command: 
 /exports/work/eng_software/CodeSaturne-3.1.0-openmpi/libexec/code_saturne/cs_solver --param NACA0012.xml --mpi

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

                                  (R)
                      Code_Saturne

                      Version 3.1.0


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

  build Wed 25 Sep 2013 13:32:54 BST
  MPI version 2.1 (Open MPI 1.6.2)


  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:                Wed 13 Aug 2014 12:16:52 BST
  System:              Linux 2.6.32-431.20.3.el6.x86_64
  Machine:             eddie429
  Processor:           model name	: Intel(R) Xeon(R) CPU           E5645  @ 2.40GHz
  Memory:              24017 MB
  User:                s0341262 (Susan Tully)
  Directory:           /exports/work/see_ies_marine/sTully/ALE/tutorial/RESU/20140813-1216
  MPI ranks:           12 (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:
    METIS
    PT-SCOTCH 6.0.0

 Reading metadata from file: "mesh_input"

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

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


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




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


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

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

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


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

 --- Physics
       NVAR   =              9 (Nb variables                )
       NSCAL  =              0 (Nb scalars                  )
       NSCAUS =              0 (Nb user scalars             )
       NSCAPP =              0 (Nb specific physics scalars )
       NPROCE =              7 (Nb cell properties          )
       NPROFA =              1 (Nb internal face properties )
       NPROFB =              2 (Nb boundary face properties )


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


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

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

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

  -- Continuous phase:

       RO0    =    0.10000E+04 (Reference density           )
       VISCL0 =    0.10000E-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

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


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

 --- Continuous phase:

   - Commons
       ITURB  =             20 (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)     )
       ISCALT =             -1 (Temperature salar number    )

   - k-epsilon           (ITURB = 20)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       ICLKEP =              0 (k-epsilon clipping model    )
       IKECOU =              1 (k-epsilon coupling mode     )
       IGRAKE =              1 (Account for gravity         )


   - 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-epsilon           (ITURB = 20)
       Ce1    =    0.14400E+01 (Cepsilon 1: production coef.)
       CE2    =    0.19200E+01 (Cepsilon 2: dissipat.  coef.)
       SIGMAK =    0.10000E+01 (Prandtl relative to k       )
       SIGMAE =    0.13000E+01 (Prandtl relative to epsilon )
       CMU    =    0.90000E-01 (Cmu constant                )


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


 ** 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-01 (Minimum time step           )
       DTMAX  =    0.10000E+03 (Maximum time step           )
       DTREF  =    0.10000E+00 (Reference time step         )

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

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

------------------------------------
 Variable          ISTAT      CDTVAR
------------------------------------
 Pressure              0  0.1000E+01
 VelocityX             1  0.1000E+01
 VelocityY             1  0.1000E+01
 VelocityZ             1  0.1000E+01
 TurbEner              1  0.1000E+01
 Dissip                1  0.1000E+01
 mesh_u                0  0.1000E+01
 mesh_v                0  0.1000E+01
 mesh_w                0  0.1000E+01
----------------------------

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

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

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


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

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

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


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


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

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

       RELAXV =    0.10000E+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 =              2 (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
 Dissip              100      1  0.1000E-04  0.1000E-06  0.0000E+00
 mesh_u              100      1  0.1000E-04  0.1000E-06  0.0000E+00
 mesh_v              100      1  0.1000E-04  0.1000E-06  0.0000E+00
 mesh_w              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
 Dissip                1      1  0.1500E+01
 mesh_u                1      1  0.1500E+01
 mesh_v                1      1  0.1500E+01
 mesh_w                1      1  0.1500E+01
-----------------------------------

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


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


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


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


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

       NBMOMT =              0 (Number of moments           )

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


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

--------------------------------------------------
 Variable         IRESOL NITMAX      EPSILO IDIRCL
--------------------------------------------------
 Pressure              0  10000  0.1000E-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
 Dissip               -1  10000  0.1000E-07      1
 mesh_u               -1  10000  0.1000E-07      1
 mesh_v               -1  10000  0.1000E-07      1
 mesh_w               -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
 Dissip                0    100     10
 mesh_u                0    100     10
 mesh_v                0    100     10
 mesh_w                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 =          15000 (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 Dissip          
         8 mesh_u          
         9 mesh_v          
        10 mesh_w          
        13 TurbVisc        
        14 CourantNb       
        15 FourierNb       
        16 total_pressure  
        17 mesh_vi1        
         --           --

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

       Number Name                  Nb. probes (-1: all)
         2 Pressure                      -1
         3 VelocityX                     -1
         4 VelocityY                     -1
         5 VelocityZ                     -1
         6 TurbEner                      -1
         7 Dissip                        -1
         8 mesh_u                        -1
         9 mesh_v                        -1
        10 mesh_w                        -1
        11 Density                       -1
        12 LamVisc                       -1
        13 TurbVisc                      -1
        14 CourantNb                     -1
        15 FourierNb                     -1
        16 total_pressure                -1
        17 mesh_vi1                      -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 Dissip                         0
         8 mesh_u                         0
         9 mesh_v                         0
        10 mesh_w                         0
        13 TurbVisc                    -999
        14 CourantNb                   -999
        15 FourierNb                   -999
        16 total_pressure              -999
        17 mesh_vi1                    -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   =              1 (1: activated                )
       NALINF =           5000 (Fluid initialization
                                                  iterations)


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


 Reading file:        mesh_input
 Finished reading:    mesh_input
 No "partition_input/domain_number_12" file available;

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

 Partitioning 67600 cells to 12 domains on 12 ranks
   (SCOTCH_dgraphPart).

  wall-clock time: 0.321630 s

  Number of cells per domain (histogramm):
    [       5515 ;       5549 [ =          2
    [       5549 ;       5583 [ =          0
    [       5583 ;       5618 [ =          2
    [       5618 ;       5652 [ =          6
    [       5652 ;       5687 [ =          1
    [       5687 ;       5721 [ =          0
    [       5721 ;       5755 [ =          0
    [       5755 ;       5790 [ =          0
    [       5790 ;       5824 [ =          0
    [       5824 ;       5859 ] =          1

 Writing file:        partition_output/domain_number_12
 Finished writing:    partition_output/domain_number_12

 Partitioning finished (0.351 s)


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

  -1: name: results
      directory: postprocessing
      format: EnSight Gold
      options: binary
      time dependency: fixed mesh
      output: every 500 time steps and at calculation end

   1: name: transient_coords
      directory: postprocessing
      format: EnSight Gold
      options: 
      time dependency: transient coordinates
      output: every 500 time steps and at calculation end


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

 Halo construction with extended neighborhood
 ============================================

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

 Histogram of the number of cells per rank:

    minimum value =               5515
    maximum value =               5859

      1 : [       5515 ;       5583 [ =          2
      2 : [       5583 ;       5652 [ =          8
      3 : [       5652 ;       5721 [ =          1
      4 : [       5721 ;       5790 [ =          0
      5 : [       5790 ;       5859 ] =          1

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

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

    minimum value =               5945
    maximum value =               6293

      1 : [       5945 ;       6014 [ =          4
      2 : [       6014 ;       6084 [ =          4
      3 : [       6084 ;       6153 [ =          1
      4 : [       6153 ;       6223 [ =          0
      5 : [       6223 ;       6293 ] =          3

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

 Histogram of the number of ghost cells per rank:

    minimum value =                380
    maximum value =                655

      1 : [        380 ;        435 [ =          9
      2 : [        435 ;        490 [ =          1
      3 : [        490 ;        545 [ =          0
      4 : [        545 ;        600 [ =          0
      5 : [        600 ;        655 ] =          2

 Histogram of the number of ghost cells
 in the standard neighborhood per rank:

    minimum value =                325
    maximum value =                580

      1 : [        325 ;        376 [ =          1
      2 : [        376 ;        427 [ =          9
      3 : [        427 ;        478 [ =          0
      4 : [        478 ;        529 [ =          0
      5 : [        529 ;        580 ] =          2

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

 Histogram of the number of interior faces per rank:

    minimum value =              15522
    maximum value =              16484

      1 : [      15522 ;      15714 [ =          2
      2 : [      15714 ;      15906 [ =          6
      3 : [      15906 ;      16099 [ =          3
      4 : [      16099 ;      16291 [ =          0
      5 : [      16291 ;      16484 ] =          1

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

 Histogram of the number of boundary faces per rank:

    minimum value =               2387
    maximum value =               2621

      1 : [       2387 ;       2433 [ =          1
      2 : [       2433 ;       2480 [ =          2
      3 : [       2480 ;       2527 [ =          3
      4 : [       2527 ;       2574 [ =          3
      5 : [       2574 ;       2621 ] =          3

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

 Histogram of the number of interior faces per cell:

    minimum value =                  3
    maximum value =                  6

      1 : [          3 ;          4 [ =          4
      2 : [          4 ;          5 [ =       1310
      3 : [          5 ;          6 ] =      66286

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =          9
      2 : [          3 ;          4 ] =          3

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

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

 Renumbering mesh:

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


 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =               5339
    maximum value =               5990

      1 : [       5339 ;       5469 [ =          1
      2 : [       5469 ;       5599 [ =          0
      3 : [       5599 ;       5729 [ =          7
      4 : [       5729 ;       5859 [ =          2
      5 : [       5859 ;       5990 ] =          2

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =                587
    maximum value =               1092

      1 : [        587 ;        688 [ =          8
      2 : [        688 ;        789 [ =          0
      3 : [        789 ;        890 [ =          0
      4 : [        890 ;        991 [ =          1
      5 : [        991 ;       1092 ] =          3

 Mesh coordinates:               minimum    and maximum
                       X : -1.0322404e+00  3.0000000e+00
                       Y : -1.0000063e-01  1.0000000e-01
                       Z : -1.7245361e+00  1.7245361e+00
 Mesh
     Number of cells:          67600
     Number of interior faces: 187640
     Number of boundary faces: 30320
     Number of vertices:       83088

 Groups:
    "back"
       boundary faces:        13520
    "bot"
       boundary faces:          795
    "foil"
       boundary faces:         1190
    "front"
       boundary faces:        13520
    "inlet"
       boundary faces:          100
    "outlet"
       boundary faces:          400
    "top"
       boundary faces:          795

 --- Information on the volumes
       Minimum control volume      =  5.3794804e-07
       Maximum control volume      =  6.5971646e-03
       Total volume for the domain =  2.7653092e+00

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

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

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 0 -->   0 %

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

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

 Computing geometric quantities (0.0227 s)
                                                             
       ALMAX  =    0.14031E+01 (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         0.4000E-02  0.4000E-02
  VelocityY         0.0000E+00  0.0000E+00
  VelocityZ         0.0000E+00  0.0000E+00
  TurbEner          0.6000E-03  0.6000E-03
  Dissip            0.9427E-06  0.9427E-06
  mesh_u            0.0000E+00  0.0000E+00
  mesh_v            0.0000E+00  0.0000E+00
  mesh_w            0.0000E+00  0.0000E+00
 ---------------------------------

  Local Time Step   0.1000E+00  0.1000E+00
 ---------------------------------



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

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


ALL PHASES: COUPLING MODE FOR STRUCTURES ACTIVATED     
              WITH NBSTRU =          1 STRUCTURE(S)    
                                                       
            NEWMARK COEFFICIENTS:                      
              ALPNMK =   0.0000E+00
              BETNMK =   0.2500E+00
              GAMNMK =   0.5000E+00
                                                       
            MONITORING FILES FOR STRUCTURES:           
                 IHISTR =    0 ( 1 : activated)      


ALL PHASES: CODE_ASTER COUPLING MODE NOT ACTIVATED     
              NBASTE =          0


ALL PHASES: IMPLICIT SCHEME FOR COUPING ACTIVATED      
                                                       
            NB OF MAX INNER ITERATIONS :         20
            CONVERGENCE THRESHOLD      :   0.1000E-07

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



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



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


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




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


 INSTANT    0.000000000E+00   ALE INITIALIZATION 
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  Density           0.1000E+04  0.1000E+04
  LamVisc           0.1000E-02  0.1000E-02
  TurbVisc          0.3437E+02  0.3437E+02
 -----------------------------------------

 --- Mesh viscosity (ALE method)
 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  mesh_vi1          0.1000E+01  0.1000E+11
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         100
Smooth wall               5        1190
Rough wall                6           0
Symmetry                  4       28630
Free outlet               3         400
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.30000E+01   0.21108E-17  -0.25080E-02



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100         0.000000000E+00
Smooth wall               5        1190         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.000000000E+00
Free outlet               3         400         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.24537E-03 0.29493E-02
   Friction velocity        uet   :  0.24262E-04 0.29419E-03
   Friction velocity        uk    :  0.13416E-01 0.13416E-01
   Dimensionless distance   yplus :  0.33990E+02 0.35291E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.00000E+00       0   0.00000E+00   0.00000E+00 
c  VelocityX    0.00000E+00       0   0.00000E+00   0.00000E+00 
c  VelocityY    0.00000E+00       0   0.00000E+00   0.00000E+00 
c  VelocityZ    0.00000E+00       0   0.00000E+00   0.00000E+00 
c  TurbEner     0.00000E+00       0   0.00000E+00   0.00000E+00 
c  Dissip       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure     0.00000E+00   0.00000E+00         --         -- 
v  VelocityX    0.40000E-02   0.40000E-02         --         -- 
v  VelocityY    0.00000E+00   0.00000E+00         --         -- 
v  VelocityZ    0.00000E+00   0.00000E+00         --         -- 
v  TurbEner     0.60000E-03   0.60000E-03          0          0 
v  Dissip       0.94269E-06   0.94269E-06          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.34370E+02   0.34370E+02          0          0 
v  CourantNb    0.00000E+00   0.00000E+00          0          0 
v  FourierNb    0.22140E+01   0.11235E+04          0          0 
v  total_pressu 0.10132E+06   0.10132E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.60000E-03   0.60000E-03          0          0 
a  Dissip       0.94269E-06   0.94269E-06          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.71308E-01  0.80000E-01  0.43667E-01  
Courant max  0.00000E+00  0.71308E-01  0.80000E-01  0.43667E-01  
Fourier min  0.22140E+01  0.27584E+01 -0.80000E-01  0.15530E+01  
Fourier max  0.11235E+04 -0.21138E-02 -0.40000E-01  0.39696E-02  
Cou_Fou min  0.22140E+01  0.27584E+01 -0.80000E-01  0.15530E+01  
Cou_Fou max  0.11235E+04 -0.21138E-02 -0.40000E-01  0.39696E-02  
---------------------------------------------------------------
  
  

 TIME FOR ALE INITIALIZATION:           0.10725E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100         0.000000000E+00
Smooth wall               5        1190         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.000000000E+00
Free outlet               3         400         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.24537E-03 0.29493E-02
   Friction velocity        uet   :  0.24262E-04 0.29419E-03
   Friction velocity        uk    :  0.13416E-01 0.13416E-01
   Dimensionless distance   yplus :  0.33990E+02 0.35291E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62826E-02     648   0.67545E-01   0.10000E+01 
c  VelocityX    0.15228E+01    1470   0.90122E-05   0.63348E-07 
c  VelocityY    0.15228E+01    1470   0.90122E-05   0.35301E-18 
c  VelocityZ    0.15228E+01    1470   0.90122E-05   0.55331E-07 
c  TurbEner     0.22348E+00    2120   0.47726E-02   0.23586E-07 
c  Dissip       0.11984E+01    3310   0.16556E-01   0.11703E-02 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.11357E+01   0.31849E+01         --         -- 
v  VelocityX    0.14546E-02   0.47466E-02         --         -- 
v  VelocityY   -0.47063E-08   0.41716E-08         --         -- 
v  VelocityZ   -0.18238E-02   0.18239E-02         --         -- 
v  TurbEner     0.80903E-06   0.59991E-03       2080          0 
v  Dissip       0.81042E-06   0.17467E+00          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.34370E+02   0.34370E+02          0          0 
v  CourantNb    0.00000E+00   0.00000E+00          0          0 
v  FourierNb    0.22140E+01   0.11235E+04          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.67657E-04   0.59991E-03       2080          0 
a  Dissip       0.81042E-06   0.17467E+00          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.00000E+00  0.71308E-01  0.80000E-01  0.43667E-01  
Courant max  0.00000E+00  0.71308E-01  0.80000E-01  0.43667E-01  
Fourier min  0.22140E+01  0.27584E+01 -0.80000E-01  0.15530E+01  
Fourier max  0.11235E+04 -0.21138E-02 -0.40000E-01  0.39696E-02  
Cou_Fou min  0.22140E+01  0.27584E+01 -0.80000E-01  0.15530E+01  
Cou_Fou max  0.11235E+04 -0.21138E-02 -0.40000E-01  0.39696E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                1:        0.20537E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.390693947E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.183926241E-22
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45063E-02 0.00000E+00
   Friction velocity        uet   :  0.40528E-04 0.25559E-02
   Friction velocity        uk    :  0.51130E-03 0.45052E-02
   Dimensionless distance   yplus :  0.12954E+01 0.11414E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1180
   Nb of faces within the viscous sub-layer     :         10
   Total number of wall faces                   :       1190
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          2
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            


   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.23602E-02     537   0.48728E-01   0.99766E+00 
c  VelocityX    0.15184E+01     832   0.31921E-04   0.67809E-10 
c  VelocityY    0.15184E+01     832   0.31921E-04   0.79707E-14 
c  VelocityZ    0.15184E+01     832   0.31921E-04   0.87799E-10 
c  TurbEner     0.21901E+00    1012   0.26173E-02   0.32998E-07 
c  Dissip       0.25666E-01     795   0.51238E-04   0.11170E-02 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.41445E-01   0.81023E-01         --         -- 
v  VelocityX    0.13547E-02   0.47148E-02         --         -- 
v  VelocityY   -0.43600E-06   0.43603E-06         --         -- 
v  VelocityZ   -0.18508E-02   0.18509E-02         --         -- 
v  TurbEner     0.10459E-08   0.59981E-03       1210          0 
v  Dissip       0.72641E-06   0.37506E-02        180          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.44633E-09   0.34369E+02          0          0 
v  CourantNb    0.73618E-03   0.12155E+00          0          0 
v  FourierNb    0.51808E-02   0.34945E+03          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.34250E-05   0.59981E-03       1210          0 
a  Dissip      -0.72410E-03   0.37506E-02        180          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73618E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.12155E+00  0.12947E-01  0.86638E-16  0.22371E-01  
Fourier min  0.51808E-02  0.51273E+00  0.80000E-01 -0.54009E-01  
Fourier max  0.34945E+03  0.11007E+01 -0.80000E-01 -0.85638E+00  
Cou_Fou min  0.20538E-01 -0.17772E+00 -0.80000E-01  0.12228E-01  
Cou_Fou max  0.34954E+03  0.11007E+01 -0.80000E-01 -0.85638E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                2:        0.11226E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.382066161E-22
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.15307E-02
   Friction velocity        uet   :  0.21464E-03 0.76058E-02
   Friction velocity        uk    :  0.17976E-03 0.10137E-02
   Dimensionless distance   yplus :  0.45542E+00 0.25681E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1180
   Total number of wall faces                   :       1190
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          3
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            


   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.73932E-03     521   0.20846E-01   0.44462E+00 
c  VelocityX    0.15139E+01     897   0.31379E-04   0.31378E-10 
c  VelocityY    0.15139E+01     897   0.31379E-04   0.26148E-14 
c  VelocityZ    0.15139E+01     897   0.31379E-04   0.27042E-10 
c  TurbEner     0.21666E+00    1012   0.14801E-02   0.47737E-08 
c  Dissip       0.12312E-01     840   0.44332E-04   0.16713E-05 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.26551E-01   0.52062E-01         --         -- 
v  VelocityX    0.13641E-02   0.47058E-02         --         -- 
v  VelocityY   -0.71909E-06   0.71911E-06         --         -- 
v  VelocityZ   -0.18250E-02   0.18251E-02         --         -- 
v  TurbEner     0.55390E-10   0.59972E-03       1230          0 
v  Dissip       0.14721E-07   0.12114E-02       1360          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.36473E-12   0.34369E+02          0          0 
v  CourantNb    0.73609E-03   0.12251E+00          0          0 
v  FourierNb    0.39241E-02   0.34384E+03          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.21365E-06   0.59972E-03       1230          0 
a  Dissip      -0.89179E-05   0.12114E-02       1360          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73609E-03  0.27286E+01  0.80000E-01 -0.25076E-02  
Courant max  0.12251E+00  0.12947E-01  0.86638E-16  0.22371E-01  
Fourier min  0.39241E-02  0.52033E+00  0.80000E-01  0.16777E+00  
Fourier max  0.34384E+03  0.11007E+01  0.80000E-01 -0.85638E+00  
Cou_Fou min  0.20004E-01 -0.17772E+00  0.80000E-01  0.12228E-01  
Cou_Fou max  0.34393E+03  0.11007E+01  0.80000E-01 -0.85638E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                3:        0.11404E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.677626358E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.720495313E-22
Free outlet               3         400         0.275925776E+01
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   :  0.10691E-02 0.26411E-01
   Friction velocity        uk    :  0.50554E-04 0.35359E-03
   Dimensionless distance   yplus :  0.13084E+00 0.89583E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1190
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.45493E-03     520   0.42890E-01   0.36766E+00 
c  VelocityX    0.15110E+01     746   0.18758E-04   0.20906E-10 
c  VelocityY    0.15110E+01     746   0.18758E-04   0.17538E-14 
c  VelocityZ    0.15110E+01     746   0.18758E-04   0.14902E-10 
c  TurbEner     0.21502E+00    1013   0.46181E-03   0.18821E-08 
c  Dissip       0.79959E-02     861   0.47751E-04   0.87748E-07 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.10888E-01   0.37501E-01         --         -- 
v  VelocityX    0.12313E-02   0.47071E-02         --         -- 
v  VelocityY   -0.89343E-06   0.89345E-06         --         -- 
v  VelocityZ   -0.18980E-02   0.18980E-02         --         -- 
v  TurbEner     0.53516E-11   0.59962E-03        550          0 
v  Dissip       0.78528E-10   0.69675E-03       1130          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.15083E-12   0.34368E+02          0          0 
v  CourantNb    0.73605E-03   0.12274E+00          0          0 
v  FourierNb    0.32538E-02   0.33961E+03          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.27800E-07   0.59962E-03        550          0 
a  Dissip      -0.25595E-05   0.69675E-03       1130          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73605E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.12274E+00  0.12947E-01  0.86638E-16  0.22371E-01  
Fourier min  0.32538E-02  0.52120E+00  0.80000E-01  0.18084E+00  
Fourier max  0.33961E+03  0.11103E+01 -0.80000E-01 -0.92614E+00  
Cou_Fou min  0.19616E-01 -0.17772E+00  0.80000E-01  0.12228E-01  
Cou_Fou max  0.33970E+03  0.11103E+01 -0.80000E-01 -0.92614E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                4:        0.10480E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.189766057E-21
Free outlet               3         400         0.275925776E+01
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   :  0.23392E-02 0.24365E+00
   Friction velocity        uk    :  0.54719E-05 0.13174E-03
   Dimensionless distance   yplus :  0.14175E-01 0.33377E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1190
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.44348E-03     431   0.30480E-01   0.49883E+00 
c  VelocityX    0.15090E+01     665   0.68369E-05   0.13195E-10 
c  VelocityY    0.15090E+01     665   0.68369E-05   0.36281E-15 
c  VelocityZ    0.15090E+01     665   0.68369E-05   0.47184E-11 
c  TurbEner     0.21379E+00    1013   0.32920E-03   0.10285E-08 
c  Dissip       0.58823E-02     875   0.46081E-04   0.15282E-07 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.93991E-02   0.23976E-01         --         -- 
v  VelocityX    0.12076E-02   0.47081E-02         --         -- 
v  VelocityY   -0.99852E-06   0.99853E-06         --         -- 
v  VelocityZ   -0.19648E-02   0.19648E-02         --         -- 
v  TurbEner     0.83698E-13   0.59953E-03       1150          0 
v  Dissip       0.90557E-11   0.47794E-03        650          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.30643E-13   0.34368E+02          0          0 
v  CourantNb    0.73604E-03   0.12267E+00          0          0 
v  FourierNb    0.29077E-02   0.33568E+03          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.52983E-08   0.59953E-03       1150          0 
a  Dissip      -0.34748E-06   0.47794E-03        650          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73604E-03  0.27286E+01  0.10461E-16 -0.25076E-02  
Courant max  0.12267E+00  0.12947E-01  0.86638E-16  0.22371E-01  
Fourier min  0.29077E-02  0.52120E+00  0.80000E-01  0.18084E+00  
Fourier max  0.33568E+03  0.11103E+01  0.80000E-01 -0.92614E+00  
Cou_Fou min  0.19331E-01 -0.17772E+00 -0.80000E-01  0.12228E-01  
Cou_Fou max  0.33577E+03  0.11103E+01  0.80000E-01 -0.92614E+00  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                5:        0.96595E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.912742111E-22
Free outlet               3         400         0.275925776E+01
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   :  0.39120E-02 0.48604E+00
   Friction velocity        uk    :  0.19115E-05 0.64170E-04
   Dimensionless distance   yplus :  0.50196E-02 0.16879E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1190
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.21448E-03     431   0.62591E-02   0.30414E+00 
c  VelocityX    0.15075E+01     661   0.38833E-05   0.11408E-10 
c  VelocityY    0.15075E+01     661   0.38833E-05   0.68205E-16 
c  VelocityZ    0.15075E+01     661   0.38833E-05   0.31047E-11 
c  TurbEner     0.21281E+00    1013   0.24991E-03   0.65413E-09 
c  Dissip       0.46497E-02     885   0.50061E-04   0.45101E-08 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.83229E-02   0.23094E-01         --         -- 
v  VelocityX    0.12046E-02   0.47091E-02         --         -- 
v  VelocityY   -0.10532E-05   0.10532E-05         --         -- 
v  VelocityZ   -0.20118E-02   0.20118E-02         --         -- 
v  TurbEner     0.56871E-14   0.59944E-03       1245          0 
v  Dissip       0.29089E-12   0.36508E-03       1075          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.56815E-15   0.34368E+02          0          0 
v  CourantNb    0.73604E-03   0.12219E+00          0          0 
v  FourierNb    0.27307E-02   0.33148E+03          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.22957E-08   0.59944E-03       1245          0 
a  Dissip      -0.39969E-07   0.36508E-03       1075          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73604E-03  0.27286E+01  0.10461E-16 -0.25076E-02  
Courant max  0.12219E+00  0.12947E-01  0.86638E-16  0.22371E-01  
Fourier min  0.27307E-02  0.52120E+00  0.80000E-01  0.18084E+00  
Fourier max  0.33148E+03  0.11164E+01  0.40000E-01  0.10030E+01  
Cou_Fou min  0.19121E-01 -0.17772E+00  0.80000E-01  0.12228E-01  
Cou_Fou max  0.33157E+03  0.11164E+01  0.40000E-01  0.10030E+01  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                6:        0.95950E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.537307931E-22
Free outlet               3         400         0.275925776E+01
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   :  0.57149E-02 0.21289E+01
   Friction velocity        uk    :  0.75449E-06 0.55084E-04
   Dimensionless distance   yplus :  0.19524E-02 0.14489E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1190
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.19220E-03     465   0.10698E-01   0.33721E+00 
c  VelocityX    0.15063E+01     651   0.30867E-05   0.10099E-10 
c  VelocityY    0.15063E+01     651   0.30867E-05   0.49447E-16 
c  VelocityZ    0.15063E+01     651   0.30867E-05   0.11963E-11 
c  TurbEner     0.21200E+00    1013   0.19606E-03   0.45469E-09 
c  Dissip       0.38498E-02     892   0.53537E-04   0.17691E-08 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.70484E-02   0.21144E-01         --         -- 
v  VelocityX    0.11917E-02   0.47103E-02         --         -- 
v  VelocityY   -0.10797E-05   0.10797E-05         --         -- 
v  VelocityZ   -0.20369E-02   0.20369E-02         --         -- 
v  TurbEner     0.83831E-15   0.59934E-03        755          0 
v  Dissip       0.48665E-13   0.29531E-03        510          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.33926E-16   0.34367E+02          0          0 
v  CourantNb    0.73605E-03   0.12172E+00          0          0 
v  FourierNb    0.26307E-02   0.32989E+03          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.19083E-09   0.59934E-03        755          0 
a  Dissip      -0.48556E-08   0.29531E-03        510          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73605E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.12172E+00  0.12947E-01  0.86638E-16  0.22371E-01  
Fourier min  0.26307E-02  0.52120E+00  0.80000E-01  0.18084E+00  
Fourier max  0.32989E+03  0.11210E+01  0.80000E-01 -0.10027E+01  
Cou_Fou min  0.18966E-01 -0.17772E+00 -0.80000E-01  0.12228E-01  
Cou_Fou max  0.32998E+03  0.11210E+01  0.80000E-01 -0.10027E+01  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                7:        0.98219E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.177035634E-21
Free outlet               3         400         0.275925776E+01
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   :  0.78618E-02 0.30122E+02
   Friction velocity        uk    :  0.49857E-07 0.47822E-04
   Dimensionless distance   yplus :  0.12632E-03 0.12579E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1190
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.11407E-03     430   0.10199E-01   0.23417E+00 
c  VelocityX    0.15053E+01     642   0.20947E-05   0.93723E-11 
c  VelocityY    0.15053E+01     642   0.20947E-05   0.22434E-16 
c  VelocityZ    0.15053E+01     642   0.20947E-05   0.79642E-12 
c  TurbEner     0.21132E+00    1012   0.15807E-03   0.33523E-09 
c  Dissip       0.32911E-02     897   0.56593E-04   0.82875E-09 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.65142E-02   0.20622E-01         --         -- 
v  VelocityX    0.11446E-02   0.47114E-02         --         -- 
v  VelocityY   -0.11805E-05   0.11805E-05         --         -- 
v  VelocityZ   -0.20527E-02   0.20527E-02         --         -- 
v  TurbEner     0.26561E-16   0.59925E-03       1610          0 
v  Dissip       0.99273E-14   0.24764E-03        300          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.30282E-16   0.34367E+02          0          0 
v  CourantNb    0.73606E-03   0.12105E+00          0          0 
v  FourierNb    0.25467E-02   0.32704E+03          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.11418E-09   0.59925E-03       1610          0 
a  Dissip      -0.19482E-09   0.24764E-03        300          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73606E-03  0.27286E+01  0.80000E-01 -0.25076E-02  
Courant max  0.12105E+00  0.12947E-01  0.86638E-16  0.22371E-01  
Fourier min  0.25467E-02  0.52230E+00  0.80000E-01  0.19718E+00  
Fourier max  0.32704E+03  0.11210E+01  0.80000E-01 -0.10027E+01  
Cou_Fou min  0.18856E-01 -0.17772E+00 -0.80000E-01  0.12228E-01  
Cou_Fou max  0.32713E+03  0.11210E+01  0.80000E-01 -0.10027E+01  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                8:        0.96588E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.412338225E-22
Free outlet               3         400         0.275925776E+01
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   :  0.10272E-01 0.28801E+02
   Friction velocity        uk    :  0.62123E-07 0.41785E-04
   Dimensionless distance   yplus :  0.15769E-03 0.10991E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1190
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.87648E-04     411   0.48234E-02   0.20605E+00 
c  VelocityX    0.15044E+01     648   0.15504E-05   0.88194E-11 
c  VelocityY    0.15044E+01     648   0.15504E-05   0.11400E-16 
c  VelocityZ    0.15044E+01     648   0.15504E-05   0.57055E-12 
c  TurbEner     0.21072E+00    1012   0.13042E-03   0.25782E-09 
c  Dissip       0.28794E-02     902   0.59328E-04   0.43847E-09 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.62823E-02   0.19972E-01         --         -- 
v  VelocityX    0.11064E-02   0.47124E-02         --         -- 
v  VelocityY   -0.13721E-05   0.13721E-05         --         -- 
v  VelocityZ   -0.20631E-02   0.20632E-02         --         -- 
v  TurbEner     0.97660E-17   0.59915E-03       1126          0 
v  Dissip       0.72591E-14   0.21349E-03        235          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.21761E-18   0.34366E+02          0          0 
v  CourantNb    0.73607E-03   0.12036E+00          0          0 
v  FourierNb    0.24796E-02   0.32395E+03          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.51266E-10   0.59915E-03       1126          0 
a  Dissip      -0.50080E-10   0.21349E-03        235          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73607E-03  0.27286E+01  0.80000E-01 -0.25076E-02  
Courant max  0.12036E+00  0.12947E-01  0.86638E-16  0.22371E-01  
Fourier min  0.24796E-02  0.52230E+00  0.80000E-01  0.19718E+00  
Fourier max  0.32395E+03  0.11210E+01  0.80000E-01 -0.10027E+01  
Cou_Fou min  0.18779E-01 -0.17772E+00 -0.80000E-01  0.12228E-01  
Cou_Fou max  0.32404E+03  0.11210E+01  0.80000E-01 -0.10027E+01  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP                9:        0.94967E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.123287878E-21
Free outlet               3         400         0.275925776E+01
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   :  0.12880E-01 0.26908E+03
   Friction velocity        uk    :  0.65714E-08 0.36691E-04
   Dimensionless distance   yplus :  0.16671E-04 0.96508E-01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1190
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62325E-04     374   0.28577E-02   0.16389E+00 
c  VelocityX    0.15037E+01     643   0.13369E-05   0.83832E-11 
c  VelocityY    0.15037E+01     643   0.13369E-05   0.81613E-17 
c  VelocityZ    0.15037E+01     643   0.13369E-05   0.47897E-12 
c  TurbEner     0.21020E+00    1012   0.10975E-03   0.20471E-09 
c  Dissip       0.25636E-02     905   0.61799E-04   0.25345E-09 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.61586E-02   0.19373E-01         --         -- 
v  VelocityX    0.10744E-02   0.47132E-02         --         -- 
v  VelocityY   -0.15557E-05   0.15557E-05         --         -- 
v  VelocityZ   -0.20700E-02   0.20700E-02         --         -- 
v  TurbEner     0.19951E-17   0.59906E-03       1285          0 
v  Dissip       0.12187E-16   0.18770E-03        620          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.78692E-19   0.34366E+02          0          0 
v  CourantNb    0.73607E-03   0.11967E+00          0          0 
v  FourierNb    0.24314E-02   0.32251E+03          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.12615E-09   0.59906E-03       1285          0 
a  Dissip      -0.41065E-11   0.18770E-03        620          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73607E-03  0.27286E+01  0.80000E-01 -0.25076E-02  
Courant max  0.11967E+00  0.12947E-01  0.86638E-16  0.22371E-01  
Fourier min  0.24314E-02  0.52230E+00  0.80000E-01  0.19718E+00  
Fourier max  0.32251E+03  0.11329E+01 -0.80000E-01 -0.10886E+01  
Cou_Fou min  0.18729E-01 -0.17772E+00 -0.80000E-01  0.12228E-01  
Cou_Fou max  0.32260E+03  0.11329E+01 -0.80000E-01 -0.10886E+01  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               10:        0.93257E+00

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.451124431E-22
Free outlet               3         400         0.275925776E+01
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   :  0.15625E-01 0.34116E+02
   Friction velocity        uk    :  0.47534E-07 0.32359E-04
   Dimensionless distance   yplus :  0.12043E-03 0.85115E-01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1190
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.48169E-04     374   0.35003E-02   0.13942E+00 
c  VelocityX    0.15030E+01     634   0.12296E-05   0.80234E-11 
c  VelocityY    0.15030E+01     634   0.12296E-05   0.61204E-17 
c  VelocityZ    0.15030E+01     634   0.12296E-05   0.42370E-12 
c  TurbEner     0.20973E+00    1012   0.93914E-04   0.16665E-09 
c  Dissip       0.23136E-02     908   0.64040E-04   0.15668E-09 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.60489E-02   0.18937E-01         --         -- 
v  VelocityX    0.10473E-02   0.47139E-02         --         -- 
v  VelocityY   -0.17178E-05   0.17178E-05         --         -- 
v  VelocityZ   -0.20746E-02   0.20746E-02         --         -- 
v  TurbEner     0.12437E-18   0.59897E-03        990          0 
v  Dissip       0.18815E-16   0.16689E-03        410          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.19762E-20   0.34365E+02          0          0 
v  CourantNb    0.73608E-03   0.11899E+00          0          0 
v  FourierNb    0.23954E-02   0.31965E+03          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner    -0.29476E-10   0.59897E-03        990          0 
a  Dissip      -0.10081E-12   0.16689E-03        410          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73608E-03  0.27286E+01  0.80000E-01 -0.25076E-02  
Courant max  0.11899E+00  0.12947E-01  0.86638E-16  0.22371E-01  
Fourier min  0.23954E-02  0.52230E+00  0.80000E-01  0.19718E+00  
Fourier max  0.31965E+03  0.11282E+01  0.40000E-01  0.10889E+01  
Cou_Fou min  0.18702E-01 -0.17772E+00 -0.80000E-01  0.12228E-01  
Cou_Fou max  0.31974E+03  0.11282E+01  0.40000E-01  0.10889E+01  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP               11:        0.92733E+00

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


 INSTANT    0.498100000E+03   TIME STEP NUMBER            4981
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.130866590E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.547474017E-22
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20193E-02
   Friction velocity        uet   :  0.44417E-04 0.17088E-02
   Friction velocity        uk    :  0.84768E-03 0.17036E-02
   Dimensionless distance   yplus :  0.21585E+01 0.43161E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.16345E-05     188   0.82093E-04   0.61333E-02 
c  VelocityX    0.14910E+01      44   0.10768E-05   0.32988E-13 
c  VelocityY    0.14910E+01      44   0.10768E-05   0.12474E-16 
c  VelocityZ    0.14910E+01      44   0.10768E-05   0.53299E-14 
c  TurbEner     0.27797E-01     182   0.10264E-07   0.41838E-14 
c  Dissip       0.51175E-04     150   0.16722E-07   0.66227E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.51118E-02   0.23474E-01         --         -- 
v  VelocityX    0.94715E-03   0.42151E-02         --         -- 
v  VelocityY   -0.92332E-05   0.92332E-05         --         -- 
v  VelocityZ   -0.21854E-02   0.21854E-02         --         -- 
v  TurbEner     0.27431E-06   0.89248E-04          0          0 
v  Dissip       0.51022E-09   0.34096E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.10037E-02   0.44125E+01          0          0 
v  CourantNb    0.73502E-03   0.11341E+00          0          0 
v  FourierNb    0.11563E-02   0.33480E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27431E-06   0.89248E-04          0          0 
a  Dissip       0.51022E-09   0.34096E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11341E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11563E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33480E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35199E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33481E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4981:        0.32244E+00

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


 INSTANT    0.498200000E+03   TIME STEP NUMBER            4982
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.430928012E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.108880880E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20190E-02
   Friction velocity        uet   :  0.44418E-04 0.17087E-02
   Friction velocity        uk    :  0.84763E-03 0.17031E-02
   Dimensionless distance   yplus :  0.21583E+01 0.43148E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.15924E-05     193   0.80755E-04   0.59753E-02 
c  VelocityX    0.14910E+01      44   0.12596E-05   0.31642E-13 
c  VelocityY    0.14910E+01      44   0.12596E-05   0.11694E-16 
c  VelocityZ    0.14910E+01      44   0.12596E-05   0.51951E-14 
c  TurbEner     0.27788E-01     182   0.10249E-07   0.41803E-14 
c  Dissip       0.51152E-04     150   0.16706E-07   0.63347E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.51095E-02   0.23466E-01         --         -- 
v  VelocityX    0.94708E-03   0.42152E-02         --         -- 
v  VelocityY   -0.92363E-05   0.92362E-05         --         -- 
v  VelocityZ   -0.21853E-02   0.21852E-02         --         -- 
v  TurbEner     0.27428E-06   0.89219E-04          0          0 
v  Dissip       0.51014E-09   0.34067E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.10033E-02   0.44116E+01          0          0 
v  CourantNb    0.73502E-03   0.11340E+00          0          0 
v  FourierNb    0.11561E-02   0.33473E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27428E-06   0.89219E-04          0          0 
a  Dissip       0.51014E-09   0.34067E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11340E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11561E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33473E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35197E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33473E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4982:        0.32233E+00

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


 INSTANT    0.498300000E+03   TIME STEP NUMBER            4983
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.762753169E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.110383376E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20186E-02
   Friction velocity        uet   :  0.44419E-04 0.17086E-02
   Friction velocity        uk    :  0.84758E-03 0.17026E-02
   Dimensionless distance   yplus :  0.21582E+01 0.43135E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.15571E-05     187   0.77675E-04   0.58419E-02 
c  VelocityX    0.14910E+01      44   0.13566E-05   0.30414E-13 
c  VelocityY    0.14910E+01      44   0.13566E-05   0.10999E-16 
c  VelocityZ    0.14910E+01      44   0.13566E-05   0.51066E-14 
c  TurbEner     0.27779E-01     182   0.10235E-07   0.41768E-14 
c  Dissip       0.51129E-04     150   0.16689E-07   0.60836E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.51086E-02   0.23459E-01         --         -- 
v  VelocityX    0.94701E-03   0.42152E-02         --         -- 
v  VelocityY   -0.92383E-05   0.92383E-05         --         -- 
v  VelocityZ   -0.21851E-02   0.21851E-02         --         -- 
v  TurbEner     0.27425E-06   0.89189E-04          0          0 
v  Dissip       0.51006E-09   0.34038E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.10028E-02   0.44106E+01          0          0 
v  CourantNb    0.73502E-03   0.11339E+00          0          0 
v  FourierNb    0.11560E-02   0.33465E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27425E-06   0.89189E-04          0          0 
a  Dissip       0.51006E-09   0.34038E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11339E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11560E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33465E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35196E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33466E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4983:        0.32127E+00

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


 INSTANT    0.498400000E+03   TIME STEP NUMBER            4984
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.369094607E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.105917893E-22
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20182E-02
   Friction velocity        uet   :  0.44420E-04 0.17085E-02
   Friction velocity        uk    :  0.84753E-03 0.17021E-02
   Dimensionless distance   yplus :  0.21581E+01 0.43122E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.15293E-05     194   0.82617E-04   0.57384E-02 
c  VelocityX    0.14910E+01      44   0.12633E-05   0.29287E-13 
c  VelocityY    0.14910E+01      44   0.12633E-05   0.10521E-16 
c  VelocityZ    0.14910E+01      44   0.12633E-05   0.49930E-14 
c  TurbEner     0.27769E-01     182   0.10221E-07   0.41733E-14 
c  Dissip       0.51106E-04     150   0.16674E-07   0.58637E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.51052E-02   0.23452E-01         --         -- 
v  VelocityX    0.94695E-03   0.42152E-02         --         -- 
v  VelocityY   -0.92394E-05   0.92394E-05         --         -- 
v  VelocityZ   -0.21850E-02   0.21850E-02         --         -- 
v  TurbEner     0.27422E-06   0.89160E-04          0          0 
v  Dissip       0.50998E-09   0.34009E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.10024E-02   0.44096E+01          0          0 
v  CourantNb    0.73502E-03   0.11338E+00          0          0 
v  FourierNb    0.11558E-02   0.33458E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27422E-06   0.89160E-04          0          0 
a  Dissip       0.50998E-09   0.34009E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11338E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11558E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33458E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35194E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33458E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4984:        0.32431E+00

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


 INSTANT    0.498500000E+03   TIME STEP NUMBER            4985
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.757247455E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.713378657E-22
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20178E-02
   Friction velocity        uet   :  0.44421E-04 0.17084E-02
   Friction velocity        uk    :  0.84748E-03 0.17016E-02
   Dimensionless distance   yplus :  0.21580E+01 0.43109E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.15889E-05     192   0.10270E-03   0.59625E-02 
c  VelocityX    0.14910E+01      44   0.12639E-05   0.28291E-13 
c  VelocityY    0.14910E+01      44   0.12639E-05   0.98242E-17 
c  VelocityZ    0.14910E+01      44   0.12639E-05   0.48982E-14 
c  TurbEner     0.27760E-01     182   0.10206E-07   0.41698E-14 
c  Dissip       0.51083E-04     150   0.16656E-07   0.56706E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.51055E-02   0.23444E-01         --         -- 
v  VelocityX    0.94688E-03   0.42153E-02         --         -- 
v  VelocityY   -0.92399E-05   0.92399E-05         --         -- 
v  VelocityZ   -0.21849E-02   0.21849E-02         --         -- 
v  TurbEner     0.27420E-06   0.89130E-04          0          0 
v  Dissip       0.50990E-09   0.33981E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.10020E-02   0.44087E+01          0          0 
v  CourantNb    0.73502E-03   0.11337E+00          0          0 
v  FourierNb    0.11557E-02   0.33450E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27420E-06   0.89130E-04          0          0 
a  Dissip       0.50990E-09   0.33981E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11337E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11557E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33450E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35193E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33451E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4985:        0.32134E+00

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


 INSTANT    0.498600000E+03   TIME STEP NUMBER            4986
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.858679650E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.182382015E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20174E-02
   Friction velocity        uet   :  0.44422E-04 0.17084E-02
   Friction velocity        uk    :  0.84742E-03 0.17011E-02
   Dimensionless distance   yplus :  0.21578E+01 0.43096E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.14698E-05     174   0.80078E-04   0.55162E-02 
c  VelocityX    0.14910E+01      44   0.11617E-05   0.27353E-13 
c  VelocityY    0.14910E+01      44   0.11617E-05   0.96999E-17 
c  VelocityZ    0.14910E+01      44   0.11617E-05   0.47973E-14 
c  TurbEner     0.27751E-01     182   0.10192E-07   0.41663E-14 
c  Dissip       0.51060E-04     150   0.16641E-07   0.55000E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.51015E-02   0.23437E-01         --         -- 
v  VelocityX    0.94681E-03   0.42153E-02         --         -- 
v  VelocityY   -0.92096E-05   0.92096E-05         --         -- 
v  VelocityZ   -0.21848E-02   0.21848E-02         --         -- 
v  TurbEner     0.27417E-06   0.89101E-04          0          0 
v  Dissip       0.50981E-09   0.33952E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.10016E-02   0.44077E+01          0          0 
v  CourantNb    0.73502E-03   0.11336E+00          0          0 
v  FourierNb    0.11555E-02   0.33443E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27417E-06   0.89101E-04          0          0 
a  Dissip       0.50981E-09   0.33952E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11336E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11555E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33443E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35191E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33444E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4986:        0.31523E+00

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


 INSTANT    0.498700000E+03   TIME STEP NUMBER            4987
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.368035816E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.162201717E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20169E-02
   Friction velocity        uet   :  0.44423E-04 0.17084E-02
   Friction velocity        uk    :  0.84737E-03 0.17005E-02
   Dimensionless distance   yplus :  0.21577E+01 0.43083E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.14127E-05     190   0.10628E-03   0.53026E-02 
c  VelocityX    0.14910E+01      44   0.14332E-05   0.26505E-13 
c  VelocityY    0.14910E+01      44   0.14332E-05   0.89919E-17 
c  VelocityZ    0.14910E+01      44   0.14332E-05   0.47233E-14 
c  TurbEner     0.27742E-01     182   0.10177E-07   0.41628E-14 
c  Dissip       0.51037E-04     150   0.16623E-07   0.53490E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.51014E-02   0.23430E-01         --         -- 
v  VelocityX    0.94675E-03   0.42154E-02         --         -- 
v  VelocityY   -0.91831E-05   0.91830E-05         --         -- 
v  VelocityZ   -0.21847E-02   0.21846E-02         --         -- 
v  TurbEner     0.27414E-06   0.89071E-04          0          0 
v  Dissip       0.50973E-09   0.33923E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.10011E-02   0.44068E+01          0          0 
v  CourantNb    0.73502E-03   0.11336E+00          0          0 
v  FourierNb    0.11554E-02   0.33436E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27414E-06   0.89071E-04          0          0 
a  Dissip       0.50973E-09   0.33923E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11336E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11554E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33436E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35190E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33436E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4987:        0.32305E+00

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


 INSTANT    0.498800000E+03   TIME STEP NUMBER            4988
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.606263832E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.105641627E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20164E-02
   Friction velocity        uet   :  0.44425E-04 0.17084E-02
   Friction velocity        uk    :  0.84731E-03 0.17000E-02
   Dimensionless distance   yplus :  0.21575E+01 0.43070E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.15373E-05     192   0.11642E-03   0.57678E-02 
c  VelocityX    0.14910E+01      44   0.14780E-05   0.25761E-13 
c  VelocityY    0.14910E+01      44   0.14780E-05   0.88393E-17 
c  VelocityZ    0.14910E+01      44   0.14780E-05   0.46836E-14 
c  TurbEner     0.27732E-01     182   0.10163E-07   0.41593E-14 
c  Dissip       0.51014E-04     150   0.16609E-07   0.52152E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.50987E-02   0.23423E-01         --         -- 
v  VelocityX    0.94668E-03   0.42154E-02         --         -- 
v  VelocityY   -0.91613E-05   0.91612E-05         --         -- 
v  VelocityZ   -0.21845E-02   0.21845E-02         --         -- 
v  TurbEner     0.27411E-06   0.89042E-04          0          0 
v  Dissip       0.50965E-09   0.33895E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.10007E-02   0.44058E+01          0          0 
v  CourantNb    0.73502E-03   0.11335E+00          0          0 
v  FourierNb    0.11552E-02   0.33428E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27411E-06   0.89042E-04          0          0 
a  Dissip       0.50965E-09   0.33895E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01  0.80000E-01 -0.25076E-02  
Courant max  0.11335E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11552E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33428E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35189E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33429E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4988:        0.32396E+00

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


 INSTANT    0.498900000E+03   TIME STEP NUMBER            4989
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.876043826E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.125337249E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20159E-02
   Friction velocity        uet   :  0.44426E-04 0.17084E-02
   Friction velocity        uk    :  0.84724E-03 0.16995E-02
   Dimensionless distance   yplus :  0.21574E+01 0.43057E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.14604E-05     175   0.90835E-04   0.54786E-02 
c  VelocityX    0.14910E+01      44   0.11067E-05   0.25061E-13 
c  VelocityY    0.14910E+01      44   0.11067E-05   0.82228E-17 
c  VelocityZ    0.14910E+01      44   0.11067E-05   0.45809E-14 
c  TurbEner     0.27723E-01     182   0.10149E-07   0.41558E-14 
c  Dissip       0.50991E-04     150   0.16591E-07   0.50962E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.50980E-02   0.23415E-01         --         -- 
v  VelocityX    0.94661E-03   0.42154E-02         --         -- 
v  VelocityY   -0.91442E-05   0.91442E-05         --         -- 
v  VelocityZ   -0.21844E-02   0.21844E-02         --         -- 
v  TurbEner     0.27409E-06   0.89013E-04          0          0 
v  Dissip       0.50957E-09   0.33866E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.10003E-02   0.44048E+01          0          0 
v  CourantNb    0.73502E-03   0.11334E+00          0          0 
v  FourierNb    0.11551E-02   0.33421E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27409E-06   0.89013E-04          0          0 
a  Dissip       0.50957E-09   0.33866E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11334E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11551E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33421E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35187E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33421E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4989:        0.31454E+00

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


 INSTANT    0.499000000E+03   TIME STEP NUMBER            4990
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190        -0.675508775E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.506486569E-22
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20154E-02
   Friction velocity        uet   :  0.44427E-04 0.17085E-02
   Friction velocity        uk    :  0.84717E-03 0.16990E-02
   Dimensionless distance   yplus :  0.21572E+01 0.43044E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13598E-05     203   0.94297E-04   0.51014E-02 
c  VelocityX    0.14910E+01      44   0.14531E-05   0.24410E-13 
c  VelocityY    0.14910E+01      44   0.14531E-05   0.79820E-17 
c  VelocityZ    0.14910E+01      44   0.14531E-05   0.44901E-14 
c  TurbEner     0.27714E-01     182   0.10134E-07   0.41523E-14 
c  Dissip       0.50968E-04     150   0.16576E-07   0.49903E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.50949E-02   0.23408E-01         --         -- 
v  VelocityX    0.94655E-03   0.42155E-02         --         -- 
v  VelocityY   -0.91281E-05   0.91280E-05         --         -- 
v  VelocityZ   -0.21843E-02   0.21843E-02         --         -- 
v  TurbEner     0.27406E-06   0.88983E-04          0          0 
v  Dissip       0.50949E-09   0.33837E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.99987E-03   0.44039E+01          0          0 
v  CourantNb    0.73502E-03   0.11333E+00          0          0 
v  FourierNb    0.11549E-02   0.33413E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27406E-06   0.88983E-04          0          0 
a  Dissip       0.50949E-09   0.33837E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11333E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11549E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33413E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35186E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33414E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4990:        0.32724E+00

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


 INSTANT    0.499100000E+03   TIME STEP NUMBER            4991
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.292226367E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.227167710E-22
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20149E-02
   Friction velocity        uet   :  0.44428E-04 0.17085E-02
   Friction velocity        uk    :  0.84710E-03 0.16985E-02
   Dimensionless distance   yplus :  0.21570E+01 0.43031E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.14283E-05     195   0.11874E-03   0.53567E-02 
c  VelocityX    0.14910E+01      44   0.14827E-05   0.23826E-13 
c  VelocityY    0.14910E+01      44   0.14827E-05   0.77892E-17 
c  VelocityZ    0.14910E+01      44   0.14827E-05   0.44789E-14 
c  TurbEner     0.27704E-01     182   0.10120E-07   0.41489E-14 
c  Dissip       0.50945E-04     150   0.16558E-07   0.48956E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.50946E-02   0.23401E-01         --         -- 
v  VelocityX    0.94648E-03   0.42155E-02         --         -- 
v  VelocityY   -0.91142E-05   0.91142E-05         --         -- 
v  VelocityZ   -0.21842E-02   0.21842E-02         --         -- 
v  TurbEner     0.27403E-06   0.88954E-04          0          0 
v  Dissip       0.50941E-09   0.33809E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.99944E-03   0.44029E+01          0          0 
v  CourantNb    0.73502E-03   0.11332E+00          0          0 
v  FourierNb    0.11548E-02   0.33406E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27403E-06   0.88954E-04          0          0 
a  Dissip       0.50941E-09   0.33809E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11332E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11548E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33406E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35184E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33407E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4991:        0.32499E+00

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


 INSTANT    0.499200000E+03   TIME STEP NUMBER            4992
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.984675801E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.522868620E-22
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20144E-02
   Friction velocity        uet   :  0.44429E-04 0.17086E-02
   Friction velocity        uk    :  0.84703E-03 0.16980E-02
   Dimensionless distance   yplus :  0.21568E+01 0.43018E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13439E-05     174   0.82813E-04   0.50404E-02 
c  VelocityX    0.14910E+01      44   0.11381E-05   0.23274E-13 
c  VelocityY    0.14910E+01      44   0.11381E-05   0.72380E-17 
c  VelocityZ    0.14910E+01      44   0.11381E-05   0.43662E-14 
c  TurbEner     0.27695E-01     182   0.10106E-07   0.41454E-14 
c  Dissip       0.50923E-04     150   0.16543E-07   0.48108E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.50912E-02   0.23394E-01         --         -- 
v  VelocityX    0.94642E-03   0.42156E-02         --         -- 
v  VelocityY   -0.91007E-05   0.91007E-05         --         -- 
v  VelocityZ   -0.21841E-02   0.21841E-02         --         -- 
v  TurbEner     0.27400E-06   0.88924E-04          0          0 
v  Dissip       0.50933E-09   0.33780E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.99902E-03   0.44019E+01          0          0 
v  CourantNb    0.73502E-03   0.11331E+00          0          0 
v  FourierNb    0.11546E-02   0.33398E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27400E-06   0.88924E-04          0          0 
a  Dissip       0.50933E-09   0.33780E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11331E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11546E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33398E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35183E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33399E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4992:        0.31496E+00

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


 INSTANT    0.499300000E+03   TIME STEP NUMBER            4993
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.505890428E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.100053312E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20140E-02
   Friction velocity        uet   :  0.44431E-04 0.17087E-02
   Friction velocity        uk    :  0.84694E-03 0.16975E-02
   Dimensionless distance   yplus :  0.21566E+01 0.43005E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13524E-05     203   0.11326E-03   0.50726E-02 
c  VelocityX    0.14910E+01      44   0.12675E-05   0.22766E-13 
c  VelocityY    0.14910E+01      44   0.12675E-05   0.69787E-17 
c  VelocityZ    0.14910E+01      44   0.12675E-05   0.43025E-14 
c  TurbEner     0.27686E-01     182   0.10092E-07   0.41419E-14 
c  Dissip       0.50900E-04     150   0.16526E-07   0.47344E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.50910E-02   0.23387E-01         --         -- 
v  VelocityX    0.94635E-03   0.42156E-02         --         -- 
v  VelocityY   -0.90890E-05   0.90890E-05         --         -- 
v  VelocityZ   -0.21840E-02   0.21839E-02         --         -- 
v  TurbEner     0.27398E-06   0.88895E-04          0          0 
v  Dissip       0.50925E-09   0.33752E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.99859E-03   0.44010E+01          0          0 
v  CourantNb    0.73502E-03   0.11331E+00          0          0 
v  FourierNb    0.11545E-02   0.33391E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27398E-06   0.88895E-04          0          0 
a  Dissip       0.50925E-09   0.33752E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11331E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11545E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33391E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35181E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33392E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4993:        0.32753E+00

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


 INSTANT    0.499400000E+03   TIME STEP NUMBER            4994
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.926654044E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.114173543E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20135E-02
   Friction velocity        uet   :  0.44432E-04 0.17088E-02
   Friction velocity        uk    :  0.84686E-03 0.16970E-02
   Dimensionless distance   yplus :  0.21564E+01 0.42992E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13244E-05     191   0.10563E-03   0.49672E-02 
c  VelocityX    0.14910E+01      44   0.11573E-05   0.22294E-13 
c  VelocityY    0.14910E+01      44   0.11573E-05   0.66039E-17 
c  VelocityZ    0.14910E+01      44   0.11573E-05   0.42386E-14 
c  TurbEner     0.27677E-01     182   0.10077E-07   0.41384E-14 
c  Dissip       0.50877E-04     150   0.16511E-07   0.46656E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.50882E-02   0.23380E-01         --         -- 
v  VelocityX    0.94629E-03   0.42157E-02         --         -- 
v  VelocityY   -0.90776E-05   0.90775E-05         --         -- 
v  VelocityZ   -0.21838E-02   0.21838E-02         --         -- 
v  TurbEner     0.27395E-06   0.88866E-04          0          0 
v  Dissip       0.50917E-09   0.33723E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.99816E-03   0.44000E+01          0          0 
v  CourantNb    0.73502E-03   0.11330E+00          0          0 
v  FourierNb    0.11544E-02   0.33384E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27395E-06   0.88866E-04          0          0 
a  Dissip       0.50917E-09   0.33723E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11330E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11544E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33384E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35180E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33384E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4994:        0.32306E+00

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


 INSTANT    0.499500000E+03   TIME STEP NUMBER            4995
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.787740641E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.253727960E-22
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20130E-02
   Friction velocity        uet   :  0.44433E-04 0.17090E-02
   Friction velocity        uk    :  0.84676E-03 0.16964E-02
   Dimensionless distance   yplus :  0.21561E+01 0.42979E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        390
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.12422E-05     176   0.10139E-03   0.46600E-02 
c  VelocityX    0.14910E+01      44   0.13781E-05   0.21838E-13 
c  VelocityY    0.14910E+01      44   0.13781E-05   0.62681E-17 
c  VelocityZ    0.14910E+01      44   0.13781E-05   0.41870E-14 
c  TurbEner     0.27667E-01     182   0.10063E-07   0.41350E-14 
c  Dissip       0.50854E-04     150   0.16493E-07   0.46031E-19 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.50878E-02   0.23373E-01         --         -- 
v  VelocityX    0.94622E-03   0.42157E-02         --         -- 
v  VelocityY   -0.90670E-05   0.90670E-05         --         -- 
v  VelocityZ   -0.21837E-02   0.21837E-02         --         -- 
v  TurbEner     0.27392E-06   0.88836E-04          0          0 
v  Dissip       0.50910E-09   0.33695E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.99773E-03   0.43991E+01          0          0 
v  CourantNb    0.73502E-03   0.11329E+00          0          0 
v  FourierNb    0.11542E-02   0.33376E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27392E-06   0.88836E-04          0          0 
a  Dissip       0.50910E-09   0.33695E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01  0.80000E-01 -0.25076E-02  
Courant max  0.11329E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11542E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33376E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35178E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33377E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4995:        0.31709E+00

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


 INSTANT    0.499600000E+03   TIME STEP NUMBER            4996
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.104608569E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.156918747E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20125E-02
   Friction velocity        uet   :  0.44435E-04 0.17091E-02
   Friction velocity        uk    :  0.84667E-03 0.16959E-02
   Dimensionless distance   yplus :  0.21559E+01 0.42966E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        386
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.32296E-05     231   0.11057E-03   0.12114E-01 
c  VelocityX    0.14910E+01      44   0.14562E-05   0.25701E-13 
c  VelocityY    0.14910E+01      44   0.14562E-05   0.23953E-16 
c  VelocityZ    0.14910E+01      44   0.14562E-05   0.42698E-14 
c  TurbEner     0.27658E-01     182   0.10049E-07   0.41317E-14 
c  Dissip       0.50831E-04     150   0.16483E-07   0.20608E-18 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.50832E-02   0.23361E-01         --         -- 
v  VelocityX    0.94616E-03   0.42158E-02         --         -- 
v  VelocityY   -0.90532E-05   0.90532E-05         --         -- 
v  VelocityZ   -0.21836E-02   0.21836E-02         --         -- 
v  TurbEner     0.27389E-06   0.88807E-04          0          0 
v  Dissip       0.50902E-09   0.33666E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.99730E-03   0.43981E+01          0          0 
v  CourantNb    0.73502E-03   0.11328E+00          0          0 
v  FourierNb    0.11541E-02   0.33369E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27389E-06   0.88807E-04          0          0 
a  Dissip       0.50902E-09   0.33666E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01  0.80000E-01 -0.25076E-02  
Courant max  0.11328E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11541E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33369E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35177E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33370E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4996:        0.33794E+00

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


 INSTANT    0.499700000E+03   TIME STEP NUMBER            4997
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.659838666E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.781459496E-22
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20120E-02
   Friction velocity        uet   :  0.44436E-04 0.17093E-02
   Friction velocity        uk    :  0.84656E-03 0.16954E-02
   Dimensionless distance   yplus :  0.21556E+01 0.42953E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        386
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.19909E-05     195   0.10934E-03   0.74673E-02 
c  VelocityX    0.14910E+01      44   0.14758E-05   0.23750E-13 
c  VelocityY    0.14910E+01      44   0.14758E-05   0.45038E-16 
c  VelocityZ    0.14910E+01      44   0.14758E-05   0.43813E-14 
c  TurbEner     0.27649E-01     182   0.10035E-07   0.41282E-14 
c  Dissip       0.50808E-04     150   0.16465E-07   0.15378E-18 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.50830E-02   0.23353E-01         --         -- 
v  VelocityX    0.94609E-03   0.42159E-02         --         -- 
v  VelocityY   -0.90377E-05   0.90377E-05         --         -- 
v  VelocityZ   -0.21835E-02   0.21835E-02         --         -- 
v  TurbEner     0.27387E-06   0.88778E-04          0          0 
v  Dissip       0.50894E-09   0.33638E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.99687E-03   0.43971E+01          0          0 
v  CourantNb    0.73502E-03   0.11327E+00          0          0 
v  FourierNb    0.11539E-02   0.33361E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27387E-06   0.88778E-04          0          0 
a  Dissip       0.50894E-09   0.33638E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01  0.80000E-01 -0.25076E-02  
Courant max  0.11327E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11539E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33361E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35175E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33362E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4997:        0.32571E+00

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


 INSTANT    0.499800000E+03   TIME STEP NUMBER            4998
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.385611749E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.164827047E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20115E-02
   Friction velocity        uet   :  0.44437E-04 0.17095E-02
   Friction velocity        uk    :  0.84645E-03 0.16949E-02
   Dimensionless distance   yplus :  0.21554E+01 0.42940E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        382
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.34145E-05     248   0.11203E-03   0.12808E-01 
c  VelocityX    0.14910E+01      44   0.14066E-05   0.26898E-13 
c  VelocityY    0.14910E+01      44   0.14066E-05   0.30586E-16 
c  VelocityZ    0.14910E+01      44   0.14066E-05   0.45596E-14 
c  TurbEner     0.27639E-01     182   0.10021E-07   0.41248E-14 
c  Dissip       0.50786E-04     150   0.16453E-07   0.28949E-18 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.50790E-02   0.23342E-01         --         -- 
v  VelocityX    0.94603E-03   0.42159E-02         --         -- 
v  VelocityY   -0.90242E-05   0.90241E-05         --         -- 
v  VelocityZ   -0.21834E-02   0.21834E-02         --         -- 
v  TurbEner     0.27384E-06   0.88748E-04          0          0 
v  Dissip       0.50886E-09   0.33609E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.99644E-03   0.43962E+01          0          0 
v  CourantNb    0.73502E-03   0.11327E+00          0          0 
v  FourierNb    0.11538E-02   0.33354E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27384E-06   0.88748E-04          0          0 
a  Dissip       0.50886E-09   0.33609E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01  0.80000E-01 -0.25076E-02  
Courant max  0.11327E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11538E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33354E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35174E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33355E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4998:        0.34465E+00

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


 INSTANT    0.499900000E+03   TIME STEP NUMBER            4999
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.134042964E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.712893977E-22
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20111E-02
   Friction velocity        uet   :  0.44439E-04 0.17097E-02
   Friction velocity        uk    :  0.84634E-03 0.16944E-02
   Dimensionless distance   yplus :  0.21551E+01 0.42928E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        376
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.39870E-05     252   0.11167E-03   0.14957E-01 
c  VelocityX    0.14910E+01      44   0.10829E-05   0.31468E-13 
c  VelocityY    0.14910E+01      44   0.10829E-05   0.34808E-16 
c  VelocityZ    0.14910E+01      44   0.10829E-05   0.52124E-14 
c  TurbEner     0.27630E-01     181   0.10353E-07   0.41216E-14 
c  Dissip       0.50763E-04     150   0.16436E-07   0.50006E-18 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.50767E-02   0.23329E-01         --         -- 
v  VelocityX    0.94596E-03   0.42160E-02         --         -- 
v  VelocityY   -0.90083E-05   0.90083E-05         --         -- 
v  VelocityZ   -0.21833E-02   0.21833E-02         --         -- 
v  TurbEner     0.27381E-06   0.88719E-04          0          0 
v  Dissip       0.50878E-09   0.33581E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.99602E-03   0.43952E+01          0          0 
v  CourantNb    0.73501E-03   0.11326E+00          0          0 
v  FourierNb    0.11536E-02   0.33347E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27381E-06   0.88719E-04          0          0 
a  Dissip       0.50878E-09   0.33581E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73501E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11326E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11536E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33347E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35172E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33347E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             4999:        0.34556E+00

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


 INSTANT    0.500000000E+03   TIME STEP NUMBER            5000
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.751953499E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.145641949E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20106E-02
   Friction velocity        uet   :  0.44440E-04 0.17099E-02
   Friction velocity        uk    :  0.84622E-03 0.16939E-02
   Dimensionless distance   yplus :  0.21548E+01 0.42915E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        376
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.26249E-05     197   0.11476E-03   0.98505E-02 
c  VelocityX    0.14910E+01      43   0.12591E-05   0.27333E-13 
c  VelocityY    0.14910E+01      43   0.12591E-05   0.42210E-16 
c  VelocityZ    0.14910E+01      43   0.12591E-05   0.53533E-14 
c  TurbEner     0.27621E-01     181   0.10338E-07   0.41180E-14 
c  Dissip       0.50740E-04     150   0.16419E-07   0.36036E-18 
c  mesh_u       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_v       0.00000E+00       0   0.00000E+00   0.00000E+00 
c  mesh_w       0.00000E+00       0   0.00000E+00   0.00000E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.50740E-02   0.23321E-01         --         -- 
v  VelocityX    0.94590E-03   0.42160E-02         --         -- 
v  VelocityY   -0.89911E-05   0.89911E-05         --         -- 
v  VelocityZ   -0.21832E-02   0.21832E-02         --         -- 
v  TurbEner     0.27379E-06   0.88690E-04          0          0 
v  Dissip       0.50870E-09   0.33553E-05          0          0 
v  mesh_u       0.00000E+00   0.00000E+00         --         -- 
v  mesh_v       0.00000E+00   0.00000E+00         --         -- 
v  mesh_w       0.00000E+00   0.00000E+00         --         -- 
v  TurbVisc     0.99559E-03   0.43943E+01          0          0 
v  CourantNb    0.73501E-03   0.11325E+00          0          0 
v  FourierNb    0.11535E-02   0.33339E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27379E-06   0.88690E-04          0          0 
a  Dissip       0.50870E-09   0.33553E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73501E-03  0.27286E+01  0.80000E-01 -0.25076E-02  
Courant max  0.11325E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11535E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33339E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35171E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33340E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             5000:        0.52570E+00

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


 INSTANT    0.500100000E+03   TIME STEP NUMBER            5001
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.874985035E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.173674001E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20101E-02
   Friction velocity        uet   :  0.44441E-04 0.17101E-02
   Friction velocity        uk    :  0.84609E-03 0.16934E-02
   Dimensionless distance   yplus :  0.21544E+01 0.42902E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        368
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.874985035E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.173674001E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20037E-02
   Friction velocity        uet   :  0.44300E-04 0.17041E-02
   Friction velocity        uk    :  0.84609E-03 0.16934E-02
   Dimensionless distance   yplus :  0.21544E+01 0.42902E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        368
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.22381E-04     540   0.55676E-02   0.84029E-01 
c  VelocityX    0.14910E+01      43   0.13359E-05   0.84868E-12 
c  VelocityY    0.14910E+01      43   0.13359E-05   0.65332E-16 
c  VelocityZ    0.14910E+01      43   0.13359E-05   0.63524E-12 
c  TurbEner     0.27612E-01     181   0.10324E-07   0.41121E-14 
c  Dissip       0.50717E-04     150   0.16436E-07   0.69312E-18 
c  mesh_u       0.22291E+05     258   0.82505E-03   0.17796E-09 
c  mesh_v       0.22291E+05     258   0.82505E-03   0.10269E-23 
c  mesh_w       0.22291E+05     258   0.82505E-03   0.43602E-19 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.82245E-02   0.12211E-01         --         -- 
v  VelocityX    0.95119E-03   0.42147E-02         --         -- 
v  VelocityY   -0.89661E-05   0.89661E-05         --         -- 
v  VelocityZ   -0.21786E-02   0.21786E-02         --         -- 
v  TurbEner     0.27376E-06   0.88661E-04          0          0 
v  Dissip       0.50863E-09   0.33526E-05          0          0 
v  mesh_u       0.26390E-10   0.13946E-04         --         -- 
v  mesh_v      -0.93412E-11   0.88779E-11         --         -- 
v  mesh_w      -0.21829E-09  -0.41307E-15         --         -- 
v  TurbVisc     0.99516E-03   0.43933E+01          0          0 
v  CourantNb    0.73501E-03   0.11324E+00          0          0 
v  FourierNb    0.11533E-02   0.33332E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27376E-06   0.88661E-04          0          0 
a  Dissip       0.50863E-09   0.33526E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73501E-03  0.27286E+01  0.80000E-01 -0.25076E-02  
Courant max  0.11324E+00  0.12947E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11533E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33332E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35170E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33333E+02  0.27286E+01  0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             5001:        0.94848E+00

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


 INSTANT    0.500200000E+03   TIME STEP NUMBER            5002
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.768894158E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.234526706E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20084E-02
   Friction velocity        uet   :  0.44425E-04 0.17091E-02
   Friction velocity        uk    :  0.84595E-03 0.16929E-02
   Dimensionless distance   yplus :  0.21541E+01 0.42890E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        366
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.768894158E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.234526706E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.19862E-02
   Friction velocity        uet   :  0.43935E-04 0.16884E-02
   Friction velocity        uk    :  0.84595E-03 0.16929E-02
   Dimensionless distance   yplus :  0.21541E+01 0.42890E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        366
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.38383E-04     572   0.10388E-01   0.14216E+00 
c  VelocityX    0.14910E+01      84   0.11191E-05   0.48161E-11 
c  VelocityY    0.14910E+01      84   0.11191E-05   0.46753E-16 
c  VelocityZ    0.14910E+01      84   0.11191E-05   0.40576E-11 
c  TurbEner     0.27602E-01     181   0.10311E-07   0.41019E-14 
c  Dissip       0.50695E-04     150   0.17109E-07   0.60019E-18 
c  mesh_u       0.77103E+05     239   0.69516E-03   0.10699E-08 
c  mesh_v       0.77103E+05     239   0.69516E-03   0.62572E-23 
c  mesh_w       0.77103E+05     239   0.69516E-03   0.89261E-17 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.21135E-01   0.62773E-02         --         -- 
v  VelocityX    0.96620E-03   0.42118E-02         --         -- 
v  VelocityY   -0.89395E-05   0.89394E-05         --         -- 
v  VelocityZ   -0.21663E-02   0.21662E-02         --         -- 
v  TurbEner     0.27373E-06   0.88631E-04          0          0 
v  Dissip       0.50855E-09   0.33505E-05          0          0 
v  mesh_u      -0.93570E-08   0.48238E-04         --         -- 
v  mesh_v      -0.32539E-10   0.30763E-10         --         -- 
v  mesh_w      -0.21082E-12   0.29100E-08         --         -- 
v  TurbVisc     0.99471E-03   0.43924E+01          0          0 
v  CourantNb    0.73502E-03   0.11284E+00          0          0 
v  FourierNb    0.11532E-02   0.33325E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27373E-06   0.88631E-04          0          0 
a  Dissip       0.50855E-09   0.33505E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11284E+00  0.12948E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11532E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33325E+02  0.27286E+01 -0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35163E-02 -0.94251E+00  0.80000E-01 -0.68721E-01  
Cou_Fou max  0.33325E+02  0.27286E+01 -0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             5002:        0.14346E+01

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


 INSTANT    0.500300000E+03   TIME STEP NUMBER            5003
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190        -0.354086242E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630        -0.869847808E-22
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20045E-02
   Friction velocity        uet   :  0.44384E-04 0.17064E-02
   Friction velocity        uk    :  0.84580E-03 0.16926E-02
   Dimensionless distance   yplus :  0.21537E+01 0.42881E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        366
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190        -0.354086242E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630        -0.869847808E-22
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.19721E-02
   Friction velocity        uet   :  0.43663E-04 0.16761E-02
   Friction velocity        uk    :  0.84580E-03 0.16926E-02
   Dimensionless distance   yplus :  0.21537E+01 0.42881E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        366
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190        -0.354086242E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630        -0.869847808E-22
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.19722E-02
   Friction velocity        uet   :  0.43664E-04 0.16761E-02
   Friction velocity        uk    :  0.84580E-03 0.16926E-02
   Dimensionless distance   yplus :  0.21537E+01 0.42881E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        366
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.15378E-04     539   0.33468E-02   0.57269E-01 
c  VelocityX    0.14910E+01     102   0.46118E-06   0.20421E-11 
c  VelocityY    0.14910E+01     102   0.46118E-06   0.42022E-16 
c  VelocityZ    0.14910E+01     102   0.46118E-06   0.17632E-11 
c  TurbEner     0.27593E-01     181   0.10297E-07   0.40943E-14 
c  Dissip       0.50672E-04     150   0.17843E-07   0.45442E-18 
c  mesh_u       0.11222E+06     203   0.26543E-03   0.43955E-09 
c  mesh_v       0.11222E+06     203   0.26543E-03   0.26820E-23 
c  mesh_w       0.11222E+06     203   0.26543E-03   0.18997E-14 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.13561E-01   0.44451E-02         --         -- 
v  VelocityX    0.98024E-03   0.42100E-02         --         -- 
v  VelocityY   -0.89117E-05   0.89116E-05         --         -- 
v  VelocityZ   -0.21553E-02   0.21554E-02         --         -- 
v  TurbEner     0.27371E-06   0.88602E-04          0          0 
v  Dissip       0.50847E-09   0.33486E-05          0          0 
v  mesh_u      -0.58527E-07   0.70206E-04         --         -- 
v  mesh_v      -0.48195E-10   0.45153E-10         --         -- 
v  mesh_w      -0.43096E-07   0.51882E-11         --         -- 
v  TurbVisc     0.99423E-03   0.43914E+01          0          0 
v  CourantNb    0.73502E-03   0.11186E+00          0          0 
v  FourierNb    0.11531E-02   0.33317E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27371E-06   0.88602E-04          0          0 
a  Dissip       0.50847E-09   0.33486E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11186E+00  0.12952E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11531E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33317E+02  0.27286E+01 -0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35146E-02 -0.94251E+00  0.80000E-01 -0.68721E-01  
Cou_Fou max  0.33318E+02  0.27286E+01 -0.40000E-01  0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             5003:        0.19968E+01

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


 INSTANT    0.500400000E+03   TIME STEP NUMBER            5004
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.172106507E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.128743500E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20014E-02
   Friction velocity        uet   :  0.44325E-04 0.17046E-02
   Friction velocity        uk    :  0.84566E-03 0.16923E-02
   Dimensionless distance   yplus :  0.21534E+01 0.42874E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        366
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.172106507E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.128743500E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.19699E-02
   Friction velocity        uet   :  0.43654E-04 0.16750E-02
   Friction velocity        uk    :  0.84566E-03 0.16923E-02
   Dimensionless distance   yplus :  0.21534E+01 0.42874E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        366
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.172106507E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.128743500E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.19700E-02
   Friction velocity        uet   :  0.43655E-04 0.16750E-02
   Friction velocity        uk    :  0.84566E-03 0.16923E-02
   Dimensionless distance   yplus :  0.21534E+01 0.42874E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        366
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.37086E-04     574   0.12026E-01   0.13953E+00 
c  VelocityX    0.14910E+01      91   0.54164E-06   0.17387E-12 
c  VelocityY    0.14910E+01      91   0.54164E-06   0.41928E-16 
c  VelocityZ    0.14910E+01      91   0.54164E-06   0.15027E-12 
c  TurbEner     0.27584E-01     181   0.10282E-07   0.40909E-14 
c  Dissip       0.50649E-04     150   0.17558E-07   0.36062E-18 
c  mesh_u       0.11016E+06     110   0.16735E-04   0.20111E-11 
c  mesh_v       0.11016E+06     110   0.16735E-04   0.89370E-25 
c  mesh_w       0.11016E+06     110   0.16735E-04   0.30378E-12 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.73012E-02   0.23138E-01         --         -- 
v  VelocityX    0.98532E-03   0.42104E-02         --         -- 
v  VelocityY   -0.88836E-05   0.88835E-05         --         -- 
v  VelocityZ   -0.21533E-02   0.21502E-02         --         -- 
v  TurbEner     0.27368E-06   0.88573E-04          0          0 
v  Dissip       0.50839E-09   0.33468E-05          0          0 
v  mesh_u      -0.84156E-07   0.68914E-04         --         -- 
v  mesh_v      -0.48600E-10   0.44945E-10         --         -- 
v  mesh_w      -0.10099E-07   0.63576E-06         --         -- 
v  TurbVisc     0.99375E-03   0.43904E+01          0          0 
v  CourantNb    0.73502E-03   0.11121E+00          0          0 
v  FourierNb    0.11529E-02   0.33310E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27368E-06   0.88573E-04          0          0 
a  Dissip       0.50839E-09   0.33468E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01  0.25076E-02  
Courant max  0.11121E+00  0.12959E-01  0.80000E-01  0.22371E-01  
Fourier min  0.11529E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33310E+02  0.27286E+01 -0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35130E-02 -0.94251E+00  0.80000E-01 -0.68721E-01  
Cou_Fou max  0.33311E+02  0.27286E+01 -0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             5004:        0.18827E+01

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


 INSTANT    0.500500000E+03   TIME STEP NUMBER            5005
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.460044769E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630        -0.221952912E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20019E-02
   Friction velocity        uet   :  0.44014E-04 0.17057E-02
   Friction velocity        uk    :  0.84553E-03 0.16921E-02
   Dimensionless distance   yplus :  0.21530E+01 0.42866E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        360
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.460044769E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630        -0.221952912E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.19651E-02
   Friction velocity        uet   :  0.42791E-04 0.16710E-02
   Friction velocity        uk    :  0.84553E-03 0.16921E-02
   Dimensionless distance   yplus :  0.21530E+01 0.42866E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        360
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.460044769E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630        -0.221952912E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.19652E-02
   Friction velocity        uet   :  0.42788E-04 0.16711E-02
   Friction velocity        uk    :  0.84553E-03 0.16921E-02
   Dimensionless distance   yplus :  0.21530E+01 0.42866E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        360
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.13280E-03     539   0.41827E-01   0.45330E+00 
c  VelocityX    0.14910E+01      82   0.92120E-06   0.30508E-10 
c  VelocityY    0.14910E+01      82   0.92120E-06   0.10093E-16 
c  VelocityZ    0.14910E+01      82   0.92120E-06   0.27722E-10 
c  TurbEner     0.27575E-01     181   0.10269E-07   0.40856E-14 
c  Dissip       0.50626E-04     150   0.18445E-07   0.62174E-18 
c  mesh_u       0.12934E+06     183   0.15594E-03   0.11722E-09 
c  mesh_v       0.12934E+06     183   0.15594E-03   0.15040E-23 
c  mesh_w       0.12934E+06     183   0.15594E-03   0.84515E-10 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.54471E-01   0.48526E-01         --         -- 
v  VelocityX    0.98948E-03   0.42127E-02         --         -- 
v  VelocityY   -0.88665E-05   0.88664E-05         --         -- 
v  VelocityZ   -0.21242E-02   0.21675E-02         --         -- 
v  TurbEner     0.27365E-06   0.88544E-04          0          0 
v  Dissip       0.50832E-09   0.33455E-05          0          0 
v  mesh_u      -0.81557E-07   0.80376E-04         --         -- 
v  mesh_v      -0.57889E-10   0.56128E-10         --         -- 
v  mesh_w      -0.93510E-05   0.11499E-08         --         -- 
v  TurbVisc     0.99328E-03   0.43895E+01          0          0 
v  CourantNb    0.73502E-03   0.11115E+00          0          0 
v  FourierNb    0.11528E-02   0.33302E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27365E-06   0.88544E-04          0          0 
a  Dissip       0.50832E-09   0.33455E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73502E-03  0.27286E+01 -0.80000E-01 -0.25076E-02  
Courant max  0.11115E+00  0.12967E-01  0.80000E-01 -0.22371E-01  
Fourier min  0.11528E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33302E+02  0.27286E+01 -0.40000E-01 -0.25076E-02  
Cou_Fou min  0.35124E-02 -0.94251E+00  0.80000E-01  0.68721E-01  
Cou_Fou max  0.33303E+02  0.27286E+01 -0.40000E-01  0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             5005:        0.19311E+01

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


 INSTANT    0.500600000E+03   TIME STEP NUMBER            5006
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.697955149E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.285331641E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.20133E-02
   Friction velocity        uet   :  0.38527E-04 0.17141E-02
   Friction velocity        uk    :  0.84540E-03 0.16920E-02
   Dimensionless distance   yplus :  0.21527E+01 0.42863E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        356
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.697955149E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.285331641E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.19653E-02
   Friction velocity        uet   :  0.32272E-04 0.16667E-02
   Friction velocity        uk    :  0.84540E-03 0.16920E-02
   Dimensionless distance   yplus :  0.21527E+01 0.42863E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        356
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.697955149E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.285331641E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.19656E-02
   Friction velocity        uet   :  0.32204E-04 0.16669E-02
   Friction velocity        uk    :  0.84540E-03 0.16920E-02
   Dimensionless distance   yplus :  0.21527E+01 0.42863E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        356
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.19448E-02     608   0.97712E-01   0.10567E+01 
c  VelocityX    0.14910E+01     129   0.45348E-06   0.65104E-08 
c  VelocityY    0.14910E+01     129   0.45348E-06   0.71568E-16 
c  VelocityZ    0.14910E+01     129   0.45348E-06   0.59394E-08 
c  TurbEner     0.27565E-01     181   0.10277E-07   0.40756E-14 
c  Dissip       0.50604E-04     150   0.85020E-07   0.70042E-18 
c  mesh_u       0.28680E+06     261   0.71671E-03   0.11076E-08 
c  mesh_v       0.28680E+06     261   0.71671E-03   0.16496E-21 
c  mesh_w       0.28680E+06     261   0.71671E-03   0.19769E-07 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.75519E+00   0.75150E+00         --         -- 
v  VelocityX    0.95578E-03   0.42782E-02         --         -- 
v  VelocityY   -0.88665E-05   0.88665E-05         --         -- 
v  VelocityZ   -0.25070E-02   0.18188E-02         --         -- 
v  TurbEner     0.27363E-06   0.88514E-04          0          0 
v  Dissip       0.50824E-09   0.33520E-05          0          0 
v  mesh_u      -0.79596E-07   0.11486E-03         --         -- 
v  mesh_v      -0.15075E-09   0.14897E-09         --         -- 
v  mesh_w      -0.14311E-07   0.13785E-03         --         -- 
v  TurbVisc     0.99281E-03   0.43885E+01          0          0 
v  CourantNb    0.73613E-03   0.11190E+00          0          0 
v  FourierNb    0.11526E-02   0.33295E+02          0          0 
v  total_pressu 0.10132E+06   0.10133E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27363E-06   0.88514E-04          0          0 
a  Dissip       0.50824E-09   0.33520E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.73613E-03  0.27290E+01  0.80000E-01  0.23719E-01  
Courant max  0.11190E+00  0.12972E-01  0.80000E-01  0.22370E-01  
Fourier min  0.11526E-02 -0.94251E+00  0.80000E-01 -0.68721E-01  
Fourier max  0.33295E+02  0.27286E+01 -0.40000E-01  0.25076E-02  
Cou_Fou min  0.35117E-02 -0.94251E+00  0.80000E-01 -0.68721E-01  
Cou_Fou max  0.33296E+02  0.27286E+01 -0.40000E-01 -0.25076E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             5006:        0.22059E+01

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


 INSTANT    0.500700000E+03   TIME STEP NUMBER            5007
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.419281309E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630        -0.272956019E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.22822E-02
   Friction velocity        uet   :  0.41343E-04 0.18481E-02
   Friction velocity        uk    :  0.84506E-03 0.16941E-02
   Dimensionless distance   yplus :  0.21519E+01 0.42922E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        356
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.419281309E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630        -0.272956019E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.22675E-02
   Friction velocity        uet   :  0.34029E-04 0.18180E-02
   Friction velocity        uk    :  0.84506E-03 0.16941E-02
   Dimensionless distance   yplus :  0.21519E+01 0.42922E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        356
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.419281309E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630        -0.272956019E-21
Free outlet               3         400         0.275925776E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.22696E-02
   Friction velocity        uet   :  0.35085E-04 0.18195E-02
   Friction velocity        uk    :  0.84506E-03 0.16941E-02
   Dimensionless distance   yplus :  0.21519E+01 0.42922E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        356
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.28659E-01     576   0.98774E-01   0.10679E+01 
c  VelocityX    0.14909E+01     191   0.33689E-05   0.14131E-05 
c  VelocityY    0.14909E+01     191   0.33689E-05   0.64232E-14 
c  VelocityZ    0.14909E+01     191   0.33689E-05   0.12891E-05 
c  TurbEner     0.27556E-01     181   0.16850E-07   0.41389E-14 
c  Dissip       0.50581E-04     150   0.14589E-05   0.43657E-17 
c  mesh_u       0.32548E+07     289   0.85026E-03   0.38172E-09 
c  mesh_v       0.32548E+07     289   0.85026E-03   0.34540E-19 
c  mesh_w       0.32548E+07     289   0.85026E-03   0.43183E-05 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.11103E+02   0.11098E+02         --         -- 
v  VelocityX   -0.88323E-02   0.14929E-01         --         -- 
v  VelocityY   -0.92687E-05   0.92687E-05         --         -- 
v  VelocityZ   -0.22173E-02   0.10651E-01         --         -- 
v  TurbEner     0.27360E-06   0.88485E-04          0          0 
v  Dissip       0.50816E-09   0.31561E-05          0          0 
v  mesh_u      -0.26015E-07   0.13510E-03         --         -- 
v  mesh_v      -0.12803E-08   0.13629E-08         --         -- 
v  mesh_w      -0.20318E-02   0.46947E-07         --         -- 
v  TurbVisc     0.99229E-03   0.43876E+01          0          0 
v  CourantNb    0.75831E-03   0.12601E+00          0          0 
v  FourierNb    0.11525E-02   0.33288E+02          0          0 
v  total_pressu 0.10131E+06   0.10134E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27360E-06   0.88485E-04          0          0 
a  Dissip       0.50816E-09   0.31561E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.75831E-03  0.27319E+01  0.23034E-13 -0.17586E+00  
Courant max  0.12601E+00  0.11130E-02  0.80000E-01 -0.11276E-01  
Fourier min  0.11525E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Fourier max  0.33288E+02  0.27286E+01  0.40000E-01 -0.25069E-02  
Cou_Fou min  0.35100E-02 -0.94251E+00 -0.80000E-01  0.68721E-01  
Cou_Fou max  0.33289E+02  0.27286E+01  0.40000E-01 -0.25069E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             5007:        0.23239E+01

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


 INSTANT    0.500800000E+03   TIME STEP NUMBER            5008
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.324413619E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.287698168E-21
Free outlet               3         400         0.275925777E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.89168E-02
   Friction velocity        uet   :  0.36354E-05 0.38560E-02
   Friction velocity        uk    :  0.84335E-03 0.18283E-02
   Dimensionless distance   yplus :  0.21493E+01 0.46392E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        353
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.324413619E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.287698168E-21
Free outlet               3         400         0.275925777E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.11153E-01
   Friction velocity        uet   :  0.28125E-04 0.43224E-02
   Friction velocity        uk    :  0.84335E-03 0.18283E-02
   Dimensionless distance   yplus :  0.21493E+01 0.46392E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        353
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.324413619E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.287698168E-21
Free outlet               3         400         0.275925777E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.11210E-01
   Friction velocity        uet   :  0.39027E-04 0.43433E-02
   Friction velocity        uk    :  0.84335E-03 0.18283E-02
   Dimensionless distance   yplus :  0.21493E+01 0.46392E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        353
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.324413619E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630         0.287698168E-21
Free outlet               3         400         0.275925777E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.11210E-01
   Friction velocity        uet   :  0.39018E-04 0.43434E-02
   Friction velocity        uk    :  0.84335E-03 0.18283E-02
   Dimensionless distance   yplus :  0.21493E+01 0.46392E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        353
   Total number of wall faces                   :       1190
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.42234E+00     576   0.98808E-01   0.10680E+01 
c  VelocityX    0.14940E+01     255   0.44597E-04   0.30697E-03 
c  VelocityY    0.14940E+01     255   0.44597E-04   0.19667E-12 
c  VelocityZ    0.14940E+01     255   0.44597E-04   0.27969E-03 
c  TurbEner     0.27547E-01     181   0.83551E-07   0.98099E-14 
c  Dissip       0.50558E-04     150   0.62269E-05   0.12917E-15 
c  mesh_u       0.47871E+08     294   0.10664E-02   0.18307E-10 
c  mesh_v       0.47871E+08     294   0.10664E-02   0.75065E-17 
c  mesh_w       0.47871E+08     294   0.10664E-02   0.93849E-03 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.16363E+03   0.16361E+03         --         -- 
v  VelocityX   -0.17243E+00   0.18071E+00         --         -- 
v  VelocityY   -0.27318E-04   0.27318E-04         --         -- 
v  VelocityZ   -0.15712E+00   0.29520E-01         --         -- 
v  TurbEner     0.27358E-06   0.88457E-04          0          0 
v  Dissip       0.50806E-09   0.23102E-05          0          0 
v  mesh_u      -0.17791E-07   0.13042E-03         --         -- 
v  mesh_v      -0.21229E-07   0.19956E-07         --         -- 
v  mesh_w      -0.57221E-06   0.29949E-01         --         -- 
v  TurbVisc     0.99435E-03   0.43866E+01          0          0 
v  CourantNb    0.80871E-03   0.49707E+00          0          0 
v  FourierNb    0.11523E-02   0.33280E+02          0          0 
v  total_pressu 0.10116E+06   0.10149E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27358E-06   0.88457E-04          0          0 
a  Dissip       0.50806E-09   0.23102E-05          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.80871E-03  0.27584E+01 -0.80000E-01  0.15530E+01  
Courant max  0.49707E+00 -0.12865E-02 -0.79994E-01  0.63384E-02  
Fourier min  0.11523E-02 -0.94250E+00  0.80000E-01 -0.68727E-01  
Fourier max  0.33280E+02  0.27286E+01  0.40000E-01  0.24973E-02  
Cou_Fou min  0.35085E-02 -0.94250E+00 -0.80000E-01 -0.68727E-01  
Cou_Fou max  0.33284E+02  0.27286E+01  0.40000E-01  0.24973E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             5008:        0.31530E+01

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


 INSTANT    0.500900000E+03   TIME STEP NUMBER            5009
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190        -0.112757026E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630        -0.598863674E-22
Free outlet               3         400         0.275925765E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.10893E+00
   Friction velocity        uet   :  0.12122E-04 0.60820E-01
   Friction velocity        uk    :  0.86276E-03 0.22260E-02
   Dimensionless distance   yplus :  0.19211E+01 0.57809E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        312
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190        -0.112757026E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630        -0.598863674E-22
Free outlet               3         400         0.275925765E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.16057E+00
   Friction velocity        uet   :  0.58456E-04 0.11878E+00
   Friction velocity        uk    :  0.86276E-03 0.22260E-02
   Dimensionless distance   yplus :  0.19211E+01 0.57809E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        312
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190        -0.112757026E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630        -0.598863674E-22
Free outlet               3         400         0.275925765E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.16160E+00
   Friction velocity        uet   :  0.45053E-04 0.11128E+00
   Friction velocity        uk    :  0.86276E-03 0.22260E-02
   Dimensionless distance   yplus :  0.19211E+01 0.57809E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        312
   Total number of wall faces                   :       1190
------------------------------------------------------------




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190        -0.112757026E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630        -0.598863674E-22
Free outlet               3         400         0.275925765E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.16161E+00
   Friction velocity        uet   :  0.44901E-04 0.11127E+00
   Friction velocity        uk    :  0.86276E-03 0.22260E-02
   Dimensionless distance   yplus :  0.19211E+01 0.57809E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        312
   Total number of wall faces                   :       1190
------------------------------------------------------------


 --- Information on the volumes
       Minimum control volume      = -2.0721573e-06
       Maximum control volume      =  6.6092676e-03
       Total volume for the domain =  2.7653092e+00

Abort due to the detection of a negative control volume.

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  Pressure     0.62125E+01     608   0.99046E-01   0.10680E+01 
c  VelocityX    0.20443E+01     313   0.56746E-02   0.66978E-01 
c  VelocityY    0.20443E+01     313   0.56746E-02   0.13209E-08 
c  VelocityZ    0.20443E+01     313   0.56746E-02   0.61995E-01 
c  TurbEner     0.27539E-01     180   0.42131E-05   0.28767E-10 
c  Dissip       0.16368E-03     130   0.34485E-03   0.14045E-10 
c  mesh_u       0.70559E+09     292   0.72943E-02   0.35704E-08 
c  mesh_v       0.70559E+09     292   0.72943E-02   0.16288E-14 
c  mesh_w       0.70559E+09     292   0.72943E-02   0.20413E+00 
---------------------------------------------------------------
  
  

   ** INFORMATION ON VARIABLES
      ------------------------
---------------------------------------------------------------
   Variable      Min. value    Max. value   Min clip   Max clip
---------------------------------------------------------------
v  Pressure    -0.24095E+04   0.24080E+04         --         -- 
v  VelocityX   -0.26353E+01   0.27571E+01         --         -- 
v  VelocityY   -0.33547E-02   0.39548E-02         --         -- 
v  VelocityZ   -0.43294E+00   0.25589E+01         --         -- 
v  TurbEner     0.27368E-06   0.89397E-04          0          0 
v  Dissip       0.50820E-09   0.69693E-04          0          0 
v  mesh_u      -0.19436E-06   0.19242E-03         --         -- 
v  mesh_v      -0.28688E-06   0.29123E-06         --         -- 
v  mesh_w      -0.44143E+00   0.17992E-03         --         -- 
v  TurbVisc     0.10574E-02   0.43857E+01          0          0 
v  CourantNb    0.52099E-03   0.10702E+02          0          0 
v  FourierNb    0.11522E-02   0.33273E+02          0          0 
v  total_pressu 0.98915E+05   0.10373E+06          0          0 
v  mesh_vi1     0.10000E+01   0.10000E+11          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON CLIPPINGS
      ------------------------
---------------------------------------------------------------
   Variable    Min wo clips  Max wo clips   Min clip   Max clip
---------------------------------------------------------------
a  TurbEner     0.27368E-06   0.89397E-04          0          0 
a  Dissip       0.50820E-09   0.69693E-04          0          0 
---------------------------------------------------------------
  
  

   ** INFORMATION ON THE TIME STEP
      -----------------------------
---------------------------------------------------------------
Criterion    Value      at         xc           yc           zc
---------------------------------------------------------------
Courant min  0.52099E-03  0.27584E+01 -0.80000E-01 -0.15530E+01  
Courant max  0.10702E+02  0.12361E-02  0.79925E-01  0.12785E-01  
Fourier min  0.11522E-02 -0.94250E+00  0.80000E-01  0.68813E-01  
Fourier max  0.33273E+02  0.27286E+01 -0.40000E-01 -0.23560E-02  
Cou_Fou min  0.36109E-02 -0.93781E+00 -0.80000E-01  0.77420E+00  
Cou_Fou max  0.33313E+02  0.27286E+01 -0.40000E-01 -0.23560E-02  
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             5009:        0.32996E+01

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


 INSTANT    0.501000000E+03   TIME STEP NUMBER            5010
 ============================================================= 


 Warning:
 --------
   _iterative_scalar_gradient; variable:  1; sweeps: 100
                               normed residual:  8.9178e+55; norm:  1.6406e+01


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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         100        -0.275925776E+01
Smooth wall               5        1190         0.281025203E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4       28630        -0.372195137E-20
Free outlet               3         400         0.275925867E+01
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87368E+00 0.16599E+01
   Friction velocity        uet   :  0.12805E-03 0.31928E+00
   Friction velocity        uk    :  0.15541E-02 0.38701E-02
   Dimensionless distance   yplus :  0.41109E+01 0.38852E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         28
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       1190
------------------------------------------------------------


Incoming flow detained for        105 outlet faces on        400
 Warning:
 --------
   _iterative_scalar_gradient; variable:  1; sweeps: 100
                               normed residual:  9.9885e+55; norm:  1.4648e+01
 Warning:
 --------
   _iterative_scalar_gradient; variable:  1; sweeps: 100
                               normed residual:  9.9885e+55; norm:  1.4648e+01
 Warning:
 --------
   _iterative_scalar_gradient; variable:  1; sweeps: 100
                               normed residual:  9.9885e+55; norm:  1.4648e+01


Conjugate gradient [Pressure:0000]: divergence after 1 iterations:
  initial residual:  2.1393e+02; current residual:  1.2431e+07



cs_multigrid.c:1230: Fatal error.

algebraic multigrid [Pressure]: divergence after 4 cycles:
  initial residual: -1.0000e+00; current residual:  1.2431e+07


Call stack:
   1: 0x7fd476403092 <bft_error+0x92>                 (libsaturne.so.0)
   2: 0x7fd476083846 <+0x319846>                      (libsaturne.so.0)
   3: 0x7fd476081da5 <cs_multigrid_solve+0x715>       (libsaturne.so.0)
   4: 0x7fd47608166f <resmgr_+0x16f>                  (libsaturne.so.0)
   5: 0x7fd4760c13bf <invers_+0x10f>                  (libsaturne.so.0)
   6: 0x7fd475f7d719 <resopv_+0x8289>                 (libsaturne.so.0)
   7: 0x7fd475f0b7a1 <navstv_+0x2f61>                 (libsaturne.so.0)
   8: 0x7fd475f9ff5c <tridim_+0x2a2c>                 (libsaturne.so.0)
   9: 0x7fd475de6d04 <caltri_+0x3fe4>                 (libsaturne.so.0)
  10: 0x7fd475dba142 <cs_run+0x8e2>                   (libsaturne.so.0)
  11: 0x7fd475db983c <main+0x14c>                     (libsaturne.so.0)
  12: 0x7fd471238d1d <__libc_start_main+0xfd>         (libc.so.6)
  13: 0x4007e9     <>                               (cs_solver)
End of stack

