0.054545
v  total_pressure      1.0132e+05      1.0142e+05      1.0135e+05      1.0135e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0015558          1587.9          13.476        0.054545


 TIME FOR THE TIME STEP                1:        0.30253E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.126108995E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431250025E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12547E-04 0.37327E-05
   Friction velocity        uet   :  0.00000E+00 0.21621E-05
   Friction velocity        uk    :  0.26412E-02 0.13420E-01
   Dimensionless distance   yplus :  0.52101E+00 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      30030
   Nb of faces within the viscous sub-layer     :         75
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.11997E-01    1327   0.81473E+00   0.10567E+01 
c  VelocityX    0.54688E+02     282   0.71941E-03   0.45829E-12 
c  VelocityY    0.54688E+02     282   0.71941E-03   0.61591E-12 
c  VelocityZ    0.54688E+02     282   0.71941E-03   0.16040E-12 
c  TurbEner     0.90783E+05       3   0.16054E-06   0.60674E-11 
c  omega        0.24920E+07   10000   0.38610E-01   0.15784E+04 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega          -0.030015                           835


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure            -0.0035653          4.2365         0.26049         0.77801
v  Velocity[x]        -1.0721e-05      1.8811e-05      5.1867e-07      1.1693e-07
v  Velocity[y]        -2.2973e-05      1.6586e-06     -5.5109e-07     -4.9948e-08
v  Velocity[z]        -1.0536e-05      1.0976e-05       7.659e-08     -4.2476e-08
v  TurbEner            2.8653e-06       0.0006005      0.00059608      0.00059999
v  omega               1.3103e-08      2.5131e+05          50.202        0.015014
v  TurbVisc            2.7306e-07      9.7644e+07          482.88          812.67
v  CourantNb                    0      1.0083e-05      1.2766e-07      6.6334e-10
v  FourierNb           4.4828e-05          6570.7         0.43161        0.064264
v  total_pressure      1.0132e+05      1.0133e+05      1.0133e+05      1.0133e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      4.4848e-05          6570.7         0.43161        0.064264


 TIME FOR THE TIME STEP                2:        0.63166E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665         0.728335599E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431250057E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12858E-04 0.37405E-05
   Friction velocity        uet   :  0.00000E+00 0.21680E-05
   Friction velocity        uk    :  0.16032E-03 0.13422E-01
   Dimensionless distance   yplus :  0.31626E-01 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      29958
   Nb of faces within the viscous sub-layer     :        303
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.10863E-01    1341   0.10062E+01   0.11408E+01 
c  VelocityX    0.58469E+02    1531   0.19138E-02   0.23618E-12 
c  VelocityY    0.58469E+02    1531   0.19138E-02   0.27999E-12 
c  VelocityZ    0.58469E+02    1531   0.19138E-02   0.11056E-12 
c  TurbEner     0.90780E+05    5409   0.15870E-06   0.47032E-11 
c  omega        0.19714E+07   10000   0.21197E-01   0.41630E+03 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega           -0.20581                           853


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure              -0.21154          1.8977       0.0066418         0.27667
v  Velocity[x]        -1.1039e-05      1.9388e-05      5.1937e-07      1.1801e-07
v  Velocity[y]        -2.3697e-05      2.2243e-06     -5.5163e-07     -5.2893e-08
v  Velocity[z]        -1.0986e-05      1.1436e-05      7.5285e-08     -4.2748e-08
v  TurbEner            1.2481e-07      0.00060066      0.00059475      0.00059999
v  omega               2.1314e-09      1.2861e+05          39.941        0.015139
v  TurbVisc            1.2166e-08      4.7395e+07          515.76          771.97
v  CourantNb                    0      9.8651e-06      1.2842e-07      6.6577e-10
v  FourierNb           4.4803e-05           17272         0.47747        0.061726
v  total_pressure      1.0132e+05      1.0133e+05      1.0133e+05      1.0133e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      4.4817e-05           17272         0.47747        0.061726


 TIME FOR THE TIME STEP                3:        0.10327E+04

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665         0.223917909E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431249959E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12827E-04 0.37372E-05
   Friction velocity        uet   :  0.00000E+00 0.22203E-05
   Friction velocity        uk    :  0.15378E-04 0.13424E-01
   Dimensionless distance   yplus :  0.30336E-02 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      29887
   Nb of faces within the viscous sub-layer     :        398
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13113E-01    1214   0.17052E+01   0.13438E+01 
c  VelocityX    0.58096E+02     300   0.21188E-02   0.47459E-13 
c  VelocityY    0.58096E+02     300   0.21188E-02   0.47441E-13 
c  VelocityZ    0.58096E+02     300   0.21188E-02   0.14279E-12 
c  TurbEner     0.90778E+05    1534   0.23614E-06   0.43214E-11 
c  omega        0.20563E+07    5337   0.35281E-01   0.11675E+03 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega          -0.090996                           760


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure              -0.19582         0.49231      -0.0094354        0.046517
v  Velocity[x]        -1.1164e-05       1.976e-05      5.1914e-07      1.1804e-07
v  Velocity[y]        -2.4091e-05      2.5451e-06     -5.5262e-07     -5.3501e-08
v  Velocity[z]        -1.1177e-05      1.1673e-05      7.4863e-08     -4.2868e-08
v  TurbEner            1.0179e-08      0.00060081      0.00059358      0.00059999
v  omega               4.4989e-09           67207          34.039        0.015279
v  TurbVisc            1.0348e-09      1.5809e+07          454.57          912.76
v  CourantNb                    0      9.7121e-06      1.2848e-07      6.6679e-10
v  FourierNb           4.4777e-05          1516.3         0.42049        0.060842
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0133e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      4.4791e-05          1516.3         0.42049        0.060842


 TIME FOR THE TIME STEP                4:        0.48151E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.165596048E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431250041E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12721E-04 0.37310E-05
   Friction velocity        uet   :  0.00000E+00 0.22697E-05
   Friction velocity        uk    :  0.23495E-05 0.13425E-01
   Dimensionless distance   yplus :  0.46347E-03 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      29810
   Nb of faces within the viscous sub-layer     :        464
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23432E-01     894   0.22437E+01   0.15573E+01 
c  VelocityX    0.57758E+02     515   0.31608E-02   0.13869E-13 
c  VelocityY    0.57758E+02     515   0.31608E-02   0.14667E-13 
c  VelocityZ    0.57758E+02     515   0.31608E-02   0.53617E-12 
c  TurbEner     0.90776E+05   10000   0.13898E-06   0.44081E-11 
c  omega        0.19891E+07   10000   0.33155E-01   0.36411E+02 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega           -0.18917                           730


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure              -0.28104         0.18866      -0.0036816       -0.031082
v  Velocity[x]        -1.1241e-05      1.9999e-05      5.1905e-07      1.1781e-07
v  Velocity[y]        -2.4332e-05      2.7393e-06     -5.5359e-07     -5.3185e-08
v  Velocity[z]        -1.1281e-05      1.1839e-05      7.4969e-08     -4.3091e-08
v  TurbEner            1.4737e-09        0.000601      0.00059251      0.00059998
v  omega                1.405e-08           36410          30.397        0.015428
v  TurbVisc            1.6128e-10      1.3803e+08          520.58          876.24
v  CourantNb                    0      9.6538e-06      1.2866e-07      6.6686e-10
v  FourierNb           4.4752e-05           22343         0.43811        0.066203
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0132e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      4.4765e-05           22343         0.43811        0.066203


 TIME FOR THE TIME STEP                5:        0.10838E+04

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665         0.760010690E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431250069E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12591E-04 0.37251E-05
   Friction velocity        uet   :  0.00000E+00 0.23134E-05
   Friction velocity        uk    :  0.55159E-06 0.13427E-01
   Dimensionless distance   yplus :  0.10832E-03 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      29739
   Nb of faces within the viscous sub-layer     :        526
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.48963E-01     931   0.25141E+01   0.16444E+01 
c  VelocityX    0.58071E+02     391   0.38517E-02   0.34483E-13 
c  VelocityY    0.58071E+02     391   0.38517E-02   0.36558E-13 
c  VelocityZ    0.58071E+02     391   0.38517E-02   0.27547E-11 
c  TurbEner     0.90775E+05    7707   0.20444E-06   0.40285E-11 
c  omega        0.23709E+07   10000   0.77408E-01   0.13225E+02 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega           -0.12505                           693


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure              -0.64068         0.56764      -0.0010802       -0.037431
v  Velocity[x]         -1.139e-05      2.0168e-05      5.1921e-07      1.1762e-07
v  Velocity[y]        -2.4493e-05      2.8645e-06     -5.5441e-07     -5.2703e-08
v  Velocity[z]        -1.1343e-05      1.1968e-05      7.5263e-08     -4.3533e-08
v  TurbEner            3.4939e-10      0.00060119       0.0005915      0.00059998
v  omega               2.8465e-08           20861           27.97        0.015583
v  TurbVisc            4.3006e-11        4.42e+07          473.39          1159.2
v  CourantNb                    0      9.6327e-06      1.2888e-07       6.668e-10
v  FourierNb           4.4727e-05          9885.5         0.42386        0.062088
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0132e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       4.474e-05          9885.5         0.42386        0.062088


 TIME FOR THE TIME STEP                6:        0.96319E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.759737257E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431250144E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12450E-04 0.37219E-05
   Friction velocity        uet   :  0.00000E+00 0.23526E-05
   Friction velocity        uk    :  0.18743E-06 0.13428E-01
   Dimensionless distance   yplus :  0.36974E-04 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      29666
   Nb of faces within the viscous sub-layer     :        595
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.11077E+00     929   0.26305E+01   0.16785E+01 
c  VelocityX    0.61234E+02     614   0.17341E-02   0.13176E-12 
c  VelocityY    0.61234E+02     614   0.17341E-02   0.13727E-12 
c  VelocityZ    0.61234E+02     614   0.17341E-02   0.15315E-10 
c  TurbEner     0.90773E+05    1906   0.12027E-06   0.39261E-11 
c  omega        0.20136E+07   10000   0.11655E-01   0.57151E+01 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega           -0.21444                           647


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -1.4825          1.2899      -0.0011074       -0.025785
v  Velocity[x]        -1.1527e-05      2.0312e-05      5.1948e-07      1.1745e-07
v  Velocity[y]         -2.461e-05      2.9477e-06     -5.5512e-07     -5.2204e-08
v  Velocity[z]        -1.1382e-05      1.2071e-05      7.5567e-08     -4.4232e-08
v  TurbEner            1.2236e-10      0.00060137      0.00059055      0.00059997
v  omega               1.1529e-08           12880          26.232        0.015724
v  TurbVisc            1.7738e-11      2.1816e+07          471.56          905.58
v  CourantNb                    0       9.627e-06      1.2912e-07      6.6743e-10
v  FourierNb           4.4702e-05          5247.8         0.42022        0.059835
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0132e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      4.4715e-05          5247.8         0.42022        0.059835


 TIME FOR THE TIME STEP                7:        0.73827E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665         0.691655165E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431250315E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12060E-04 0.37194E-05
   Friction velocity        uet   :  0.00000E+00 0.23873E-05
   Friction velocity        uk    :  0.85332E-07 0.13430E-01
   Dimensionless distance   yplus :  0.16833E-04 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      29578
   Nb of faces within the viscous sub-layer     :        651
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.25804E+00     942   0.26949E+01   0.16955E+01 
c  VelocityX    0.77038E+02     423   0.60861E-02   0.68825E-12 
c  VelocityY    0.77038E+02     423   0.60861E-02   0.69357E-12 
c  VelocityZ    0.77038E+02     423   0.60861E-02   0.86167E-10 
c  TurbEner     0.90772E+05   10000   0.44933E-06   0.38578E-11 
c  omega        0.21814E+07   10000   0.28761E-01   0.28997E+01 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega           -0.12768                           660


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -3.525          2.9872      3.8688e-05       -0.017785
v  Velocity[x]        -1.1643e-05      2.0429e-05      5.1958e-07      1.1717e-07
v  Velocity[y]        -2.4707e-05      3.0038e-06     -5.5591e-07      -5.153e-08
v  Velocity[z]        -1.9559e-05      1.5259e-05      7.5825e-08     -4.4872e-08
v  TurbEner            5.6876e-11      0.00060154      0.00058964      0.00059997
v  omega               1.5404e-09          8656.6          24.907        0.015862
v  TurbVisc            1.0019e-11      5.3866e+07          519.85          910.68
v  CourantNb                    0      9.6298e-06      1.2934e-07      6.7048e-10
v  FourierNb           4.4677e-05           18995         0.45179        0.062767
v  total_pressure      1.0132e+05      1.0133e+05      1.0133e+05      1.0132e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       4.469e-05           18995         0.45179        0.062767


 TIME FOR THE TIME STEP                8:        0.10684E+04

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665         0.535930952E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431250578E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11934E-04 0.37179E-05
   Friction velocity        uet   :  0.00000E+00 0.24189E-05
   Friction velocity        uk    :  0.48037E-07 0.13431E-01
   Dimensionless distance   yplus :  0.94762E-05 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      29497
   Nb of faces within the viscous sub-layer     :        711
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.61035E+00     917   0.27395E+01   0.17065E+01 
c  VelocityX    0.13534E+03     333   0.31200E-02   0.39792E-11 
c  VelocityY    0.13534E+03     333   0.31200E-02   0.39741E-11 
c  VelocityZ    0.13534E+03     333   0.31200E-02   0.49342E-09 
c  TurbEner     0.90771E+05   10000   0.15178E-06   0.37935E-11 
c  omega        0.20683E+07   10000   0.17479E-01   0.16696E+01 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega           -0.22149                           625


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -8.3753          7.2171      -0.0027729       -0.037799
v  Velocity[x]         -1.175e-05      2.0536e-05      5.1917e-07      1.1638e-07
v  Velocity[y]        -2.4806e-05      3.3811e-06     -5.5706e-07     -5.0032e-08
v  Velocity[z]          -4.69e-05      4.0597e-05      7.6137e-08     -4.4333e-08
v  TurbEner            3.2055e-11      0.00060171      0.00058877      0.00059997
v  omega               8.6453e-09          6334.4          23.849        0.015998
v  TurbVisc             6.898e-12      4.0314e+08          703.92          1011.1
v  CourantNb                    0      9.6411e-06      1.2956e-07      6.8002e-10
v  FourierNb           4.4653e-05      1.2766e+05         0.55655        0.080013
v  total_pressure      1.0132e+05      1.0133e+05      1.0132e+05      1.0132e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      4.4665e-05      1.2766e+05         0.55655        0.080013


 TIME FOR THE TIME STEP                9:        0.10524E+04

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.682718924E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431251788E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11819E-04 0.38085E-05
   Friction velocity        uet   :  0.00000E+00 0.24502E-05
   Friction velocity        uk    :  0.31246E-07 0.13432E-01
   Dimensionless distance   yplus :  0.61639E-05 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      29421
   Nb of faces within the viscous sub-layer     :        757
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12


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


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

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

   ** Writing the auxiliary restart file
      ----------------------------------

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


 Time for restart files:    0.70642E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.14700E+01     913   0.27642E+01   0.17071E+01 
c  VelocityX    0.29919E+03     468   0.16385E-02   0.23181E-10 
c  VelocityY    0.29919E+03     468   0.16385E-02   0.22726E-10 
c  VelocityZ    0.29919E+03     468   0.16385E-02   0.29544E-08 
c  TurbEner     0.90770E+05    1928   0.31232E-06   0.37788E-11 
c  omega        0.20667E+07   10000   0.15724E-01   0.10567E+01 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega          -0.055808                           525


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -19.909           16.84      -0.0088522       -0.090347
v  Velocity[x]        -1.1867e-05      2.0659e-05      5.1767e-07      1.1452e-07
v  Velocity[y]        -2.4936e-05      8.2953e-06     -5.5913e-07     -4.6615e-08
v  Velocity[z]        -0.00011221      0.00010845      7.6633e-08     -3.7551e-08
v  TurbEner            2.0521e-11      0.00060187      0.00058793      0.00059996
v  omega               4.2914e-08          5014.4          22.972        0.016123
v  TurbVisc            5.2997e-12       1.952e+07          482.66          982.68
v  CourantNb                    0      9.6644e-06      1.2978e-07      7.0547e-10
v  FourierNb           4.4628e-05          6848.4          0.4148        0.060096
v  total_pressure      1.0131e+05      1.0134e+05      1.0132e+05      1.0132e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       4.464e-05          6848.4          0.4148        0.060096


 TIME FOR THE TIME STEP               10:        0.70811E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665         0.104843994E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431254110E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11727E-04 0.92541E-05
   Friction velocity        uet   :  0.00000E+00 0.24845E-05
   Friction velocity        uk    :  0.22363E-07 0.13434E-01
   Dimensionless distance   yplus :  0.44116E-05 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      29329
   Nb of faces within the viscous sub-layer     :        797
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.35832E+01     909   0.27864E+01   0.17067E+01 
c  VelocityX    0.71568E+03     458   0.12864E-02   0.13920E-09 
c  VelocityY    0.71568E+03     458   0.12864E-02   0.13283E-09 
c  VelocityZ    0.71568E+03     458   0.12864E-02   0.17969E-07 
c  TurbEner     0.90769E+05     346   0.94152E-07   0.37315E-11 
c  omega        0.21231E+07    5332   0.21350E-01   0.71760E+00 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega           -0.16024                           547


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -49.679          39.851       -0.024613        -0.20688
v  Velocity[x]        -2.3956e-05      2.2027e-05      5.1344e-07      1.1002e-07
v  Velocity[y]        -2.5154e-05      1.9749e-05     -5.6344e-07     -3.8867e-08
v  Velocity[z]        -0.00026845      0.00029047       7.751e-08      -8.436e-09
v  TurbEner            1.4293e-11      0.00060202      0.00058712      0.00059996
v  omega               1.5002e-08          4212.7          22.224        0.016253
v  TurbVisc            4.2929e-12      1.4471e+07          450.78          995.56
v  CourantNb                    0      9.7135e-06      1.3004e-07      7.7258e-10
v  FourierNb           4.4604e-05          4304.4         0.39202         0.05756
v  total_pressure      1.0128e+05      1.0136e+05      1.0132e+05      1.0132e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      4.4615e-05          4304.4         0.39202         0.05756


 TIME FOR THE TIME STEP               11:        0.42728E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665         0.430949614E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431259221E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11686E-04 0.22296E-04
   Friction velocity        uet   :  0.00000E+00 0.25278E-05
   Friction velocity        uk    :  0.17050E-07 0.13435E-01
   Dimensionless distance   yplus :  0.33634E-05 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      29227
   Nb of faces within the viscous sub-layer     :        832
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.88338E+01     907   0.28073E+01   0.17063E+01 
c  VelocityX    0.17534E+04     519   0.96293E-03   0.85882E-09 
c  VelocityY    0.17534E+04     519   0.96293E-03   0.79541E-09 
c  VelocityZ    0.17534E+04     519   0.96293E-03   0.11161E-06 
c  TurbEner     0.90768E+05     480   0.12175E-06   0.37405E-11 
c  omega        0.21111E+07    2344   0.10023E-01   0.51367E+00 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega          -0.059806                           533


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -131.84           107.7       -0.062351        -0.45489
v  Velocity[x]        -6.3869e-05      5.8794e-05      5.0237e-07      9.9202e-08
v  Velocity[y]        -4.4815e-05      5.1246e-05     -5.7337e-07     -2.1433e-08
v  Velocity[z]        -0.00064241      0.00077984      7.9081e-08      9.4889e-08
v  TurbEner            1.0534e-11      0.00060217      0.00058634      0.00059996
v  omega               1.5298e-08          3693.3          21.574        0.016383
v  TurbVisc             3.551e-12      7.9597e+06          429.65          1084.6
v  CourantNb                    0      9.8191e-06      1.3039e-07      9.4723e-10
v  FourierNb           4.4579e-05          1291.2          0.3764        0.056345
v  total_pressure      1.0119e+05      1.0143e+05      1.0132e+05      1.0132e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       4.459e-05          1291.2          0.3764        0.056345


 TIME FOR THE TIME STEP               12:        0.31073E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665         0.591988077E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431271668E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11763E-04 0.53554E-04
   Friction velocity        uet   :  0.00000E+00 0.33764E-05
   Friction velocity        uk    :  0.13562E-07 0.13436E-01
   Dimensionless distance   yplus :  0.26754E-05 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      29138
   Nb of faces within the viscous sub-layer     :        875
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.21997E+02     895   0.28285E+01   0.17064E+01 
c  VelocityX    0.43516E+04     272   0.53978E-03   0.54233E-08 
c  VelocityY    0.43516E+04     272   0.53978E-03   0.48604E-08 
c  VelocityZ    0.43516E+04     272   0.53978E-03   0.70574E-06 
c  TurbEner     0.90767E+05    3144   0.66825E-05   0.72277E-11 
c  omega        0.21527E+07   10000   0.87705E-02   0.38324E+00 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega           -0.17126                           523


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                  -353          290.54         -0.1552         -1.0034
v  Velocity[x]        -0.00017134      0.00015788      4.7393e-07      7.3397e-08
v  Velocity[y]         -0.0001063      0.00013759     -5.9746e-07      1.8211e-08
v  Velocity[z]         -0.0015377       0.0020973       8.225e-08      4.2782e-07
v  TurbEner            8.0805e-12      0.00060247      0.00058558      0.00059995
v  omega               6.9564e-09          3360.4          20.998        0.016511
v  TurbVisc             2.963e-12      2.0236e+07          449.22          1149.5
v  CourantNb                    0      1.0063e-05      1.3096e-07      1.3984e-09
v  FourierNb           4.4555e-05          3589.3         0.38455         0.05853
v  total_pressure      1.0097e+05      1.0162e+05      1.0132e+05      1.0132e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      4.4565e-05          3589.3         0.38455         0.05853


 TIME FOR THE TIME STEP               13:        0.74628E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665         0.198927773E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431301619E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12126E-04 0.12827E-03
   Friction velocity        uet   :  0.00000E+00 0.80873E-05
   Friction velocity        uk    :  0.11116E-07 0.13437E-01
   Dimensionless distance   yplus :  0.21929E-05 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      29050
   Nb of faces within the viscous sub-layer     :        922
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.55265E+02     892   0.28507E+01   0.17073E+01 
c  VelocityX    0.10908E+05      82   0.29157E-03   0.34867E-07 
c  VelocityY    0.10908E+05      82   0.29157E-03   0.30213E-07 
c  VelocityZ    0.10908E+05      82   0.29157E-03   0.45352E-05 
c  TurbEner     0.90767E+05    9301   0.13162E-06   0.37945E-11 
c  omega        0.21518E+07   10000   0.40823E-02   0.29566E+00 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega          -0.059828                           521


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -948.15          783.45        -0.38513         -2.2278
v  Velocity[x]        -0.00046107      0.00042465      4.0256e-07      1.2837e-08
v  Velocity[y]        -0.00025416      0.00037027     -6.5638e-07      1.0929e-07
v  Velocity[z]         -0.0036803       0.0056458      8.9525e-08      1.4457e-06
v  TurbEner            6.3902e-12      0.00060249      0.00058484      0.00059995
v  omega               6.2349e-08          3143.9          20.481        0.016633
v  TurbVisc            2.4887e-12       8.927e+07          552.04          1006.6
v  CourantNb                    0      1.0645e-05      1.3212e-07      2.5369e-09
v  FourierNb           4.4531e-05           14294         0.42608        0.069163
v  total_pressure      1.0038e+05      1.0211e+05      1.0132e+05      1.0132e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      4.4537e-05           14294         0.42608        0.069163


 TIME FOR THE TIME STEP               14:        0.10015E+04

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665         0.259522812E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431373359E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13177E-04 0.34036E-03
   Friction velocity        uet   :  0.00000E+00 0.21334E-04
   Friction velocity        uk    :  0.93223E-08 0.13439E-01
   Dimensionless distance   yplus :  0.18390E-05 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      28939
   Nb of faces within the viscous sub-layer     :        947
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.14000E+03     878   0.28734E+01   0.17090E+01 
c  VelocityX    0.27586E+05     116   0.17047E-03   0.22782E-06 
c  VelocityY    0.27586E+05     116   0.17047E-03   0.19085E-06 
c  VelocityZ    0.27586E+05     116   0.17047E-03   0.29594E-04 
c  TurbEner     0.90765E+05    2380   0.41277E-06   0.39516E-11 
c  omega        0.22763E+07    9552   0.69183E-01   0.23445E+00 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega          -0.032881                           392


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -2549.5            2113        -0.93955         -4.9247
v  Velocity[x]         -0.0012423       0.0011432      2.2543e-07     -1.2804e-07
v  Velocity[y]        -0.00063171      0.00099751     -8.0078e-07      3.1919e-07
v  Velocity[z]         -0.0088084        0.015206      1.0788e-07      4.4592e-06
v  TurbEner            5.1802e-12       0.0006026      0.00058413      0.00059995
v  omega               2.2959e-08          2994.3          20.013        0.016741
v  TurbVisc            2.1037e-12      9.9602e+06          432.82          881.44
v  CourantNb                    0      1.2049e-05      1.3517e-07       5.391e-09
v  FourierNb           4.4507e-05          3967.6         0.37416        0.055013
v  total_pressure           98776      1.0344e+05      1.0132e+05      1.0132e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      4.4511e-05          3967.6         0.37416        0.055013


 TIME FOR THE TIME STEP               15:        0.67100E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665         0.285778319E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.431643564E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16118E-04 0.91660E-03
   Friction velocity        uet   :  0.00000E+00 0.57454E-04
   Friction velocity        uk    :  0.79643E-08 0.13440E-01
   Dimensionless distance   yplus :  0.15711E-05 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      28856
   Nb of faces within the viscous sub-layer     :        972
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.35746E+03     873   0.28955E+01   0.17108E+01 
c  VelocityX    0.70325E+05      35   0.11203E-03   0.15105E-05 
c  VelocityY    0.70325E+05      35   0.11203E-03   0.12232E-05 
c  VelocityZ    0.70325E+05      35   0.11203E-03   0.19594E-03 
c  TurbEner     0.90764E+05    2314   0.17310E-06   0.42302E-11 
c  omega        0.21937E+07   10000   0.87550E-02   0.18959E+00 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega          -0.076914                           489


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure               -6859.4          5699.8         -2.2969         -10.892
v  Velocity[x]         -0.0033488       0.0030788     -2.1098e-07     -4.5309e-07
v  Velocity[y]         -0.0016387       0.0026888     -1.1533e-06       8.054e-07
v  Velocity[z]           -0.02108         0.04097      1.5775e-07       1.319e-05
v  TurbEner            4.2897e-12      0.00060273      0.00058343      0.00059994
v  omega                3.637e-09          2889.9          19.585        0.016845
v  TurbVisc            1.7906e-12      2.7048e+07           429.8          988.39
v  CourantNb                    0      1.5458e-05      1.5129e-07      1.2542e-08
v  FourierNb           4.4483e-05          5838.9         0.36721        0.055247
v  total_pressure           94466      1.0702e+05      1.0132e+05      1.0131e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       4.451e-05          5838.9         0.36721        0.055247


 TIME FOR THE TIME STEP               16:        0.68251E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665         0.127568108E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.432170079E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23866E-04 0.24686E-02
   Friction velocity        uet   :  0.00000E+00 0.15474E-03
   Friction velocity        uk    :  0.69137E-08 0.13441E-01
   Dimensionless distance   yplus :  0.13638E-05 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      28765
   Nb of faces within the viscous sub-layer     :       1003
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.91942E+03     871   0.29163E+01   0.17126E+01 
c  VelocityX    0.18062E+06      13   0.73036E-04   0.10150E-04 
c  VelocityY    0.18062E+06      13   0.73036E-04   0.79515E-05 
c  VelocityZ    0.18062E+06      13   0.73036E-04   0.13148E-02 
c  TurbEner     0.90763E+05    7550   0.21499E-06   0.50064E-11 
c  omega        0.22403E+07   10000   0.10602E-01   0.15687E+00 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega           -0.10771                           427


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -18461           15379         -5.5723         -24.073
v  Velocity[x]         -0.0090287       0.0082948     -1.2781e-06     -1.1954e-06
v  Velocity[y]         -0.0044035       0.0072492     -2.0108e-06      1.9382e-06
v  Velocity[z]          -0.050448         0.11041      2.9935e-07      3.8098e-05
v  TurbEner             3.621e-12      0.00060285      0.00058275      0.00059994
v  omega               2.6685e-08          2816.3           19.19         0.01694
v  TurbVisc            1.5364e-12      2.4458e+07          434.03          779.82
v  CourantNb                    0      2.3726e-05       2.381e-07      3.0452e-08
v  FourierNb            4.446e-05          8007.5         0.37111        0.053954
v  total_pressure           82864       1.167e+05      1.0132e+05       1.013e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      4.4543e-05          8007.5         0.37111        0.053954


 TIME FOR THE TIME STEP               17:        0.91045E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.230847243E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.433465724E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42812E-04 0.66507E-02
   Friction velocity        uet   :  0.00000E+00 0.41688E-03
   Friction velocity        uk    :  0.60885E-08 0.13442E-01
   Dimensionless distance   yplus :  0.12011E-05 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      28665
   Nb of faces within the viscous sub-layer     :       1028
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23809E+04     858   0.29351E+01   0.17143E+01 
c  VelocityX    0.46711E+06      11   0.41466E-04   0.69029E-04 
c  VelocityY    0.46711E+06      11   0.41466E-04   0.52385E-04 
c  VelocityZ    0.46711E+06      11   0.41466E-04   0.89291E-02 
c  TurbEner     0.90762E+05    1309   0.55225E-06   0.76748E-11 
c  omega        0.22692E+07    4349   0.26595E-01   0.13162E+00 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega           -0.15722                           416


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure                -49693           41503         -13.453         -52.979
v  Velocity[x]          -0.024343        0.022354      -3.869e-06     -2.8697e-06
v  Velocity[y]          -0.011844        0.019546     -4.0836e-06      4.5893e-06
v  Velocity[z]           -0.12071         0.29761      7.1044e-07      0.00010835
v  TurbEner            3.1116e-12      0.00060312      0.00058209      0.00059994
v  omega               1.6456e-09          2764.3          18.825        0.017039
v  TurbVisc            1.3307e-12      2.0776e+07           431.1          894.85
v  CourantNb                    0      4.3722e-05       4.844e-07      7.5117e-08
v  FourierNb           2.0936e-05          2250.6         0.35568        0.056267
v  total_pressure           51632      1.4283e+05      1.0131e+05      1.0127e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      2.6718e-05          2250.6         0.35568        0.056267


 TIME FOR THE TIME STEP               18:        0.37189E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665        -0.532452879E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.436643931E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88583E-04 0.17914E-01
   Friction velocity        uet   :  0.00000E+00 0.11229E-02
   Friction velocity        uk    :  0.54341E-08 0.13451E-01
   Dimensionless distance   yplus :  0.10720E-05 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      28569
   Nb of faces within the viscous sub-layer     :       1055
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62030E+04     842   0.29519E+01   0.17157E+01 
c  VelocityX    0.12155E+07      11   0.18948E-04   0.47431E-03 
c  VelocityY    0.12155E+07      11   0.18948E-04   0.34945E-03 
c  VelocityZ    0.12155E+07      11   0.18948E-04   0.61287E-01 
c  TurbEner     0.90761E+05    6446   0.37284E-04   0.37214E-09 
c  omega        0.28057E+07   10000   0.44722E-01   0.11212E+00 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega          -0.050217                           425


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure           -1.3381e+05      1.1199e+05         -32.148         -116.06
v  Velocity[x]          -0.065639        0.060252     -1.0119e-05     -6.5708e-06
v  Velocity[y]          -0.031877        0.052721     -9.0736e-06      1.0834e-05
v  Velocity[z]           -0.28879         0.80226       1.913e-06      0.00030478
v  TurbEner            2.7196e-12      0.00061357      0.00058144      0.00059993
v  omega               3.9711e-08          2727.2          18.484        0.017135
v  TurbVisc             1.165e-12      3.5766e+07          450.69          856.32
v  CourantNb                    0       9.196e-05      1.1015e-06      1.8682e-07
v  FourierNb           8.2896e-06          3483.7         0.36682        0.058151
v  total_pressure          -32483      2.1332e+05      1.0129e+05      1.0121e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      1.3328e-05          3483.7         0.36682        0.058151


 TIME FOR THE TIME STEP               19:        0.85406E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.431250000E-01
Smooth wall               5      161665         0.829537130E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4       24811         0.000000000E+00
Free outlet               3          58         0.448621613E-01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19833E-03 0.44969E-01
   Friction velocity        uet   :  0.00000E+00 0.30185E-02
   Friction velocity        uk    :  0.49122E-08 0.13567E-01
   Dimensionless distance   yplus :  0.96901E-06 0.51071E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      28457
   Nb of faces within the viscous sub-layer     :       1082
   Total number of wall faces                   :     161665
------------------------------------------------------------


 Warning:
 --------
   _iterative_scalar_gradient; variable: Var.  0; sweeps: 100
                               normed residual:  5.3304e-01; norm:  9.7245e-12


 Write final restart files
   checkpoint at iteration         20, Physical time    0.20000E-01


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

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

   ** Writing the auxiliary restart file
      ----------------------------------

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


 Time for restart files:    0.72093E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.16248E+05     837   0.29668E+01   0.17170E+01 
c  VelocityX    0.31804E+07       9   0.12137E-04   0.32888E-02 
c  VelocityY    0.31804E+07       9   0.12137E-04   0.23584E-02 
c  VelocityZ    0.31804E+07       9   0.12137E-04   0.42455E+00 
c  TurbEner     0.90759E+05   10000   0.62243E-05   0.86926E-11 
c  omega        0.26036E+07   10000   0.10837E+00   0.98082E-01 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field        initial min     initial max  clips to min  clips to max
-  --------  --------------  --------------  ------------  ------------
a  TurbEner
a  omega          -0.086664                           407


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Pressure           -3.6047e+05       3.021e+05         -76.944         -254.37
v  Velocity[x]           -0.17706         0.16242     -2.5036e-05      -1.451e-05
v  Velocity[y]          -0.085828         0.14229     -2.0939e-05      2.5682e-05
v  Velocity[z]           -0.69079          2.1627      5.4286e-06      0.00085032
v  TurbEner            2.4161e-12      0.00061362      0.00058081      0.00059993
v  omega               3.5599e-08          2700.8          18.164        0.017239
v  TurbVisc            1.0321e-12      1.5638e+07          440.61          967.73
v  CourantNb                    0        0.000208      2.6088e-06      4.6754e-07
v  FourierNb           3.2927e-06          5747.3         0.35259        0.057718
v  total_pressure     -2.5915e+05      4.0343e+05      1.0125e+05      1.0107e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      1.1347e-05          5747.3          0.3526        0.057718


 TIME FOR THE TIME STEP               20:        0.10227E+04

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.48563E-03
      -----------------------                                



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




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


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

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:          14927.692 s
  System CPU time:           37.112 s
  Total CPU time:         59856.376 s

  Elapsed time:           15072.454 s
  CPU / elapsed time          0.993

Memory use summary:

  Total memory used:                               2.825 GiB
                             local minimum:      705.031 MiB  (rank 0)
                             local maximum:      739.961 MiB  (rank 2)
  Theoretical instrumented dynamic memory:         1.306 GiB
                             local minimum:      329.873 MiB  (rank 0)
                             local maximum:      339.442 MiB  (rank 2)
