command: 
 /usr/local/libexec/code_saturne/cs_solver --param CilCurs_1ms_test05.xml --mpi

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

                                  (R)
                      Code_Saturne

                      Version 3.3.0


  Copyright (C) 1998-2014 EDF S.A., France

  build Tue 27 May 2014 08:50:33 AM CEST
  MPI version 2.2 (MPICH2 1.4.1)


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

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

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


Local case configuration:

  Date:                Wed 16 Jul 2014 08:52:30 AM CEST
  System:              Linux 3.8.0-30-generic
  Machine:             celsius
  Processor:           model name	: Intel(R) Xeon(R) CPU E3-1225 v3 @ 3.20GHz
  Memory:              15936 MB
  User:                claudio (Claudio)
  Directory:           /home/claudio/Documents/Dynamica/CilindroCursore/06_CFD/CilCurs/Test01/RESU/20140716-0852
  MPI ranks:           4 (appnum attribute: 0)
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

 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   =              6 (Nb variables                )
       NSCAL  =              0 (Nb scalars                  )
       NSCAUS =              0 (Nb user scalars             )
       NSCAPP =              0 (Nb specific physics scalars )
       NPROCE =              6 (Nb cell properties          )


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


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

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

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

  -- Continuous phase:

       RO0    =    0.88000E+03 (Reference density           )
       VISCL0 =    0.39600E-01 (Ref. molecular dyn. visc.   )
       CP0    =    0.10172E+04 (Ref. specific heat          )
       ICP    =              0 (> 0: variable CP (usphyv)   )
       P0     =    0.50000E+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

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


 ** HOMOGENEOUS MIXTURE MODEL FOR CAVITATION
    ----------------------------------------

       ICAVIT =             -1 (-1: single phase flow       )
                               ( 0: no vap./cond. model     )
                               ( 1: Merkle's model        )


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


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

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


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

 --- Continuous phase:

   - Commons
       ITURB  =             21 (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)     )

   - Linear production k-epsilon (ITURB = 21)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       ICLKEP =              0 (k-epsilon clipping model    )
       IKECOU =              0 (k-epsilon coupling mode     )
       IGRAKE =              1 (Account for gravity         )
       RELAXV =    0.10000E+01 for k        (Relaxation)
       RELAXV =    0.10000E+01 for epsilon  (Relaxation)

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

 --- Constants

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

   - Linear production k-epsilon (ITURB = 21)
       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
------------------------------------
 Velocity              1  0.1000E+01
 Pressure              0  0.1000E+01
 k                     1  0.1000E+01
 epsilon               1  0.1000E+01
----------------------------

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

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

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


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

---------------------------------------------------------------------
 Variable          ICONV  IDIFF IDIFFT ISCHCV ISSTPC   BLENCV  THETAV
---------------------------------------------------------------------
 Velocity              1      1      1      1      0 0.10E+01 0.10E+01
 Pressure              0      1      1      1      0 0.00E+00 0.10E+01
 k                     1      1      1      1      0 0.00E+00 0.10E+01
 epsilon               1      1      1      1      0 0.00E+00 0.10E+01
-------------------------------------------------------------

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


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


 ** STOKES
    ------
       IDILAT =              1 (1 : without unsteady term
                                    in the continuity equation
                                2 : with unsteady term in 
                                    the continuity equation)
       IPOROS =              0 (0 : without porous media
                                1 : with porous media)
       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
-------------------------------------------------------------------
 Velocity            100      1  0.1000E-04  0.1000E-06  0.0000E+00
 Pressure            100      2  0.1000E-04  0.1000E-06  0.0000E+00
 k                   100      1  0.1000E-04  0.1000E-06  0.0000E+00
 epsilon             100      1  0.1000E-04  0.1000E-06  0.0000E+00
-----------------------------------------------------------

-------------------------------------------
 Variable         IRCFLU IMLIGR      CLIMGR
-------------------------------------------
 Velocity              1      1  0.1500E+01
 Pressure              1      1  0.1500E+01
 k                     1      1  0.1500E+01
 epsilon               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                )


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


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

--------------------------------------------------
 Variable         IRESOL NITMAX      EPSILO IDIRCL
--------------------------------------------------
 Velocity             -1  10000  0.1000E-07      1
 Pressure              0  10000  0.1000E-07      1
 k                    -1  10000  0.1000E-07      1
 epsilon              -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
--------------------------------------                       
 Velocity              0    100     10
 Pressure              1    100     10
 k                     0    100     10
 epsilon               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 =            200 (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
Velocity
Pressure
k
epsilon
turbulent_viscosity
CourantNb
FourierNb
total_pressure
         --           --

 --- Probe history files
       NTHIST =              1 (Output frequency     )
       FRHIST =     -.10000E+01 (Output frequency (s) )
       NCAPT  =              2 (Number of probes     )
       NTHSAV =             -1 (Checkpoint frequency )

       Number Name                  Nb. probes (-1: all)
         2 Velocity[X]                   -1
         3 Velocity[Y]                   -1
         4 Velocity[Z]                   -1
         5 Pressure                      -1
         6 k                             -1
         7 epsilon                       -1
         8 Density                       -1
         9 LamVisc                       -1
        10 turbulent_viscos              -1
        11 CourantNb                     -1
        12 FourierNb                     -1
        13 total_pressure                -1
         --           --                --

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

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

         2 Velocity                       0
         5 Pressure                       0
         6 k                              0
         7 epsilon                        0
        10 turbulent_viscos            -999
        11 CourantNb                   -999
        12 FourierNb                   -999
        13 total_pressure              -999
         --           --                --

 --- Additional post-processing variables (ipstdv)
       ipstfo =              7 (Force exerted  at boundary)
       ipstyp =              1 (Yplus          at boundary)
       ipstft =              1 (Thermal flow   at boundary)
       ipsttb =              0 (Temperature    at boundary)
       ipstnu =              0 (Nusselt        at boundary)


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


 ** ALE METHOD (MOVING MESH)
    -----------

       IALE   =              0 (1: activated                )
       NALINF =              0 (Fluid initialization
                                                  iterations)


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


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

  -1: name: results
      directory: postprocessing
      format: MED 3.0.6
      options: 
      time dependency: fixed mesh
      output: every 20 time steps and at calculation end


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

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

 Partitioning by space-filling curve: Morton (in bounding box).
  Number of cells per domain (histogramm):
    [      16761 ;      16762 ] =          4

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

 Partitioning finished (0.258 s)


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

 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 =              16761
    maximum value =              16762

      1 : [      16761 ;      16762 ] =          4

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

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

    minimum value =              21699
    maximum value =              22863

      1 : [      21699 ;      21931 [ =          2
      2 : [      21931 ;      22164 [ =          0
      3 : [      22164 ;      22397 [ =          0
      4 : [      22397 ;      22630 [ =          0
      5 : [      22630 ;      22863 ] =          2

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

 Histogram of the number of ghost cells per rank:

    minimum value =               4938
    maximum value =               6102

      1 : [       4938 ;       5170 [ =          2
      2 : [       5170 ;       5403 [ =          0
      3 : [       5403 ;       5636 [ =          0
      4 : [       5636 ;       5869 [ =          0
      5 : [       5869 ;       6102 ] =          2

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

    minimum value =               1984
    maximum value =               2619

      1 : [       1984 ;       2111 [ =          2
      2 : [       2111 ;       2238 [ =          0
      3 : [       2238 ;       2365 [ =          0
      4 : [       2365 ;       2492 [ =          1
      5 : [       2492 ;       2619 ] =          1

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

 Histogram of the number of interior faces per rank:

    minimum value =              33363
    maximum value =              34101

      1 : [      33363 ;      33510 [ =          2
      2 : [      33510 ;      33658 [ =          0
      3 : [      33658 ;      33805 [ =          0
      4 : [      33805 ;      33953 [ =          1
      5 : [      33953 ;      34101 ] =          1

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

 Histogram of the number of boundary faces per rank:

    minimum value =               1114
    maximum value =               2357

      1 : [       1114 ;       1362 [ =          2
      2 : [       1362 ;       1611 [ =          0
      3 : [       1611 ;       1859 [ =          0
      4 : [       1859 ;       2108 [ =          1
      5 : [       2108 ;       2357 ] =          1

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =        229
      2 : [          3 ;          4 ] =      66816

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  3
    maximum value =                  3

      1 : [          3 ;          3 ] =          4

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

 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 =              19569
    maximum value =              21943

      1 : [      19569 ;      20043 [ =          1
      2 : [      20043 ;      20518 [ =          1
      3 : [      20518 ;      20993 [ =          1
      4 : [      20993 ;      21468 [ =          0
      5 : [      21468 ;      21943 ] =          1

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =               9266
    maximum value =               9412

      1 : [       9266 ;       9295 [ =          2
      2 : [       9295 ;       9324 [ =          1
      3 : [       9324 ;       9353 [ =          0
      4 : [       9353 ;       9382 [ =          0
      5 : [       9382 ;       9412 ] =          1

 Mesh coordinates:               minimum    and maximum
                       X : -2.0000000e-02  2.0000000e-02
                       Y :  0.0000000e+00  9.0000000e-02
                       Z : -3.0000000e-02  2.0000000e-02
 Mesh
     Number of cells:          67045
     Number of interior faces: 130712
     Number of boundary faces: 6756
     Number of vertices:       13162

 Groups:
    "G_cursor"
       boundary faces:          276
    "G_in"
       boundary faces:           84
    "G_out"
       boundary faces:           82
    "G_wall"
       boundary faces:         6314

 --- Information on the volumes
       Minimum control volume      =  1.8377501e-11
       Maximum control volume      =  1.7488623e-08
       Total volume for the domain =  9.5766503e-05

  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: 2 -->   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 %

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

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

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

 Computing geometric quantities (0.0518 s)
                                                             
       ALMAX  =    0.45893E-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
 -----------------------------------------                   
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Pressure          0.0000E+00  0.0000E+00
  k                 0.6000E-03  0.6000E-03
  epsilon           0.2882E-04  0.2882E-04
 ---------------------------------

                dt  0.1000E+00  0.1000E+00
 ---------------------------------



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

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



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



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


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




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


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


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.8800E+03  0.8800E+03
  molecular_viscos  0.3960E-01  0.3960E-01
  turbulent_viscos  0.9892E+00  0.9892E+00
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2          84
Smooth wall               5        6590
Rough wall                6           0
Symmetry                  4           0
Free outlet               3          82
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =   -0.90200E-02   0.70910E-01  -0.30000E-01



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84         0.000000000E+00
Smooth wall               5        6590         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.00000E+00 0.00000E+00
   Friction velocity        uk    :  0.39912E-03 0.39712E-02
   Dimensionless distance   yplus :  0.15869E-03 0.16351E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       6590
   Total number of wall faces                   :       6590
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ 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          1
@                                                            
@    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  VelocityX    0.59148E-01    4334   0.87542E-01   0.12407E+01 
c  VelocityY    0.59148E-01    4334   0.87542E-01   0.00000E+00 
c  VelocityZ    0.59148E-01    4334   0.87542E-01   0.00000E+00 
c  Pressure     0.78338E-02    1052   0.14275E+01   0.97924E+00 
c  k            0.21385E-01    2663   0.86643E-01   0.86993E-02 
c  epsilon      0.69784E+01    7178   0.30401E-01   0.12144E+05 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6277          1.7263       -0.064023       -0.064947
v  Velocity[Y]                -0.66443          2.4945         0.23923         0.22737
v  Velocity[Z]                 -1.7384          1.5693        0.061766      0.00041058
v  ǁVelocityǁ                 0.015581          2.7307         0.39677         0.39861
v  Pressure                      2.444          679.26           468.7          387.25
v  k                        3.2946e-07         0.23747       0.0090555       0.0083734
v  epsilon                      2.9623          91.667          33.458          26.964
v  turbulent_viscosity         0.98924         0.98924         0.98924         0.98924
v  CourantNb                         0               0               0               0
v  FourierNb                    151.69           32429          1442.1          792.04
v  total_pressure                5e+05      5.0068e+05      5.0047e+05      5.0039e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          151.69           32429          1442.1          792.04


 TIME FOR THE TIME STEP                1:        0.89309E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282683E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50793E+00 0.65247E+00
   Friction velocity        uet   :  0.21099E-01 0.12387E+01
   Friction velocity        uk    :  0.23844E-01 0.12386E+01
   Dimensionless distance   yplus :  0.25961E+00 0.65785E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        134
   Nb of faces within the viscous sub-layer     :       4419
   Total number of wall faces                   :       6590
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ 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  VelocityX    0.39838E-01     576   0.48101E+00   0.91315E-01 
c  VelocityY    0.39838E-01     576   0.48101E+00   0.00000E+00 
c  VelocityZ    0.39838E-01     576   0.48101E+00   0.00000E+00 
c  Pressure     0.30163E-01     952   0.34720E+00   0.97951E+00 
c  k            0.20723E-01      55   0.33475E-02   0.46319E-02 
c  epsilon      0.19036E+02      39   0.87836E-03   0.11487E+05 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.0979e-05                          1986
a  epsilon     -4.3379e-05                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5443           1.632       -0.074465       -0.067401
v  Velocity[Y]                 -0.6647          2.4373         0.24956         0.23136
v  Velocity[Z]                 -1.5683           1.475        0.093734     -0.00053281
v  ǁVelocityǁ                0.0043798          2.7096         0.44574         0.41972
v  Pressure                      2.049          473.04          376.99          309.77
v  k                        4.4717e-14         0.20206      0.00083529       0.0016925
v  epsilon                  1.7935e-06          95.648         0.25828         0.45939
v  turbulent_viscosity      1.9387e-12         0.04886      0.00061638      0.00082227
v  CourantNb                  0.049667          1174.5          81.849          62.329
v  FourierNb                    5.8385          1248.2          56.213          31.071
v  total_pressure                5e+05      5.0047e+05      5.0038e+05      5.0031e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.3158            2212          138.06          93.399


 TIME FOR THE TIME STEP                2:        0.20623E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.151846620E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282691E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53103E+00 0.64912E+00
   Friction velocity        uet   :  0.16962E-01 0.11878E+01
   Friction velocity        uk    :  0.16962E-01 0.11878E+01
   Dimensionless distance   yplus :  0.17428E+00 0.66777E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        137
   Nb of faces within the viscous sub-layer     :       4535
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.39270E-01     561   0.43102E+00   0.44367E-01 
c  VelocityY    0.39270E-01     561   0.43102E+00   0.00000E+00 
c  VelocityZ    0.39270E-01     561   0.43102E+00   0.00000E+00 
c  Pressure     0.31658E-01     908   0.15735E+00   0.58439E+00 
c  k            0.12887E-01      76   0.32228E-02   0.86565E-03 
c  epsilon      0.95589E+01      60   0.50911E-02   0.48620E+03 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.0803e-07                          3302
a  epsilon     -0.00063218                          1460


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5613          1.5988       -0.082172       -0.068087
v  Velocity[Y]                -0.62879          2.4641         0.25951         0.23327
v  Velocity[Z]                  -1.489          1.4921         0.11515      -0.0008458
v  ǁVelocityǁ                0.0040362          2.7552         0.49155         0.44561
v  Pressure                     2.6368             847          667.77          547.43
v  k                        4.4102e-19         0.20721       0.0025465       0.0039905
v  epsilon                  1.4223e-13          439.97          1.3926          1.6473
v  turbulent_viscosity      3.9959e-22        0.047058      0.00028709      0.00058827
v  CourantNb                   0.11663          1221.8          93.558          66.587
v  FourierNb                    5.8385          1248.2          55.851          30.997
v  total_pressure                5e+05      5.0085e+05      5.0067e+05      5.0055e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.3323          1312.4          149.41          97.584


 TIME FOR THE TIME STEP                3:        0.17222E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.206910297E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282697E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34305E+00 0.67569E+00
   Friction velocity        uet   :  0.19609E-01 0.10437E+01
   Friction velocity        uk    :  0.19609E-01 0.10437E+01
   Dimensionless distance   yplus :  0.23506E+00 0.61271E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         84
   Nb of faces within the viscous sub-layer     :       4657
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.40249E-01     553   0.45981E+00   0.27017E-01 
c  VelocityY    0.40249E-01     553   0.45981E+00   0.00000E+00 
c  VelocityZ    0.40249E-01     553   0.45981E+00   0.00000E+00 
c  Pressure     0.37907E-01     871   0.97839E-01   0.48776E+00 
c  k            0.15830E-01     124   0.10666E-02   0.20332E-03 
c  epsilon      0.99954E+01     107   0.18027E-02   0.84450E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.0515e-07                          2482
a  epsilon     -0.00047156                          2565


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5558          1.4312       -0.084758       -0.068563
v  Velocity[Y]                -0.56835          2.5351         0.26639         0.23479
v  Velocity[Z]                 -1.4764          1.4313           0.117      -0.0004922
v  ǁVelocityǁ                0.0038527          2.7665         0.51301         0.45763
v  Pressure                     2.0954          1155.1          902.85          738.02
v  k                             1e-24         0.20709       0.0041032       0.0049177
v  epsilon                  8.6024e-18          287.16          1.3904          1.6567
v  turbulent_viscosity      2.6238e-24        0.047463       0.0010392       0.0014499
v  CourantNb                  0.032683          1214.3           104.3           71.31
v  FourierNb                    5.8385          1248.2          56.737          31.626
v  total_pressure                5e+05      5.0116e+05       5.009e+05      5.0074e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.3043          1296.2          161.04          102.94


 TIME FOR THE TIME STEP                4:        0.17197E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.248802693E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282703E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35404E+00 0.64301E+00
   Friction velocity        uet   :  0.16835E-01 0.92887E+00
   Friction velocity        uk    :  0.16835E-01 0.92871E+00
   Dimensionless distance   yplus :  0.14828E+00 0.61472E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         88
   Nb of faces within the viscous sub-layer     :       4700
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.39520E-01     548   0.41528E+00   0.20374E-01 
c  VelocityY    0.39520E-01     548   0.41528E+00   0.00000E+00 
c  VelocityZ    0.39520E-01     548   0.41528E+00   0.00000E+00 
c  Pressure     0.42057E-01     841   0.69659E-01   0.41495E+00 
c  k            0.15328E-01     170   0.54372E-03   0.50045E-04 
c  epsilon      0.93662E+01     147   0.92831E-03   0.33132E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -9.9279e-06                           680
a  epsilon       -0.017819                          1005


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5149          1.4399       -0.085109        -0.06916
v  Velocity[Y]                -0.53172          2.5724         0.27051         0.23642
v  Velocity[Z]                 -1.4656          1.4278         0.11705     -0.00037167
v  ǁVelocityǁ                0.0016459           2.804         0.52039         0.46344
v  Pressure                     1.1556          1418.1            1102             898
v  k                        6.9095e-24         0.20707       0.0050676       0.0053574
v  epsilon                   1.974e-20          235.79          1.6268          1.7886
v  turbulent_viscosity      9.2067e-30        0.047565       0.0026469        0.002197
v  CourantNb                   0.21219          1189.9          109.29          73.425
v  FourierNb                    5.8385          1248.2          59.637          32.644
v  total_pressure                5e+05      5.0142e+05       5.011e+05       5.009e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.0116          1340.1          168.92          106.07


 TIME FOR THE TIME STEP                5:        0.17059E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.171091556E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282713E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31159E+00 0.64823E+00
   Friction velocity        uet   :  0.27084E-02 0.84100E+00
   Friction velocity        uk    :  0.27084E-02 0.84080E+00
   Dimensionless distance   yplus :  0.21700E-01 0.60413E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         88
   Nb of faces within the viscous sub-layer     :       4727
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.40781E-01     546   0.46001E+00   0.12527E-01 
c  VelocityY    0.40781E-01     546   0.46001E+00   0.00000E+00 
c  VelocityZ    0.40781E-01     546   0.46001E+00   0.00000E+00 
c  Pressure     0.44777E-01     822   0.54071E-01   0.35613E+00 
c  k            0.15388E-01     209   0.32263E-03   0.19619E-04 
c  epsilon      0.94179E+01     167   0.82872E-03   0.24134E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.1205e-06                             1
a  epsilon      -0.0025284                            26


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5653          1.4266       -0.085363        -0.06964
v  Velocity[Y]                -0.56517          2.6712         0.27447         0.23772
v  Velocity[Z]                 -1.4522          1.3869         0.11782      -0.0006538
v  ǁVelocityǁ                0.0037354          2.9097         0.53213         0.47168
v  Pressure                     0.3015          1649.6          1278.8          1038.8
v  k                        4.0043e-22         0.20702       0.0054047       0.0055972
v  epsilon                  1.0702e-20          232.69          1.4766          1.7249
v  turbulent_viscosity      4.1654e-27        0.047544       0.0039708       0.0027461
v  CourantNb                   0.13426          1136.1          110.78          74.316
v  FourierNb                    5.8385          1248.2          62.114          33.451
v  total_pressure                5e+05      5.0165e+05      5.0128e+05      5.0104e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.1266          1404.6           172.9          107.77


 TIME FOR THE TIME STEP                6:        0.17066E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.266977423E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282729E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34286E+00 0.64891E+00
   Friction velocity        uet   :  0.13306E-01 0.78968E+00
   Friction velocity        uk    :  0.13181E-01 0.78953E+00
   Dimensionless distance   yplus :  0.15054E+00 0.61127E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         94
   Nb of faces within the viscous sub-layer     :       4713
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.39993E-01     552   0.41438E+00   0.64669E-02 
c  VelocityY    0.39993E-01     552   0.41438E+00   0.00000E+00 
c  VelocityZ    0.39993E-01     552   0.41438E+00   0.00000E+00 
c  Pressure     0.46287E-01     804   0.43448E-01   0.30933E+00 
c  k            0.15298E-01     270   0.24238E-03   0.10878E-04 
c  epsilon      0.93392E+01     225   0.68620E-03   0.17060E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5304           1.415       -0.085336       -0.070078
v  Velocity[Y]                -0.56262          2.7729         0.27769         0.23852
v  Velocity[Z]                 -1.4301          1.4307         0.11779     -0.00084399
v  ǁVelocityǁ                0.0030981          3.0328         0.54243         0.48017
v  Pressure                   -0.65529          1858.9            1440          1166.3
v  k                        1.3545e-08         0.20698       0.0058366       0.0058748
v  epsilon                  1.9132e-06          238.19          1.5679          1.7711
v  turbulent_viscosity      1.6532e-24         0.35574       0.0052651       0.0035083
v  CourantNb                  0.034572          1087.1          113.35          75.691
v  FourierNb                    5.8385          1248.3          64.266          34.329
v  total_pressure                5e+05      5.0186e+05      5.0144e+05      5.0117e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.9621          1463.7          177.62          110.02


 TIME FOR THE TIME STEP                7:        0.17277E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.142468626E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282727E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34049E+00 0.65020E+00
   Friction velocity        uet   :  0.11329E-01 0.76834E+00
   Friction velocity        uk    :  0.11220E-01 0.76825E+00
   Dimensionless distance   yplus :  0.14324E+00 0.61070E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         95
   Nb of faces within the viscous sub-layer     :       4692
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.41047E-01     553   0.44911E+00   0.48374E-02 
c  VelocityY    0.41047E-01     553   0.44911E+00   0.00000E+00 
c  VelocityZ    0.41047E-01     553   0.44911E+00   0.00000E+00 
c  Pressure     0.47702E-01     788   0.35855E-01   0.27515E+00 
c  k            0.15302E-01     211   0.21758E-03   0.79642E-05 
c  epsilon      0.93416E+01     157   0.47924E-03   0.10700E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.5646e-06                             1
a  epsilon      -0.0048297                             3


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5691          1.4124       -0.086197       -0.070562
v  Velocity[Y]                 -0.5949          2.8511         0.27947         0.23894
v  Velocity[Z]                 -1.4493          1.4307         0.11714      -0.0011779
v  ǁVelocityǁ                0.0037968          3.0188          0.5496         0.48827
v  Pressure                    -1.6704          2051.6          1589.5          1283.5
v  k                        5.9225e-09         0.20696       0.0057534       0.0059383
v  epsilon                  1.8408e-07          243.89          1.5256          1.7667
v  turbulent_viscosity      2.2233e-10        0.047532       0.0057106       0.0039364
v  CourantNb                0.00030308          1020.5          115.58          77.083
v  FourierNb                    5.8387          1248.2          64.835          34.683
v  total_pressure                5e+05      5.0205e+05      5.0159e+05      5.0128e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.5711          1490.8          180.42          111.77


 TIME FOR THE TIME STEP                8:        0.16990E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.139229055E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282755E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37408E+00 0.65065E+00
   Friction velocity        uet   :  0.12225E-01 0.75738E+00
   Friction velocity        uk    :  0.12202E-01 0.75727E+00
   Dimensionless distance   yplus :  0.12675E+00 0.61778E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         99
   Nb of faces within the viscous sub-layer     :       4656
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.40683E-01     553   0.41518E+00   0.39677E-02 
c  VelocityY    0.40683E-01     553   0.41518E+00   0.00000E+00 
c  VelocityZ    0.40683E-01     553   0.41518E+00   0.00000E+00 
c  Pressure     0.48951E-01     782   0.30079E-01   0.24938E+00 
c  k            0.15280E-01     231   0.24050E-03   0.79890E-05 
c  epsilon      0.94244E+01     164   0.94503E-03   0.18195E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5452           1.431       -0.086047       -0.070964
v  Velocity[Y]                -0.64112          2.9336         0.28151         0.23919
v  Velocity[Z]                 -1.4775           1.608          0.1167      -0.0010927
v  ǁVelocityǁ                0.0035624          3.2402         0.55836         0.49653
v  Pressure                    -4.2766          2232.4          1729.9          1392.7
v  k                        1.6367e-07         0.20695       0.0058224        0.005994
v  epsilon                  2.0769e-05          247.03          1.5841          1.8001
v  turbulent_viscosity      9.2645e-09        0.047528        0.005729         0.00402
v  CourantNb                   0.19751          968.58          116.94          78.286
v  FourierNb                    5.8391          1248.2          64.815          34.724
v  total_pressure                5e+05      5.0223e+05      5.0173e+05      5.0139e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.8622          1516.2          181.76          113.01


 TIME FOR THE TIME STEP                9:        0.17004E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.817836780E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282754E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37025E+00 0.65042E+00
   Friction velocity        uet   :  0.51106E-02 0.75326E+00
   Friction velocity        uk    :  0.50964E-02 0.75314E+00
   Dimensionless distance   yplus :  0.59207E-01 0.61673E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         99
   Nb of faces within the viscous sub-layer     :       4615
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.41586E-01     553   0.44625E+00   0.33403E-02 
c  VelocityY    0.41586E-01     553   0.44625E+00   0.00000E+00 
c  VelocityZ    0.41586E-01     553   0.44625E+00   0.00000E+00 
c  Pressure     0.49860E-01     770   0.25983E-01   0.22767E+00 
c  k            0.15282E-01     202   0.19521E-03   0.56764E-05 
c  epsilon      0.95299E+01     147   0.52259E-03   0.14669E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6042          1.4626       -0.085951       -0.071504
v  Velocity[Y]                -0.72774          2.9346         0.28251         0.23907
v  Velocity[Z]                  -1.554          1.4411         0.11717      -0.0011471
v  ǁVelocityǁ                0.0035066          3.2324         0.56571         0.50448
v  Pressure                    -7.4905          2404.5          1863.5          1495.7
v  k                        1.3078e-08         0.20694       0.0057171       0.0059867
v  epsilon                  8.6948e-06          253.47          1.5448          1.8001
v  turbulent_viscosity      1.2532e-08        0.047526       0.0056601       0.0040133
v  CourantNb                  0.033622          889.23          118.78          79.584
v  FourierNb                    5.8391          1248.2          64.662          34.695
v  total_pressure           4.9999e+05       5.024e+05      5.0186e+05       5.015e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.5577          1542.6          183.45          114.28


 TIME FOR THE TIME STEP               10:        0.17001E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.969323329E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282755E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40185E+00 0.65128E+00
   Friction velocity        uet   :  0.12480E-01 0.75227E+00
   Friction velocity        uk    :  0.12394E-01 0.75213E+00
   Dimensionless distance   yplus :  0.11528E+00 0.62332E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        106
   Nb of faces within the viscous sub-layer     :       4582
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.41295E-01     554   0.41452E+00   0.28255E-02 
c  VelocityY    0.41295E-01     554   0.41452E+00   0.00000E+00 
c  VelocityZ    0.41295E-01     554   0.41452E+00   0.00000E+00 
c  Pressure     0.50997E-01     768   0.22633E-01   0.21121E+00 
c  k            0.15272E-01     232   0.19463E-03   0.49260E-05 
c  epsilon      0.95933E+01     171   0.55043E-03   0.11417E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5802          1.5055       -0.085585       -0.072001
v  Velocity[Y]                 -0.7553          3.1178         0.28322          0.2389
v  Velocity[Z]                 -1.6046          1.4465         0.11723     -0.00081799
v  ǁVelocityǁ                0.0043417          3.3966         0.57277         0.51252
v  Pressure                     -10.64            2568          1990.7          1593.1
v  k                         7.483e-08         0.20693       0.0058186       0.0060517
v  epsilon                  4.1298e-06          242.78          1.5743           1.823
v  turbulent_viscosity      2.4073e-10        0.047526       0.0057256       0.0040355
v  CourantNb                  0.028016          917.62          120.25          80.767
v  FourierNb                     5.839          1248.2          64.789          34.736
v  total_pressure           4.9999e+05      5.0257e+05      5.0199e+05      5.0159e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           6.455          1561.9          185.04           115.5


 TIME FOR THE TIME STEP               11:        0.17057E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.139334438E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282756E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46069E+00 0.64888E+00
   Friction velocity        uet   :  0.12014E-01 0.75288E+00
   Friction velocity        uk    :  0.11922E-01 0.75274E+00
   Dimensionless distance   yplus :  0.13555E+00 0.61900E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        101
   Nb of faces within the viscous sub-layer     :       4528
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.42970E-01     553   0.47243E+00   0.24685E-02 
c  VelocityY    0.42970E-01     553   0.47243E+00   0.00000E+00 
c  VelocityZ    0.42970E-01     553   0.47243E+00   0.00000E+00 
c  Pressure     0.51972E-01     762   0.20187E-01   0.19708E+00 
c  k            0.15286E-01     207   0.15995E-03   0.48700E-05 
c  epsilon      0.97516E+01     148   0.36065E-03   0.11719E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6538          1.4653       -0.084869       -0.072498
v  Velocity[Y]                -0.82148          3.2189         0.28393         0.23874
v  Velocity[Z]                 -1.6405          1.7056         0.11727     -0.00060808
v  ǁVelocityǁ                0.0059359          3.4945         0.57911         0.51996
v  Pressure                    -13.353          2724.4          2112.3          1685.4
v  k                        1.6695e-07         0.20698       0.0058215       0.0060888
v  epsilon                  6.9129e-06          257.79          1.5956          1.8509
v  turbulent_viscosity      1.0828e-09        0.047525       0.0057988       0.0040668
v  CourantNb                  0.071122          954.61          121.69          81.989
v  FourierNb                    5.8401          1248.2          64.908           34.78
v  total_pressure           4.9999e+05      5.0272e+05      5.0211e+05      5.0169e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.5177          1565.9           186.6          116.77


 TIME FOR THE TIME STEP               12:        0.16894E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.708262481E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282758E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52502E+00 0.64835E+00
   Friction velocity        uet   :  0.15175E-01 0.75611E+00
   Friction velocity        uk    :  0.15067E-01 0.75595E+00
   Dimensionless distance   yplus :  0.16415E+00 0.62327E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        104
   Nb of faces within the viscous sub-layer     :       4469
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          1 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.42456E-01     554   0.44211E+00   0.23121E-02 
c  VelocityY    0.42456E-01     554   0.44211E+00   0.00000E+00 
c  VelocityZ    0.42456E-01     554   0.44211E+00   0.00000E+00 
c  Pressure     0.52510E-01     749   0.18279E-01   0.18390E+00 
c  k            0.15295E-01     212   0.19858E-03   0.50622E-05 
c  epsilon      0.99069E+01     145   0.56916E-03   0.14116E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5696          1.5163       -0.084144        -0.07295
v  Velocity[Y]                -0.90235          3.3424          0.2846         0.23863
v  Velocity[Z]                 -1.7109          1.3921         0.11726      -0.0005434
v  ǁVelocityǁ                0.0054373          3.6045         0.58529         0.52762
v  Pressure                    -16.468          2873.8          2228.6            1773
v  k                        2.9497e-08         0.20692       0.0057899       0.0061072
v  epsilon                  2.8396e-05          263.28          1.6124          1.8756
v  turbulent_viscosity      1.0149e-08        0.047537       0.0057139       0.0040178
v  CourantNb                   0.15728          1002.6          122.98          83.111
v  FourierNb                    5.8414          1248.3          64.774          34.739
v  total_pressure           4.9998e+05      5.0287e+05      5.0223e+05      5.0177e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           7.221          1590.8          187.75          117.85


 TIME FOR THE TIME STEP               13:        0.16950E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.844357535E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282805E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57695E+00 0.64820E+00
   Friction velocity        uet   :  0.14007E-01 0.76000E+00
   Friction velocity        uk    :  0.13909E-01 0.75969E+00
   Dimensionless distance   yplus :  0.12260E+00 0.62473E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        103
   Nb of faces within the viscous sub-layer     :       4411
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.43921E-01     553   0.48353E+00   0.20584E-02 
c  VelocityY    0.43921E-01     553   0.48353E+00   0.00000E+00 
c  VelocityZ    0.43921E-01     553   0.48353E+00   0.00000E+00 
c  Pressure     0.53606E-01     738   0.16782E-01   0.17429E+00 
c  k            0.15306E-01     185   0.19239E-03   0.52884E-05 
c  epsilon      0.10038E+02     143   0.47145E-03   0.14751E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.1883e-05                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6838          1.5381       -0.083334       -0.073361
v  Velocity[Y]                -0.95355          3.1844         0.28527         0.23863
v  Velocity[Z]                 -1.8322          1.3854         0.11708     -0.00050855
v  ǁVelocityǁ                0.0037485          3.4462         0.59119         0.53492
v  Pressure                    -19.913          3018.1          2340.8          1856.9
v  k                        5.1335e-07         0.20693       0.0057814       0.0061268
v  epsilon                  2.2447e-05           258.2          1.6292          1.9021
v  turbulent_viscosity      2.4094e-11         0.04752       0.0056042       0.0039522
v  CourantNb                   0.26464          1031.8          124.23           84.25
v  FourierNb                    5.8422          1248.3          64.594          34.665
v  total_pressure           4.9998e+05      5.0302e+05      5.0234e+05      5.0186e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.0606          1620.7          188.82          118.92


 TIME FOR THE TIME STEP               14:        0.16657E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.598324222E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282807E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54564E+00 0.65042E+00
   Friction velocity        uet   :  0.91237E-02 0.78209E+00
   Friction velocity        uk    :  0.91131E-02 0.78177E+00
   Dimensionless distance   yplus :  0.13821E+00 0.62530E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        106
   Nb of faces within the viscous sub-layer     :       4365
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          2 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.43054E-01     553   0.43529E+00   0.22454E-02 
c  VelocityY    0.43054E-01     553   0.43529E+00   0.00000E+00 
c  VelocityZ    0.43054E-01     553   0.43529E+00   0.00000E+00 
c  Pressure     0.53928E-01     735   0.15491E-01   0.16360E+00 
c  k            0.15313E-01     197   0.18515E-03   0.64862E-05 
c  epsilon      0.10192E+02     129   0.96035E-03   0.41064E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6716          1.5618       -0.082532       -0.073713
v  Velocity[Y]                 -1.0068          3.3922         0.28588         0.23867
v  Velocity[Z]                 -1.9078          1.5418         0.11686     -0.00053468
v  ǁVelocityǁ                 0.003977          3.6304         0.59691         0.54247
v  Pressure                    -22.703          3156.7          2448.5          1936.9
v  k                         1.096e-07         0.20696       0.0057595       0.0061312
v  epsilon                  1.0564e-05          382.77          1.6458          1.9214
v  turbulent_viscosity       2.256e-07        0.047526        0.005511       0.0038685
v  CourantNb                  0.088965          1094.6          125.41           85.32
v  FourierNb                    5.8427          1248.3          64.469          34.596
v  total_pressure           4.9998e+05      5.0316e+05      5.0245e+05      5.0194e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.9313          1640.5          189.88          119.92


 TIME FOR THE TIME STEP               15:        0.16666E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.504103387E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282805E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63757E+00 0.65241E+00
   Friction velocity        uet   :  0.81577E-02 0.78694E+00
   Friction velocity        uk    :  0.81278E-02 0.78658E+00
   Dimensionless distance   yplus :  0.13130E+00 0.63198E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        110
   Nb of faces within the viscous sub-layer     :       4288
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.45020E-01     554   0.48667E+00   0.19475E-02 
c  VelocityY    0.45020E-01     554   0.48667E+00   0.00000E+00 
c  VelocityZ    0.45020E-01     554   0.48667E+00   0.00000E+00 
c  Pressure     0.54534E-01     733   0.14484E-01   0.15489E+00 
c  k            0.15330E-01     195   0.21615E-03   0.70359E-05 
c  epsilon      0.10353E+02     125   0.66174E-03   0.45451E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon      -0.0017719                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7425          1.6577        -0.08183       -0.074157
v  Velocity[Y]                 -1.0474          3.3729         0.28635         0.23867
v  Velocity[Z]                  -1.902          1.3076         0.11684     -0.00034531
v  ǁVelocityǁ                0.0046884           3.637         0.60221          0.5494
v  Pressure                    -26.258          3290.3          2552.2          2013.4
v  k                        5.5397e-07         0.20692       0.0057973       0.0062013
v  epsilon                  5.2262e-07          256.32          1.6655           1.952
v  turbulent_viscosity      7.6882e-09        0.047534       0.0054826       0.0038523
v  CourantNb                  0.043442          1180.9          126.56            86.4
v  FourierNb                    5.8425          1248.3          64.429          34.585
v  total_pressure           4.9997e+05      5.0329e+05      5.0255e+05      5.0201e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.7601          1661.1          190.99          120.99


 TIME FOR THE TIME STEP               16:        0.18836E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.246404531E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282806E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65878E+00 0.65636E+00
   Friction velocity        uet   :  0.13358E-01 0.79592E+00
   Friction velocity        uk    :  0.13323E-01 0.79553E+00
   Dimensionless distance   yplus :  0.17285E+00 0.62984E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        111
   Nb of faces within the viscous sub-layer     :       4224
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.45709E-01     555   0.49979E+00   0.19694E-02 
c  VelocityY    0.45709E-01     555   0.49979E+00   0.00000E+00 
c  VelocityZ    0.45709E-01     555   0.49979E+00   0.00000E+00 
c  Pressure     0.55304E-01     732   0.13661E-01   0.14776E+00 
c  k            0.15344E-01     210   0.21646E-03   0.62709E-05 
c  epsilon      0.10547E+02     127   0.57926E-03   0.27629E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon      -0.0097711                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9981          1.7253       -0.080937       -0.074377
v  Velocity[Y]                 -1.0707          3.4911         0.28708         0.23877
v  Velocity[Z]                 -2.0723          1.3436         0.11664     -0.00044997
v  ǁVelocityǁ                0.0056481          3.8149         0.60767         0.55678
v  Pressure                    -28.969            3419          2652.1          2086.5
v  k                         3.642e-07         0.20691       0.0058247       0.0062386
v  epsilon                  2.8569e-05          265.56          1.6897          1.9793
v  turbulent_viscosity      5.1251e-09         0.04752       0.0054859       0.0038627
v  CourantNb                   0.10348          1260.4          127.61           87.39
v  FourierNb                    5.8422          1248.3          64.427          34.593
v  total_pressure           4.9997e+05      5.0342e+05      5.0265e+05      5.0209e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.1774          1690.4          192.04          121.98


 TIME FOR THE TIME STEP               17:        0.16797E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.641207250E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282805E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71599E+00 0.65796E+00
   Friction velocity        uet   :  0.93994E-02 0.80151E+00
   Friction velocity        uk    :  0.93386E-02 0.80109E+00
   Dimensionless distance   yplus :  0.13371E+00 0.63397E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        110
   Nb of faces within the viscous sub-layer     :       4175
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.46345E-01     556   0.51023E+00   0.19160E-02 
c  VelocityY    0.46345E-01     556   0.51023E+00   0.00000E+00 
c  VelocityZ    0.46345E-01     556   0.51023E+00   0.00000E+00 
c  Pressure     0.56593E-01     730   0.12823E-01   0.14250E+00 
c  k            0.15365E-01     224   0.16999E-03   0.58000E-05 
c  epsilon      0.10710E+02     116   0.44306E-03   0.30266E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon      -0.0013587                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1267          1.8271       -0.080173       -0.074667
v  Velocity[Y]                 -1.1475          3.4671         0.28778         0.23896
v  Velocity[Z]                 -2.0045          1.4002         0.11646     -0.00040475
v  ǁVelocityǁ                0.0061312          3.7109         0.61255         0.56328
v  Pressure                    -31.127          3543.6          2748.5          2156.6
v  k                        1.8743e-07         0.20696       0.0058241       0.0062691
v  epsilon                  1.5642e-05          348.77          1.7092          2.0046
v  turbulent_viscosity      9.9414e-08        0.064966       0.0054583       0.0038501
v  CourantNb                   0.24565          1357.2          128.71          88.444
v  FourierNb                     5.841          1248.3          64.392          34.582
v  total_pressure           4.9997e+05      5.0354e+05      5.0275e+05      5.0216e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.7973          1720.2           193.1          123.03


 TIME FOR THE TIME STEP               18:        0.16708E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.460323529E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282807E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71006E+00 0.65532E+00
   Friction velocity        uet   :  0.16963E-01 0.80855E+00
   Friction velocity        uk    :  0.16855E-01 0.80809E+00
   Dimensionless distance   yplus :  0.15990E+00 0.63542E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        111
   Nb of faces within the viscous sub-layer     :       4135
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          3 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.47082E-01     557   0.52093E+00   0.19230E-02 
c  VelocityY    0.47082E-01     557   0.52093E+00   0.00000E+00 
c  VelocityZ    0.47082E-01     557   0.52093E+00   0.00000E+00 
c  Pressure     0.58041E-01     725   0.12242E-01   0.13806E+00 
c  k            0.15389E-01     176   0.20098E-03   0.68641E-05 
c  epsilon      0.11016E+02     118   0.69182E-03   0.39027E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.366          1.8871        -0.07925       -0.075044
v  Velocity[Y]                 -1.1555          3.5778         0.28852         0.23921
v  Velocity[Z]                 -2.2294          1.4572         0.11591     -0.00051216
v  ǁVelocityǁ                0.0061832          3.8849         0.61784          0.5703
v  Pressure                    -36.742          3663.8          2841.3          2223.5
v  k                             7e-08         0.20691       0.0058453       0.0063152
v  epsilon                  1.0038e-05          276.19          1.7417          2.0428
v  turbulent_viscosity      1.3792e-07        0.047534       0.0054095       0.0038303
v  CourantNb                  0.020836          1438.9          129.68          89.369
v  FourierNb                    5.8399          1248.3          64.305          34.551
v  total_pressure           4.9996e+05      5.0366e+05      5.0284e+05      5.0222e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.6536          1760.3          193.98          123.92


 TIME FOR THE TIME STEP               19:        0.16619E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.771273791E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282809E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75068E+00 0.65531E+00
   Friction velocity        uet   :  0.18187E-01 0.80767E+00
   Friction velocity        uk    :  0.18018E-01 0.80718E+00
   Dimensionless distance   yplus :  0.18598E+00 0.64138E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        111
   Nb of faces within the viscous sub-layer     :       4086
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.47691E-01     558   0.51572E+00   0.19893E-02 
c  VelocityY    0.47691E-01     558   0.51572E+00   0.00000E+00 
c  VelocityZ    0.47691E-01     558   0.51572E+00   0.00000E+00 
c  Pressure     0.59793E-01     721   0.11698E-01   0.13457E+00 
c  k            0.15418E-01     213   0.15734E-03   0.40632E-05 
c  epsilon      0.11243E+02     115   0.45681E-03   0.16179E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3977          2.0222       -0.078495       -0.075306
v  Velocity[Y]                 -1.2651          3.6319         0.28924         0.23952
v  Velocity[Z]                 -2.2161          1.5333         0.11568     -0.00063451
v  ǁVelocityǁ                0.0060358          4.1823          0.6227         0.57679
v  Pressure                    -43.246          3780.3          2931.2          2287.8
v  k                        1.8361e-09         0.20695       0.0058527       0.0063425
v  epsilon                  3.5325e-06          275.22          1.7553          2.0618
v  turbulent_viscosity      1.3865e-08         0.04752       0.0053739       0.0038121
v  CourantNb                 0.0041782          1536.5          130.78          90.399
v  FourierNb                    5.8395          1249.7           64.26          34.545
v  total_pressure           4.9996e+05      5.0378e+05      5.0293e+05      5.0229e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           7.082            1812          195.04          124.94


 TIME FOR THE TIME STEP               20:        0.16960E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.328166041E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282811E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80744E+00 0.65900E+00
   Friction velocity        uet   :  0.85545E-02 0.81011E+00
   Friction velocity        uk    :  0.85117E-02 0.80964E+00
   Dimensionless distance   yplus :  0.80752E-01 0.64390E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        117
   Nb of faces within the viscous sub-layer     :       4039
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.48455E-01     560   0.53103E+00   0.21622E-02 
c  VelocityY    0.48455E-01     560   0.53103E+00   0.00000E+00 
c  VelocityZ    0.48455E-01     560   0.53103E+00   0.00000E+00 
c  Pressure     0.61894E-01     702   0.11165E-01   0.13209E+00 
c  k            0.15449E-01     185   0.18976E-03   0.57355E-05 
c  epsilon      0.11572E+02     112   0.50812E-03   0.26662E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6343          2.0718       -0.077789       -0.075717
v  Velocity[Y]                  -1.216          3.7183         0.28996         0.23992
v  Velocity[Z]                 -2.3859          1.5818         0.11541     -0.00070346
v  ǁVelocityǁ                0.0063758          4.1985         0.62791         0.58371
v  Pressure                    -49.395          3893.2          3018.2          2349.8
v  k                         3.272e-08         0.20691       0.0058825       0.0064036
v  epsilon                  7.9212e-07          410.09          1.8028          2.1106
v  turbulent_viscosity      7.5585e-11        0.047536       0.0053312       0.0037883
v  CourantNb                  0.027025          1643.5          131.78          91.333
v  FourierNb                    5.8388          1248.7          64.182          34.513
v  total_pressure           4.9995e+05      5.0389e+05      5.0302e+05      5.0235e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.4403          1863.9          195.96          125.85


 TIME FOR THE TIME STEP               21:        0.16650E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.567872064E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282885E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85770E+00 0.65987E+00
   Friction velocity        uet   :  0.15563E-01 0.80970E+00
   Friction velocity        uk    :  0.16296E-01 0.80920E+00
   Dimensionless distance   yplus :  0.15636E+00 0.64932E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        121
   Nb of faces within the viscous sub-layer     :       3979
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.50657E-01     559   0.55593E+00   0.21090E-02 
c  VelocityY    0.50657E-01     559   0.55593E+00   0.00000E+00 
c  VelocityZ    0.50657E-01     559   0.55593E+00   0.00000E+00 
c  Pressure     0.64238E-01     700   0.10718E-01   0.13022E+00 
c  k            0.15494E-01     195   0.26494E-03   0.64092E-05 
c  epsilon      0.12118E+02     135   0.97122E-03   0.43224E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.8186          2.2037       -0.077119       -0.076008
v  Velocity[Y]                 -1.3274          3.8018         0.29057         0.24028
v  Velocity[Z]                 -2.5844          1.6612         0.11505     -0.00081516
v  ǁVelocityǁ                 0.006039          4.7084          0.6326         0.58996
v  Pressure                    -59.731          4003.3          3102.8          2409.7
v  k                        3.7233e-07         0.20696       0.0058959       0.0064351
v  epsilon                  2.9265e-05          299.62          1.8551          2.1538
v  turbulent_viscosity      1.0704e-07        0.047519       0.0052771       0.0037619
v  CourantNb                  0.087439          1739.5          132.87          92.361
v  FourierNb                    5.8389          1248.6          64.086          34.474
v  total_pressure           4.9994e+05        5.04e+05       5.031e+05      5.0241e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          5.9264          1922.4          196.95          126.84


 TIME FOR THE TIME STEP               22:        0.16684E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.843022719E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282891E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87602E+00 0.66017E+00
   Friction velocity        uet   :  0.12206E-01 0.81386E+00
   Friction velocity        uk    :  0.12044E-01 0.81330E+00
   Dimensionless distance   yplus :  0.15513E+00 0.65921E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        126
   Nb of faces within the viscous sub-layer     :       3940
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.51083E-01     561   0.56915E+00   0.21480E-02 
c  VelocityY    0.51083E-01     561   0.56915E+00   0.00000E+00 
c  VelocityZ    0.51083E-01     561   0.56915E+00   0.00000E+00 
c  Pressure     0.66488E-01     698   0.10401E-01   0.12818E+00 
c  k            0.15536E-01     177   0.20562E-03   0.58967E-05 
c  epsilon      0.12542E+02     106   0.58192E-03   0.33004E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon      -0.0028083                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.8546          2.2399        -0.07643       -0.076276
v  Velocity[Y]                 -1.3291          4.0683         0.29184         0.24083
v  Velocity[Z]                 -2.6469          1.7515         0.11485     -0.00088767
v  ǁVelocityǁ                0.0058323          4.5964         0.63799         0.59679
v  Pressure                    -72.738          4110.7          3185.2          2467.6
v  k                         2.593e-07         0.20691       0.0058775       0.0064589
v  epsilon                  2.0782e-05           350.3          1.8805           2.186
v  turbulent_viscosity      1.8756e-07        0.047538       0.0051662       0.0037163
v  CourantNb                   0.22768          1844.7          133.88          93.308
v  FourierNb                    5.8389          1248.3          63.887          34.417
v  total_pressure           4.9993e+05      5.0411e+05      5.0319e+05      5.0247e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.3965          1976.8          197.76          127.73


 TIME FOR THE TIME STEP               23:        0.16757E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.250580966E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282888E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96589E+00 0.65754E+00
   Friction velocity        uet   :  0.87240E-02 0.82413E+00
   Friction velocity        uk    :  0.12564E-01 0.82357E+00
   Dimensionless distance   yplus :  0.14776E+00 0.67093E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        127
   Nb of faces within the viscous sub-layer     :       3904
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.53152E-01     561   0.59490E+00   0.24093E-02 
c  VelocityY    0.53152E-01     561   0.59490E+00   0.00000E+00 
c  VelocityZ    0.53152E-01     561   0.59490E+00   0.00000E+00 
c  Pressure     0.69248E-01     697   0.10086E-01   0.12713E+00 
c  k            0.15569E-01     193   0.17108E-03   0.45385E-05 
c  epsilon      0.12820E+02     118   0.40268E-03   0.22632E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.6925e-05                             3
a  epsilon      -0.0045409                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9919          2.3856       -0.076053        -0.07647
v  Velocity[Y]                 -1.4115          4.3553         0.29277         0.24132
v  Velocity[Z]                 -2.7674          1.8939         0.11448      -0.0010208
v  ǁVelocityǁ                0.0057839          5.1006         0.64286         0.60288
v  Pressure                    -84.811          4215.9          3266.1          2524.2
v  k                        2.8668e-07         0.20696       0.0059068       0.0064984
v  epsilon                  2.2792e-05          287.55          1.9006          2.2105
v  turbulent_viscosity      2.5623e-07        0.047518       0.0051249       0.0037033
v  CourantNb                  0.010084          1960.2          135.06          94.349
v  FourierNb                    5.8388          1248.4          63.809          34.396
v  total_pressure           4.9992e+05      5.0422e+05      5.0327e+05      5.0252e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.6153          2048.7          198.87          128.74


 TIME FOR THE TIME STEP               24:        0.16758E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.280476432E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282897E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10708E+01 0.65534E+00
   Friction velocity        uet   :  0.11403E-01 0.83386E+00
   Friction velocity        uk    :  0.11354E-01 0.83322E+00
   Dimensionless distance   yplus :  0.15302E+00 0.67331E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        143
   Nb of faces within the viscous sub-layer     :       3875
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.55239E-01     564   0.63379E+00   0.29763E-02 
c  VelocityY    0.55239E-01     564   0.63379E+00   0.00000E+00 
c  VelocityZ    0.55239E-01     564   0.63379E+00   0.00000E+00 
c  Pressure     0.72147E-01     697   0.98312E-02   0.12625E+00 
c  k            0.15632E-01     180   0.28534E-03   0.52780E-05 
c  epsilon      0.13710E+02     114   0.96488E-03   0.87055E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.0509          2.4346       -0.075479        -0.07682
v  Velocity[Y]                 -1.4146          4.6512         0.29419         0.24215
v  Velocity[Z]                 -2.9062          2.0022          0.1142      -0.0010386
v  ǁVelocityǁ                0.0051373           5.016          0.6481         0.60892
v  Pressure                    -93.707          4322.1          3346.1          2580.1
v  k                         2.464e-07         0.20691       0.0059315       0.0065295
v  epsilon                  1.6717e-05          924.37          1.9733          2.2631
v  turbulent_viscosity      2.2061e-07         0.38983       0.0051235       0.0037054
v  CourantNb                    0.2919          2085.7          136.16          95.338
v  FourierNb                    5.8389          1248.4            63.8           34.39
v  total_pressure           4.9991e+05      5.0432e+05      5.0335e+05      5.0258e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.9024          2149.2          199.96          129.73


 TIME FOR THE TIME STEP               25:        0.16708E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.449701703E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282897E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10337E+01 0.65349E+00
   Friction velocity        uet   :  0.16206E-01 0.84889E+00
   Friction velocity        uk    :  0.16065E-01 0.84793E+00
   Dimensionless distance   yplus :  0.14467E+00 0.68391E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        147
   Nb of faces within the viscous sub-layer     :       3835
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          6 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.56884E-01     564   0.65263E+00   0.33082E-02 
c  VelocityY    0.56884E-01     564   0.65263E+00   0.00000E+00 
c  VelocityZ    0.56884E-01     564   0.65263E+00   0.00000E+00 
c  Pressure     0.75245E-01     696   0.96204E-02   0.12577E+00 
c  k            0.15689E-01     189   0.19806E-03   0.64638E-05 
c  epsilon      0.14139E+02     113   0.83805E-03   0.90972E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.2627          2.5643       -0.075232       -0.077207
v  Velocity[Y]                 -1.4216          4.8431         0.29563         0.24299
v  Velocity[Z]                 -2.8482          2.0966         0.11387      -0.0011842
v  ǁVelocityǁ                0.0055139          5.5584         0.65327           0.615
v  Pressure                    -98.017          4430.3          3425.2          2635.4
v  k                        3.4691e-07         0.20696       0.0059733       0.0065838
v  epsilon                  2.3832e-05           317.5          1.9923          2.2971
v  turbulent_viscosity      2.7496e-07        0.047518       0.0051159       0.0037008
v  CourantNb                  0.063828          2199.7          137.35          96.327
v  FourierNb                    5.8389          1248.5          63.793          34.391
v  total_pressure            4.999e+05      5.0443e+05      5.0343e+05      5.0264e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.8791          2263.3          201.15          130.72


 TIME FOR THE TIME STEP               26:        0.16800E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.459385672E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282899E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11347E+01 0.65181E+00
   Friction velocity        uet   :  0.95242E-02 0.86642E+00
   Friction velocity        uk    :  0.95019E-02 0.86541E+00
   Dimensionless distance   yplus :  0.16299E+00 0.68649E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        159
   Nb of faces within the viscous sub-layer     :       3815
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.58532E-01     566   0.63932E+00   0.35632E-02 
c  VelocityY    0.58532E-01     566   0.63932E+00   0.00000E+00 
c  VelocityZ    0.58532E-01     566   0.63932E+00   0.00000E+00 
c  Pressure     0.78013E-01     695   0.93678E-02   0.12460E+00 
c  k            0.15753E-01     184   0.17260E-03   0.33561E-05 
c  epsilon      0.14786E+02     109   0.56912E-03   0.20387E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.3892          2.6129        -0.07468       -0.077598
v  Velocity[Y]                 -1.5545           5.205         0.29717         0.24405
v  Velocity[Z]                 -3.1157          2.1148         0.11342      -0.0011323
v  ǁVelocityǁ                0.0053813          5.5015         0.65835         0.62069
v  Pressure                       -104          4538.1          3504.2          2690.8
v  k                         1.971e-07          0.2069       0.0059848       0.0065966
v  epsilon                  1.2477e-05          356.81          2.0149          2.3156
v  turbulent_viscosity      1.3643e-07        0.047537       0.0051238       0.0037074
v  CourantNb                  0.040655          2344.5          138.58          97.356
v  FourierNb                     5.839          1248.2          63.815            34.4
v  total_pressure            4.999e+05      5.0454e+05       5.035e+05      5.0269e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           6.244          2408.1           202.4          131.76


 TIME FOR THE TIME STEP               27:        0.16692E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.210690512E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282902E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12099E+01 0.68256E+00
   Friction velocity        uet   :  0.14371E-01 0.87975E+00
   Friction velocity        uk    :  0.16486E-01 0.87870E+00
   Dimensionless distance   yplus :  0.16218E+00 0.68868E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        161
   Nb of faces within the viscous sub-layer     :       3800
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          7 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.69084E-01     566   0.76303E+00   0.34232E-02 
c  VelocityY    0.69084E-01     566   0.76303E+00   0.00000E+00 
c  VelocityZ    0.69084E-01     566   0.76303E+00   0.00000E+00 
c  Pressure     0.81571E-01     691   0.92393E-02   0.12441E+00 
c  k            0.15815E-01     205   0.15818E-03   0.25679E-05 
c  epsilon      0.15289E+02     130   0.28967E-03   0.67676E+01 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.4998          2.7625       -0.074484       -0.077915
v  Velocity[Y]                 -1.5115          5.7268         0.29898         0.24498
v  Velocity[Z]                 -3.0735          2.2853         0.11301      -0.0012358
v  ǁVelocityǁ                0.0058574          5.9518         0.66377          0.6267
v  Pressure                    -116.93          4645.4          3583.2            2746
v  k                        3.9328e-07         0.20693       0.0060143       0.0066333
v  epsilon                   1.975e-05          342.09          2.0434          2.3431
v  turbulent_viscosity      2.4661e-07        0.047517       0.0051193       0.0037053
v  CourantNb                  0.018245          2469.8          139.86          98.382
v  FourierNb                     5.839          1248.3          63.807          34.396
v  total_pressure           4.9988e+05      5.0465e+05      5.0358e+05      5.0275e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.5523          2533.5          203.66          132.78


 TIME FOR THE TIME STEP               28:        0.16737E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.805650094E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282903E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13230E+01 0.68016E+00
   Friction velocity        uet   :  0.12600E-01 0.88917E+00
   Friction velocity        uk    :  0.12604E-01 0.88810E+00
   Dimensionless distance   yplus :  0.16442E+00 0.70131E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        166
   Nb of faces within the viscous sub-layer     :       3792
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.60490E-01     571   0.68472E+00   0.33807E-02 
c  VelocityY    0.60490E-01     571   0.68472E+00   0.00000E+00 
c  VelocityZ    0.60490E-01     571   0.68472E+00   0.00000E+00 
c  Pressure     0.85013E-01     690   0.91901E-02   0.12378E+00 
c  k            0.15880E-01     215   0.14710E-03   0.28102E-05 
c  epsilon      0.15909E+02     124   0.28200E-03   0.94565E+01 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon        -0.10971                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.7308          2.7912       -0.074321       -0.078208
v  Velocity[Y]                 -1.6022          5.6444          0.3007         0.24606
v  Velocity[Z]                 -3.1635          2.2964         0.11255      -0.0013065
v  ǁVelocityǁ                0.0054729          6.2334         0.66891         0.63158
v  Pressure                    -129.09            4752          3661.5          2800.8
v  k                        1.8878e-07         0.20688       0.0060199       0.0066472
v  epsilon                  1.3428e-05          334.62           2.079          2.3721
v  turbulent_viscosity      3.8475e-08        0.047534       0.0051069       0.0037026
v  CourantNb                  0.015639          2623.5          141.18          99.437
v  FourierNb                    5.8392          1248.2          63.784          34.391
v  total_pressure           4.9987e+05      5.0475e+05      5.0366e+05       5.028e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.0291          2687.2          204.96          133.83


 TIME FOR THE TIME STEP               29:        0.16943E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.160372123E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282904E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14309E+01 0.69962E+00
   Friction velocity        uet   :  0.14137E-01 0.91566E+00
   Friction velocity        uk    :  0.14112E-01 0.91458E+00
   Dimensionless distance   yplus :  0.18437E+00 0.70238E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        171
   Nb of faces within the viscous sub-layer     :       3770
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.75091E-01     571   0.80334E+00   0.37447E-02 
c  VelocityY    0.75091E-01     571   0.80334E+00   0.00000E+00 
c  VelocityZ    0.75091E-01     571   0.80334E+00   0.00000E+00 
c  Pressure     0.88796E-01     680   0.90143E-02   0.12357E+00 
c  k            0.15972E-01     224   0.24212E-03   0.40759E-05 
c  epsilon      0.16640E+02     151   0.93657E-03   0.33413E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.8576          2.9593       -0.074149       -0.078365
v  Velocity[Y]                 -1.5283          5.9788         0.30227         0.24702
v  Velocity[Z]                 -3.5077          2.4594         0.11213      -0.0014832
v  ǁVelocityǁ                0.0032358          6.4874         0.67439         0.63775
v  Pressure                    -140.25          4884.3          3739.3          2855.1
v  k                        3.8856e-07         0.20694       0.0060595       0.0066876
v  epsilon                  5.8523e-05          388.42          2.1338          2.4175
v  turbulent_viscosity       2.102e-07        0.047513       0.0050863       0.0036954
v  CourantNb                  0.077971          2763.6          142.52          100.41
v  FourierNb                    5.8391          1248.2          63.747          34.381
v  total_pressure           4.9986e+05      5.0488e+05      5.0374e+05      5.0286e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.8702          2827.4          206.27          134.79


 TIME FOR THE TIME STEP               30:        0.16968E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.624784240E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282901E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15008E+01 0.69456E+00
   Friction velocity        uet   :  0.17111E-01 0.93179E+00
   Friction velocity        uk    :  0.17080E-01 0.93063E+00
   Dimensionless distance   yplus :  0.13616E+00 0.73092E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        182
   Nb of faces within the viscous sub-layer     :       3740
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.78624E-01     574   0.81396E+00   0.38884E-02 
c  VelocityY    0.78624E-01     574   0.81396E+00   0.00000E+00 
c  VelocityZ    0.78624E-01     574   0.81396E+00   0.00000E+00 
c  Pressure     0.92509E-01     675   0.90013E-02   0.12289E+00 
c  k            0.16064E-01     220   0.26293E-03   0.47691E-05 
c  epsilon      0.17638E+02     120   0.81641E-03   0.32335E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.9191e-06                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -4.1874          3.0009       -0.073829       -0.078475
v  Velocity[Y]                 -1.6804          5.6862         0.30416         0.24798
v  Velocity[Z]                 -3.5926          2.5153         0.11169      -0.0015526
v  ǁVelocityǁ                0.0047954          6.2764         0.67923         0.64246
v  Pressure                    -150.08          5040.1          3817.1          2909.3
v  k                        1.5489e-07         0.20689        0.006053       0.0067099
v  epsilon                  1.3594e-05          356.74          2.1661          2.4502
v  turbulent_viscosity      1.0298e-07        0.047534       0.0050348       0.0036778
v  CourantNb                   0.16768          2918.9          143.92          101.51
v  FourierNb                    5.8392          1248.3          63.654          34.352
v  total_pressure           4.9985e+05      5.0504e+05      5.0382e+05      5.0291e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.7813          2982.7          207.57          135.86


 TIME FOR THE TIME STEP               31:        0.16804E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.263951348E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282906E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17010E+01 0.72102E+00
   Friction velocity        uet   :  0.20293E-01 0.95517E+00
   Friction velocity        uk    :  0.20097E-01 0.95400E+00
   Dimensionless distance   yplus :  0.16213E+00 0.73870E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        182
   Nb of faces within the viscous sub-layer     :       3730
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.84850E-01     572   0.83885E+00   0.43116E-02 
c  VelocityY    0.84850E-01     572   0.83885E+00   0.00000E+00 
c  VelocityZ    0.84850E-01     572   0.83885E+00   0.00000E+00 
c  Pressure     0.96793E-01     666   0.88373E-02   0.12264E+00 
c  k            0.16165E-01     218   0.14734E-03   0.33950E-05 
c  epsilon      0.18461E+02     109   0.28640E-03   0.12506E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -4.3612          3.1821       -0.074061       -0.078829
v  Velocity[Y]                  -1.662           6.682          0.3061         0.24904
v  Velocity[Z]                 -3.6372          2.6653         0.11129      -0.0015634
v  ǁVelocityǁ                0.0045174          6.9981         0.68497         0.64797
v  Pressure                    -161.15          5198.8          3894.8          2963.2
v  k                        2.7728e-07         0.20692        0.006086       0.0067354
v  epsilon                   2.704e-05          384.79          2.2031          2.4789
v  turbulent_viscosity      8.1556e-08        0.047515       0.0049999       0.0036625
v  CourantNb                   0.11229          3122.6          145.33          102.54
v  FourierNb                    5.8389          1248.3          63.594          34.332
v  total_pressure           4.9984e+05       5.052e+05      5.0389e+05      5.0296e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.9155          3187.1          208.93          136.87


 TIME FOR THE TIME STEP               32:        0.16706E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.794291911E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283035E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17575E+01 0.71337E+00
   Friction velocity        uet   :  0.14491E-01 0.97277E+00
   Friction velocity        uk    :  0.14445E-01 0.97150E+00
   Dimensionless distance   yplus :  0.14630E+00 0.77154E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        197
   Nb of faces within the viscous sub-layer     :       3716
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.81964E-01     578   0.81993E+00   0.55386E-02 
c  VelocityY    0.81964E-01     578   0.81993E+00   0.00000E+00 
c  VelocityZ    0.81964E-01     578   0.81993E+00   0.00000E+00 
c  Pressure     0.10133E+00     665   0.88476E-02   0.12241E+00 
c  k            0.16254E-01     204   0.14995E-03   0.31384E-05 
c  epsilon      0.19230E+02     106   0.28139E-03   0.11549E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -4.6696          3.2421       -0.073884       -0.078965
v  Velocity[Y]                  -1.734          6.1928         0.30762         0.25008
v  Velocity[Z]                 -3.9198           2.703          0.1111      -0.0016933
v  ǁVelocityǁ                 0.003199          6.9368         0.69002         0.65304
v  Pressure                    -171.76          5364.4          3973.6            3018
v  k                        5.6543e-08         0.20687       0.0060981       0.0067588
v  epsilon                   1.416e-05          368.24          2.2283          2.5034
v  turbulent_viscosity      7.5871e-09        0.047532       0.0049936       0.0036624
v  CourantNb                 0.0065898          3352.3          146.92          103.66
v  FourierNb                    5.8392          1248.2          63.574          34.325
v  total_pressure           4.9983e+05      5.0536e+05      5.0397e+05      5.0302e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.2696          3416.9          210.49          137.98


 TIME FOR THE TIME STEP               33:        0.16908E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.177286908E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283044E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19312E+01 0.73107E+00
   Friction velocity        uet   :  0.11791E-01 0.98616E+00
   Friction velocity        uk    :  0.11760E-01 0.98489E+00
   Dimensionless distance   yplus :  0.11801E+00 0.78580E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        201
   Nb of faces within the viscous sub-layer     :       3693
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10360E+00     579   0.88465E+00   0.50253E-02 
c  VelocityY    0.10360E+00     579   0.88465E+00   0.00000E+00 
c  VelocityZ    0.10360E+00     579   0.88465E+00   0.00000E+00 
c  Pressure     0.10575E+00     662   0.86675E-02   0.12196E+00 
c  k            0.16376E-01     196   0.14335E-03   0.31682E-05 
c  epsilon      0.20410E+02     106   0.23104E-03   0.15935E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -4.9436           3.403       -0.073757       -0.079015
v  Velocity[Y]                 -1.8349          7.3304         0.31001         0.25132
v  Velocity[Z]                 -3.9823          2.8126         0.11046      -0.0017445
v  ǁVelocityǁ                0.0047185          7.6132         0.69559         0.65807
v  Pressure                    -183.91          5533.5          4052.1          3072.3
v  k                        4.3178e-08         0.20693       0.0061462       0.0067983
v  epsilon                   2.865e-05          388.04          2.2858          2.5473
v  turbulent_viscosity      3.7658e-10        0.047512       0.0049972       0.0036683
v  CourantNb                  0.014524          3708.7          148.39          104.77
v  FourierNb                      5.84          1248.2          63.581          34.345
v  total_pressure           4.9982e+05      5.0553e+05      5.0405e+05      5.0307e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.4325          3773.3          211.97          139.11


 TIME FOR THE TIME STEP               34:        0.16767E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.244474884E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283018E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24260E+01 0.73494E+00
   Friction velocity        uet   :  0.97209E-02 0.10048E+01
   Friction velocity        uk    :  0.97021E-02 0.10032E+01
   Dimensionless distance   yplus :  0.10124E+00 0.82578E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        210
   Nb of faces within the viscous sub-layer     :       3676
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10063E+00     595   0.87188E+00   0.60532E-02 
c  VelocityY    0.10063E+00     595   0.87188E+00   0.00000E+00 
c  VelocityZ    0.10063E+00     595   0.87188E+00   0.00000E+00 
c  Pressure     0.11069E+00     662   0.87078E-02   0.12169E+00 
c  k            0.16514E-01     185   0.15613E-03   0.33285E-05 
c  epsilon      0.21273E+02     100   0.25193E-03   0.14515E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.3764e-07                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -5.2461          3.5158       -0.074298       -0.079462
v  Velocity[Y]                 -1.7603          6.7787         0.31211          0.2526
v  Velocity[Z]                 -4.2521          2.9625         0.11018      -0.0018262
v  ǁVelocityǁ                0.0045375           7.365         0.70118         0.66338
v  Pressure                     -195.5          5709.5          4131.6          3127.1
v  k                        1.3764e-07         0.20687       0.0061684        0.006818
v  epsilon                  2.8582e-05          390.19          2.3155          2.5736
v  turbulent_viscosity      8.9486e-10        0.047533       0.0050141       0.0036735
v  CourantNb                   0.26733          3998.5          150.08          105.92
v  FourierNb                    5.8392          1248.2           63.61          34.341
v  total_pressure            4.998e+05      5.0571e+05      5.0413e+05      5.0313e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.8998          4063.1          213.69          140.26


 TIME FOR THE TIME STEP               35:        0.16976E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.363694772E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283016E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28000E+01 0.75044E+00
   Friction velocity        uet   :  0.38555E-02 0.10304E+01
   Friction velocity        uk    :  0.38462E-02 0.10287E+01
   Dimensionless distance   yplus :  0.59247E-01 0.82753E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        212
   Nb of faces within the viscous sub-layer     :       3648
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.12777E+00     606   0.92076E+00   0.60028E-02 
c  VelocityY    0.12777E+00     606   0.92076E+00   0.00000E+00 
c  VelocityZ    0.12777E+00     606   0.92076E+00   0.00000E+00 
c  Pressure     0.11597E+00     660   0.85871E-02   0.12154E+00 
c  k            0.16674E-01     186   0.16185E-03   0.47572E-05 
c  epsilon      0.22761E+02     105   0.24650E-03   0.25677E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.3934e-07                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -5.5903          3.6899       -0.074551       -0.079625
v  Velocity[Y]                 -1.9579          8.0788         0.31424         0.25366
v  Velocity[Z]                 -4.4215          3.0963         0.10967      -0.0020595
v  ǁVelocityǁ                0.0050831          8.2888         0.70711         0.66858
v  Pressure                    -206.97          5890.1          4210.8          3181.6
v  k                        3.8627e-08         0.20693       0.0062218       0.0068625
v  epsilon                  3.3858e-05          405.17          2.4006           2.634
v  turbulent_viscosity       3.088e-09        0.047512       0.0050148        0.003668
v  CourantNb                   0.17453            4454          151.71           107.1
v  FourierNb                    5.8395          1248.2          63.617          34.343
v  total_pressure           4.9979e+05      5.0589e+05      5.0421e+05      5.0318e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.0353          4518.7          215.33          141.45


 TIME FOR THE TIME STEP               36:        0.17259E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.112433830E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283004E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33453E+01 0.75751E+00
   Friction velocity        uet   :  0.13054E-01 0.10436E+01
   Friction velocity        uk    :  0.12980E-01 0.10419E+01
   Dimensionless distance   yplus :  0.90155E-01 0.88742E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        217
   Nb of faces within the viscous sub-layer     :       3625
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.91554E-01     659   0.83315E+00   0.62295E-02 
c  VelocityY    0.91554E-01     659   0.83315E+00   0.00000E+00 
c  VelocityZ    0.91554E-01     659   0.83315E+00   0.00000E+00 
c  Pressure     0.12269E+00     660   0.86557E-02   0.12240E+00 
c  k            0.16863E-01     183   0.14305E-03   0.46012E-05 
c  epsilon      0.24017E+02     107   0.17997E-03   0.19928E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -3.256e-07                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -5.9186          3.7986       -0.075278       -0.079967
v  Velocity[Y]                 -2.0243          7.4536         0.31643         0.25482
v  Velocity[Z]                 -4.6513          3.1643         0.10954      -0.0021991
v  ǁVelocityǁ                0.0047718          8.2531          0.7127         0.67351
v  Pressure                    -217.95          6078.7            4291            3237
v  k                        4.4404e-08         0.20686       0.0062183       0.0068776
v  epsilon                  1.5455e-05          412.85          2.4059          2.6517
v  turbulent_viscosity      3.8447e-11        0.047533       0.0050041       0.0036624
v  CourantNb                   0.28218          4784.1          153.58          108.35
v  FourierNb                    5.8421          1248.2          63.589          34.331
v  total_pressure           4.9978e+05      5.0608e+05      5.0429e+05      5.0324e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.3669            4849          217.17          142.68


 TIME FOR THE TIME STEP               37:        0.18029E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.999837691E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283015E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34569E+01 0.77140E+00
   Friction velocity        uet   :  0.16662E-01 0.10740E+01
   Friction velocity        uk    :  0.16544E-01 0.10723E+01
   Dimensionless distance   yplus :  0.11490E+00 0.87309E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        224
   Nb of faces within the viscous sub-layer     :       3610
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.18264E+00     652   0.95687E+00   0.70972E-02 
c  VelocityY    0.18264E+00     652   0.95687E+00   0.00000E+00 
c  VelocityZ    0.18264E+00     652   0.95687E+00   0.00000E+00 
c  Pressure     0.12928E+00     659   0.85448E-02   0.12290E+00 
c  k            0.17061E-01     183   0.14265E-03   0.50122E-05 
c  epsilon      0.25557E+02     112   0.24797E-03   0.30147E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.2497e-07                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -6.3753           3.981       -0.075515       -0.080406
v  Velocity[Y]                 -2.3095          8.9524         0.31861         0.25629
v  Velocity[Z]                 -4.9661          3.3307         0.10861      -0.0023577
v  ǁVelocityǁ                 0.002768          9.1174         0.71936         0.67949
v  Pressure                    -228.55          6274.4          4372.9          3293.2
v  k                        9.7475e-08         0.20692       0.0062685       0.0069104
v  epsilon                  5.0901e-05          435.78           2.487          2.7022
v  turbulent_viscosity      5.0956e-09         0.04751       0.0049963       0.0036538
v  CourantNb                   0.12029          5218.7          155.39          109.65
v  FourierNb                    5.8399          1248.3          63.583          34.333
v  total_pressure           4.9977e+05      5.0627e+05      5.0437e+05      5.0329e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.4832          5283.7          218.97          143.98


 TIME FOR THE TIME STEP               38:        0.17769E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.445737275E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283019E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39121E+01 0.78003E+00
   Friction velocity        uet   :  0.13050E-01 0.10880E+01
   Friction velocity        uk    :  0.12960E-01 0.10860E+01
   Dimensionless distance   yplus :  0.77354E-01 0.91932E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        236
   Nb of faces within the viscous sub-layer     :       3573
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.17305E+00     719   0.95165E+00   0.74836E-02 
c  VelocityY    0.17305E+00     719   0.95165E+00   0.00000E+00 
c  VelocityZ    0.17305E+00     719   0.95165E+00   0.00000E+00 
c  Pressure     0.13471E+00     658   0.86167E-02   0.12188E+00 
c  k            0.17335E-01     204   0.15412E-03   0.52646E-05 
c  epsilon      0.27232E+02     108   0.21035E-03   0.24241E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.5562e-07                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -6.5823          4.1506       -0.076022       -0.080547
v  Velocity[Y]                 -2.8511          8.2416         0.32166         0.25801
v  Velocity[Z]                 -5.2166          3.4694         0.10871       -0.002203
v  ǁVelocityǁ                0.0023974          8.8637         0.72532         0.68465
v  Pressure                    -239.01          6478.5          4456.2          3350.3
v  k                        9.5291e-08         0.20685       0.0062972       0.0069513
v  epsilon                  2.6741e-05           431.5          2.5383          2.7513
v  turbulent_viscosity      3.4027e-10        0.047531       0.0049905       0.0036525
v  CourantNb                  0.032791          5694.2          157.41          111.02
v  FourierNb                    5.8503          1248.7          63.581          34.332
v  total_pressure           4.9976e+05      5.0648e+05      5.0446e+05      5.0335e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           7.509          5759.2          220.99          145.35


 TIME FOR THE TIME STEP               39:        0.18873E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.306110759E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283029E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49757E+01 0.80579E+00
   Friction velocity        uet   :  0.15211E-01 0.11018E+01
   Friction velocity        uk    :  0.15077E-01 0.10999E+01
   Dimensionless distance   yplus :  0.10348E+00 0.93574E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        245
   Nb of faces within the viscous sub-layer     :       3560
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.19993E+00     726   0.96027E+00   0.93659E-02 
c  VelocityY    0.19993E+00     726   0.96027E+00   0.00000E+00 
c  VelocityZ    0.19993E+00     726   0.96027E+00   0.00000E+00 
c  Pressure     0.14154E+00     657   0.84680E-02   0.12185E+00 
c  k            0.17614E-01     210   0.12763E-03   0.43287E-05 
c  epsilon      0.29013E+02     102   0.17806E-03   0.24004E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.8646e-07                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -7.155          4.3648       -0.076818        -0.08087
v  Velocity[Y]                 -2.9017          10.164         0.32409         0.25935
v  Velocity[Z]                 -5.3295          3.5749         0.10789      -0.0026838
v  ǁVelocityǁ                0.0017234            10.4         0.73282         0.69114
v  Pressure                    -248.97          6690.7          4541.4          3408.8
v  k                        4.4231e-07         0.20691       0.0063132       0.0069577
v  epsilon                  5.5664e-05          489.46          2.5918          2.7839
v  turbulent_viscosity      1.9555e-08        0.047509       0.0049656       0.0036378
v  CourantNb                  0.040267          6144.5          159.42          112.39
v  FourierNb                    5.8499            1249          63.544           34.32
v  total_pressure           4.9975e+05      5.0669e+05      5.0454e+05      5.0341e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.8433          6209.7          222.96          146.71


 TIME FOR THE TIME STEP               40:        0.18977E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.653709588E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283035E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47698E+01 0.81270E+00
   Friction velocity        uet   :  0.14609E-01 0.11373E+01
   Friction velocity        uk    :  0.14528E-01 0.11353E+01
   Dimensionless distance   yplus :  0.16054E+00 0.95950E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        256
   Nb of faces within the viscous sub-layer     :       3545
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.17101E+00     814   0.94205E+00   0.10818E-01 
c  VelocityY    0.17101E+00     814   0.94205E+00   0.00000E+00 
c  VelocityZ    0.17101E+00     814   0.94205E+00   0.00000E+00 
c  Pressure     0.14860E+00     654   0.85258E-02   0.12156E+00 
c  k            0.17956E-01     188   0.16754E-03   0.60529E-05 
c  epsilon      0.30811E+02     131   0.17590E-03   0.24986E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.9651e-07                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -7.402          4.5139       -0.077363       -0.080953
v  Velocity[Y]                 -3.3331          9.0543         0.32669         0.26086
v  Velocity[Z]                 -5.7222          3.6103         0.10827      -0.0025613
v  ǁVelocityǁ                0.0026232          9.9782           0.739         0.69566
v  Pressure                    -258.31          6911.5          4627.7          3467.7
v  k                        1.2787e-08         0.20684       0.0063563       0.0070062
v  epsilon                  2.3772e-05          478.34           2.665           2.847
v  turbulent_viscosity       1.808e-08         0.04753       0.0049429       0.0036289
v  CourantNb                 0.0034413          6490.7          161.69           113.9
v  FourierNb                    5.8546          1249.2          63.493          34.301
v  total_pressure           4.9974e+05      5.0691e+05      5.0463e+05      5.0347e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.0275            6556          225.18           148.2


 TIME FOR THE TIME STEP               41:        0.20230E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.102619828E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283049E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60555E+01 0.82328E+00
   Friction velocity        uet   :  0.13008E-01 0.11648E+01
   Friction velocity        uk    :  0.12998E-01 0.11627E+01
   Dimensionless distance   yplus :  0.12541E+00 0.97060E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        254
   Nb of faces within the viscous sub-layer     :       3553
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.25456E+00     809   0.97200E+00   0.12320E-01 
c  VelocityY    0.25456E+00     809   0.97200E+00   0.00000E+00 
c  VelocityZ    0.25456E+00     809   0.97200E+00   0.00000E+00 
c  Pressure     0.15616E+00     652   0.83781E-02   0.12146E+00 
c  k            0.18360E-01     218   0.12333E-03   0.47995E-05 
c  epsilon      0.33269E+02     123   0.14322E-03   0.23715E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.0734e-05                             3
a  epsilon       -0.015463                             4


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -8.0763          4.7293       -0.078621       -0.081136
v  Velocity[Y]                   -3.34          10.988          0.3289         0.26225
v  Velocity[Z]                  -5.857          3.7698         0.10719      -0.0029533
v  ǁVelocityǁ               0.00096519          11.172         0.74668         0.70157
v  Pressure                    -266.79          7139.9          4714.9          3527.2
v  k                        9.8599e-08         0.20691       0.0063337        0.006985
v  epsilon                  9.7888e-06          507.23          2.7053          2.8643
v  turbulent_viscosity      1.8736e-10        0.047508       0.0049035       0.0036143
v  CourantNb                   0.14173          7088.1          163.88          115.28
v  FourierNb                    5.8548          1248.2           63.42          34.272
v  total_pressure           4.9973e+05      5.0714e+05      5.0471e+05      5.0353e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.1721          7153.5           227.3          149.55


 TIME FOR THE TIME STEP               42:        0.20037E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.121219017E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283046E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63840E+01 0.83280E+00
   Friction velocity        uet   :  0.17681E-01 0.11543E+01
   Friction velocity        uk    :  0.17454E-01 0.11521E+01
   Dimensionless distance   yplus :  0.17235E+00 0.99640E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        265
   Nb of faces within the viscous sub-layer     :       3542
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.16564E+00     924   0.93163E+00   0.10933E-01 
c  VelocityY    0.16564E+00     924   0.93163E+00   0.00000E+00 
c  VelocityZ    0.16564E+00     924   0.93163E+00   0.00000E+00 
c  Pressure     0.16314E+00     641   0.84635E-02   0.12046E+00 
c  k            0.18867E-01     208   0.16566E-03   0.52942E-05 
c  epsilon      0.35799E+02     109   0.16974E-03   0.24431E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -8.284          4.9342       -0.078503       -0.081084
v  Velocity[Y]                 -3.8855          10.692          0.3324         0.26415
v  Velocity[Z]                 -6.2801          3.9357         0.10792      -0.0029046
v  ǁVelocityǁ                0.0009044          11.735         0.75308         0.70664
v  Pressure                    -274.96          7376.3          4804.2            3588
v  k                        3.6797e-08         0.20684       0.0063922       0.0070275
v  epsilon                   2.159e-05          521.58          2.7748          2.9212
v  turbulent_viscosity      2.0932e-08        0.047529       0.0048788       0.0035989
v  CourantNb                  0.062863          7501.2          166.31          116.82
v  FourierNb                    5.8566          1248.2          63.375          34.254
v  total_pressure           4.9973e+05      5.0738e+05       5.048e+05      5.0359e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.0074          7566.8          229.68          151.07


 TIME FOR THE TIME STEP               43:        0.21689E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.109877809E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283271E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.82814E+01 0.84518E+00
   Friction velocity        uet   :  0.11366E-01 0.11639E+01
   Friction velocity        uk    :  0.11360E-01 0.11617E+01
   Dimensionless distance   yplus :  0.10960E+00 0.10224E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        271
   Nb of faces within the viscous sub-layer     :       3538
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.36092E+00     873   0.98259E+00   0.14524E-01 
c  VelocityY    0.36092E+00     873   0.98259E+00   0.00000E+00 
c  VelocityZ    0.36092E+00     873   0.98259E+00   0.00000E+00 
c  Pressure     0.17198E+00     639   0.83273E-02   0.12061E+00 
c  k            0.19388E-01     183   0.14982E-03   0.60297E-05 
c  epsilon      0.38217E+02     131   0.15087E-03   0.28308E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.0356e-06                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -9.1421          5.2594       -0.079496       -0.081449
v  Velocity[Y]                 -4.0518          11.957         0.33424         0.26569
v  Velocity[Z]                 -6.7819          4.2087          0.1064       -0.003357
v  ǁVelocityǁ                0.0018798          12.139         0.76058         0.71226
v  Pressure                    -284.78          7624.9          4892.7          3648.1
v  k                        2.1625e-07         0.20691       0.0064032       0.0070349
v  epsilon                  1.6433e-05          575.77          2.8284          2.9512
v  turbulent_viscosity      2.3304e-09        0.047507       0.0048714        0.003594
v  CourantNb                  0.099474          8097.1          168.75          118.36
v  FourierNb                    5.8565          1248.2          63.369          34.258
v  total_pressure           4.9972e+05      5.0762e+05      5.0489e+05      5.0365e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.5342          8162.9          232.11          152.62


 TIME FOR THE TIME STEP               44:        0.20826E+01

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


 INSTANT    0.450000000E+01   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.762035838E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283254E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66630E+01 0.84819E+00
   Friction velocity        uet   :  0.14064E-01 0.11681E+01
   Friction velocity        uk    :  0.14029E-01 0.11660E+01
   Dimensionless distance   yplus :  0.19395E+00 0.10300E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        286
   Nb of faces within the viscous sub-layer     :       3537
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.36496E+00     980   0.98596E+00   0.13635E-01 
c  VelocityY    0.36496E+00     980   0.98596E+00   0.00000E+00 
c  VelocityZ    0.36496E+00     980   0.98596E+00   0.00000E+00 
c  Pressure     0.18096E+00     629   0.84652E-02   0.12032E+00 
c  k            0.20129E-01     205   0.14351E-03   0.49428E-05 
c  epsilon      0.41459E+02     122   0.13448E-03   0.25078E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -9.3814          5.4194       -0.080539       -0.081756
v  Velocity[Y]                 -4.6002          11.956         0.33853         0.26746
v  Velocity[Z]                 -7.0382          4.2844         0.10657      -0.0030225
v  ǁVelocityǁ                0.0024103           12.06         0.76852         0.71759
v  Pressure                    -296.34          7883.9          4982.2          3708.3
v  k                        3.1246e-07         0.20683       0.0064228       0.0070516
v  epsilon                  7.1268e-05          553.03          2.9011          3.0077
v  turbulent_viscosity      7.5356e-10        0.047529       0.0048438       0.0035808
v  CourantNb                  0.011763          8808.9          171.29          119.93
v  FourierNb                    5.8553          1248.2          63.312          34.234
v  total_pressure            4.997e+05      5.0788e+05      5.0498e+05      5.0371e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.1858          8874.7          234.61          154.16


 TIME FOR THE TIME STEP               45:        0.22248E+01

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


 INSTANT    0.460000000E+01   TIME STEP NUMBER              46
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.169493807E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283243E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10273E+02 0.85241E+00
   Friction velocity        uet   :  0.15381E-01 0.11989E+01
   Friction velocity        uk    :  0.15349E-01 0.11941E+01
   Dimensionless distance   yplus :  0.20823E+00 0.10811E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        292
   Nb of faces within the viscous sub-layer     :       3524
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.42514E+00     948   0.98743E+00   0.16783E-01 
c  VelocityY    0.42514E+00     948   0.98743E+00   0.00000E+00 
c  VelocityZ    0.42514E+00     948   0.98743E+00   0.00000E+00 
c  Pressure     0.19096E+00     629   0.82559E-02   0.12057E+00 
c  k            0.20905E-01     197   0.12503E-03   0.70831E-05 
c  epsilon      0.45276E+02     106   0.13298E-03   0.54111E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -10.387          5.7377       -0.081978       -0.082258
v  Velocity[Y]                 -4.6333          13.603         0.34044         0.26902
v  Velocity[Z]                  -7.168          4.5611         0.10587      -0.0038154
v  ǁVelocityǁ                0.0037034          13.789         0.77803         0.72471
v  Pressure                    -307.12          8153.5          5076.6          3772.4
v  k                        2.1703e-07          0.2069       0.0064678       0.0070796
v  epsilon                  6.2484e-05          617.26          2.9877          3.0678
v  turbulent_viscosity      1.1646e-08        0.047505       0.0048366       0.0035726
v  CourantNb                  0.035576          9461.6          174.03          121.63
v  FourierNb                    5.8543          1248.2           63.31           34.23
v  total_pressure           4.9969e+05      5.0815e+05      5.0508e+05      5.0377e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.5881          9527.6          237.34          155.86


 TIME FOR THE TIME STEP               46:        0.21927E+01

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


 INSTANT    0.470000000E+01   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.105275674E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283267E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97596E+01 0.85575E+00
   Friction velocity        uet   :  0.14622E-01 0.12450E+01
   Friction velocity        uk    :  0.14588E-01 0.12403E+01
   Dimensionless distance   yplus :  0.21780E+00 0.10792E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        306
   Nb of faces within the viscous sub-layer     :       3508
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.37015E+00    1107   0.98114E+00   0.19436E-01 
c  VelocityY    0.37015E+00    1107   0.98114E+00   0.00000E+00 
c  VelocityZ    0.37015E+00    1107   0.98114E+00   0.00000E+00 
c  Pressure     0.19867E+00     628   0.83167E-02   0.11887E+00 
c  k            0.21982E-01     207   0.15889E-03   0.73546E-05 
c  epsilon      0.49247E+02     129   0.13169E-03   0.41913E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -10.529          6.0417       -0.082577       -0.082609
v  Velocity[Y]                 -5.2283          13.021         0.34515          0.2714
v  Velocity[Z]                 -7.8895          4.6584         0.10619      -0.0034655
v  ǁVelocityǁ                0.0028686          14.319         0.78627         0.73016
v  Pressure                    -318.33          8434.8          5171.7          3836.6
v  k                        4.3791e-07         0.20682       0.0065406       0.0071283
v  epsilon                  7.8876e-05          618.74          3.0886          3.1365
v  turbulent_viscosity      5.8851e-11        0.047527       0.0048529       0.0035787
v  CourantNb                   0.09112          9946.6          177.12           123.5
v  FourierNb                    5.8543          1248.2           63.33          34.231
v  total_pressure           4.9968e+05      5.0843e+05      5.0517e+05      5.0384e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.0193           10013          240.45          157.73


 TIME FOR THE TIME STEP               47:        0.24052E+01

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


 INSTANT    0.480000000E+01   TIME STEP NUMBER              48
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.194260761E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283268E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11912E+02 0.85355E+00
   Friction velocity        uet   :  0.14027E-01 0.12761E+01
   Friction velocity        uk    :  0.13984E-01 0.12705E+01
   Dimensionless distance   yplus :  0.18365E+00 0.11201E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        316
   Nb of faces within the viscous sub-layer     :       3494
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.52764E+00    1048   0.98972E+00   0.22802E-01 
c  VelocityY    0.52764E+00    1048   0.98972E+00   0.00000E+00 
c  VelocityZ    0.52764E+00    1048   0.98972E+00   0.00000E+00 
c  Pressure     0.21157E+00     626   0.81872E-02   0.12008E+00 
c  k            0.23156E-01     201   0.12887E-03   0.77488E-05 
c  epsilon      0.53342E+02     116   0.10925E-03   0.33201E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -11.658          6.3322       -0.084558       -0.083111
v  Velocity[Y]                 -5.5152          15.093         0.34788         0.27338
v  Velocity[Z]                 -8.0838          4.9081         0.10462      -0.0039459
v  ǁVelocityǁ                0.0031243          15.277         0.79463          0.7355
v  Pressure                    -328.43          8729.4          5270.6          3903.4
v  k                        5.5294e-07         0.20689       0.0065547        0.007141
v  epsilon                   5.106e-05          658.31          3.1491          3.1843
v  turbulent_viscosity      2.4392e-08        0.047504       0.0048401       0.0035758
v  CourantNb                   0.01529           10688          180.07          125.32
v  FourierNb                    5.8541          1248.2          63.302          34.218
v  total_pressure           4.9967e+05      5.0873e+05      5.0527e+05       5.039e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.9437           10754          243.37          159.54


 TIME FOR THE TIME STEP               48:        0.23336E+01

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


 INSTANT    0.490000000E+01   TIME STEP NUMBER              49
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.135961130E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283266E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12108E+02 0.84965E+00
   Friction velocity        uet   :  0.59805E-02 0.13576E+01
   Friction velocity        uk    :  0.59613E-02 0.13514E+01
   Dimensionless distance   yplus :  0.78290E-01 0.11241E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        331
   Nb of faces within the viscous sub-layer     :       3483
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.31602E+00    1236   0.97299E+00   0.19995E-01 
c  VelocityY    0.31602E+00    1236   0.97299E+00   0.00000E+00 
c  VelocityZ    0.31602E+00    1236   0.97299E+00   0.00000E+00 
c  Pressure     0.22225E+00     625   0.82704E-02   0.11958E+00 
c  k            0.24674E-01     180   0.14505E-03   0.93071E-05 
c  epsilon      0.57841E+02     104   0.13699E-03   0.39152E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -11.936          6.5977       -0.086192       -0.083641
v  Velocity[Y]                 -6.2739          14.458         0.35305         0.27577
v  Velocity[Z]                 -8.6647          5.1197         0.10454      -0.0040543
v  ǁVelocityǁ                0.0032234          15.889         0.80526         0.74318
v  Pressure                    -340.95          9038.3          5373.7            3973
v  k                        1.3346e-07         0.20681       0.0066023       0.0071628
v  epsilon                  7.2577e-05          683.18          3.2733          3.2558
v  turbulent_viscosity      3.5365e-09        0.051812       0.0048141       0.0035589
v  CourantNb                 0.0056192           11367          183.18          127.15
v  FourierNb                    5.8543          1248.5          63.264          34.205
v  total_pressure           4.9966e+05      5.0904e+05      5.0537e+05      5.0397e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.1065           11434          246.44          161.35


 TIME FOR THE TIME STEP               49:        0.25755E+01

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


 INSTANT    0.500000000E+01   TIME STEP NUMBER              50
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.130999576E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283262E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14517E+02 0.83503E+00
   Friction velocity        uet   :  0.10311E-01 0.14240E+01
   Friction velocity        uk    :  0.10239E-01 0.14175E+01
   Dimensionless distance   yplus :  0.15529E+00 0.11780E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        341
   Nb of faces within the viscous sub-layer     :       3479
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82


 Write intermediate restart files
   checkpoint at iteration         50, Physical time    0.50000E+01


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

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

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

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


 Time for restart files:    0.10187E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.78716E+00    1157   0.99332E+00   0.25572E-01 
c  VelocityY    0.78716E+00    1157   0.99332E+00   0.00000E+00 
c  VelocityZ    0.78716E+00    1157   0.99332E+00   0.00000E+00 
c  Pressure     0.23354E+00     624   0.82058E-02   0.11916E+00 
c  k            0.26416E-01     176   0.11073E-03   0.92111E-05 
c  epsilon      0.63888E+02      94   0.10876E-03   0.36055E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8558e-05                             1
a  epsilon     -0.00084417                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -13.236          6.8325       -0.088686       -0.084183
v  Velocity[Y]                 -6.5197          13.894         0.35454         0.27745
v  Velocity[Z]                 -9.2599          5.5185         0.10495      -0.0048406
v  ǁVelocityǁ                0.0074641           16.56         0.81669         0.75065
v  Pressure                    -352.93          9367.1          5478.6          4043.9
v  k                        1.1317e-06         0.20688       0.0066476        0.007202
v  epsilon                  7.5492e-05          741.47          3.3661          3.3323
v  turbulent_viscosity       9.261e-12        0.047502       0.0048045       0.0035497
v  CourantNb                    0.1347           12197          186.71          129.35
v  FourierNb                    5.8539          1248.2           63.25          34.196
v  total_pressure           4.9965e+05      5.0937e+05      5.0548e+05      5.0404e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.2701           12263          249.96          163.55


 TIME FOR THE TIME STEP               50:        0.24895E+01

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


 INSTANT    0.510000000E+01   TIME STEP NUMBER              51
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.123340078E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283279E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12186E+02 0.81706E+00
   Friction velocity        uet   :  0.72851E-02 0.14628E+01
   Friction velocity        uk    :  0.73029E-02 0.14559E+01
   Dimensionless distance   yplus :  0.59825E-01 0.11652E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        335
   Nb of faces within the viscous sub-layer     :       3449
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.32646E+00    1385   0.96728E+00   0.28398E-01 
c  VelocityY    0.32646E+00    1385   0.96728E+00   0.00000E+00 
c  VelocityZ    0.32646E+00    1385   0.96728E+00   0.00000E+00 
c  Pressure     0.24697E+00     624   0.82133E-02   0.11934E+00 
c  k            0.28883E-01     182   0.12410E-03   0.82196E-05 
c  epsilon      0.70826E+02      91   0.91940E-04   0.33108E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -13.463          7.2615       -0.088157       -0.084323
v  Velocity[Y]                 -6.9714          16.294         0.36307         0.28036
v  Velocity[Z]                 -9.6141          5.7313         0.10458      -0.0045814
v  ǁVelocityǁ                0.0047989          16.614          0.8269         0.75763
v  Pressure                    -365.15          9708.6            5591          4120.2
v  k                        1.1812e-06          0.2068       0.0067105       0.0072461
v  epsilon                  6.9353e-05          776.39          3.5066          3.4236
v  turbulent_viscosity      6.4457e-08        0.047524       0.0047819       0.0035401
v  CourantNb                   0.37093           12968          190.51          131.55
v  FourierNb                    5.8537          1248.2          63.206          34.184
v  total_pressure           4.9963e+05      5.0971e+05      5.0559e+05      5.0412e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.1417           13035          253.71          165.73


 TIME FOR THE TIME STEP               51:        0.27824E+01

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


 INSTANT    0.520000000E+01   TIME STEP NUMBER              52
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.818593816E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283320E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17723E+02 0.79012E+00
   Friction velocity        uet   :  0.22127E-01 0.15540E+01
   Friction velocity        uk    :  0.21981E-01 0.15465E+01
   Dimensionless distance   yplus :  0.20072E+00 0.12436E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        358
   Nb of faces within the viscous sub-layer     :       3422
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.86539E+00    1282   0.99484E+00   0.26509E-01 
c  VelocityY    0.86539E+00    1282   0.99484E+00   0.00000E+00 
c  VelocityZ    0.86539E+00    1282   0.99484E+00   0.00000E+00 
c  Pressure     0.26143E+00     612   0.81809E-02   0.11968E+00 
c  k            0.31047E-01     191   0.10799E-03   0.10621E-04 
c  epsilon      0.77598E+02      95   0.10880E-03   0.44841E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.2201e-05                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -15.116          7.5513       -0.090657       -0.084769
v  Velocity[Y]                 -7.5175           16.68         0.36346         0.28255
v  Velocity[Z]                  -10.23          5.9905         0.10451      -0.0053214
v  ǁVelocityǁ                0.0047096          18.411         0.83817         0.76544
v  Pressure                    -375.95           10073          5707.8          4199.5
v  k                        2.4006e-07         0.20688       0.0067847       0.0073116
v  epsilon                    5.69e-05          837.14          3.6428          3.5359
v  turbulent_viscosity      7.3741e-07        0.047501       0.0047679       0.0035331
v  CourantNb                   0.26776           13917          194.23          133.87
v  FourierNb                      5.85          1248.3          63.182          34.179
v  total_pressure           4.9962e+05      5.1007e+05      5.0571e+05       5.042e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.8972           13985          257.42          168.05


 TIME FOR THE TIME STEP               52:        0.26535E+01

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


 INSTANT    0.530000000E+01   TIME STEP NUMBER              53
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.788128423E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283665E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18544E+02 0.77980E+00
   Friction velocity        uet   :  0.81029E-02 0.16204E+01
   Friction velocity        uk    :  0.81031E-02 0.16122E+01
   Dimensionless distance   yplus :  0.66380E-01 0.12514E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        367
   Nb of faces within the viscous sub-layer     :       3408
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.77156E+00    1481   0.99377E+00   0.36510E-01 
c  VelocityY    0.77156E+00    1481   0.99377E+00   0.00000E+00 
c  VelocityZ    0.77156E+00    1481   0.99377E+00   0.00000E+00 
c  Pressure     0.27416E+00     621   0.82042E-02   0.11878E+00 
c  k            0.34466E-01     173   0.10793E-03   0.10356E-04 
c  epsilon      0.86479E+02      85   0.11064E-03   0.53867E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -15.479          7.8477       -0.091891       -0.085501
v  Velocity[Y]                  -7.991          17.522          0.3698         0.28485
v  Velocity[Z]                 -11.169          6.3457         0.10407      -0.0053526
v  ǁVelocityǁ                0.0072396          19.482         0.85154         0.77419
v  Pressure                    -385.04           10466          5827.8            4281
v  k                        8.9191e-07          0.2068       0.0068371       0.0073525
v  epsilon                  4.1837e-05          820.65          3.7875          3.6265
v  turbulent_viscosity      7.6829e-09        0.047523       0.0047508       0.0035267
v  CourantNb                     0.215           14694          198.19           136.2
v  FourierNb                    5.8487          1248.3          63.146          34.162
v  total_pressure           4.9961e+05      5.1047e+05      5.0583e+05      5.0428e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           7.844           14762          261.33          170.36


 TIME FOR THE TIME STEP               53:        0.29358E+01

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


 INSTANT    0.540000000E+01   TIME STEP NUMBER              54
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.174835442E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283340E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17818E+02 0.73664E+00
   Friction velocity        uet   :  0.16878E-01 0.16789E+01
   Friction velocity        uk    :  0.16692E-01 0.16702E+01
   Dimensionless distance   yplus :  0.16836E+00 0.12358E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        376
   Nb of faces within the viscous sub-layer     :       3361
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.11185E+01    1441   0.99544E+00   0.43234E-01 
c  VelocityY    0.11185E+01    1441   0.99544E+00   0.00000E+00 
c  VelocityZ    0.11185E+01    1441   0.99544E+00   0.00000E+00 
c  Pressure     0.29175E+00     611   0.80752E-02   0.11960E+00 
c  k            0.38427E-01     174   0.94264E-04   0.10829E-04 
c  epsilon      0.96942E+02     102   0.86935E-04   0.55220E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8741e-05                             2
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -17.173          8.2418       -0.094614       -0.085931
v  Velocity[Y]                 -8.6104          17.959         0.37241         0.28717
v  Velocity[Z]                 -11.195          6.6431         0.10507      -0.0054288
v  ǁVelocityǁ                0.0046919          20.449         0.86513         0.78243
v  Pressure                    -409.03           10905          5953.2          4366.7
v  k                        2.4571e-07         0.20686       0.0069372       0.0074336
v  epsilon                  4.0767e-05          929.37          3.9556          3.7552
v  turbulent_viscosity      6.9311e-07        0.047499       0.0047386       0.0035214
v  CourantNb                  0.012569           15878          202.76          138.94
v  FourierNb                    5.8488          1248.3          63.124           34.15
v  total_pressure           4.9959e+05      5.1091e+05      5.0595e+05      5.0437e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.3924           15946          265.89          173.09


 TIME FOR THE TIME STEP               54:        0.28756E+01

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


 INSTANT    0.550000000E+01   TIME STEP NUMBER              55
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.144480991E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283758E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20885E+02 0.72971E+00
   Friction velocity        uet   :  0.10415E-01 0.17493E+01
   Friction velocity        uk    :  0.10342E-01 0.17398E+01
   Dimensionless distance   yplus :  0.12497E+00 0.12909E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        383
   Nb of faces within the viscous sub-layer     :       3340
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.63599E+00    1668   0.98504E+00   0.37893E-01 
c  VelocityY    0.63599E+00    1668   0.98504E+00   0.00000E+00 
c  VelocityZ    0.63599E+00    1668   0.98504E+00   0.00000E+00 
c  Pressure     0.30593E+00     608   0.81253E-02   0.11846E+00 
c  k            0.42959E-01     169   0.10563E-03   0.14018E-04 
c  epsilon      0.10948E+03      87   0.12226E-03   0.90686E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -17.574          8.6972       -0.092341       -0.086797
v  Velocity[Y]                  -9.018          19.832          0.3806         0.29014
v  Velocity[Z]                 -12.175          7.2314         0.10318      -0.0056405
v  ǁVelocityǁ                0.0026548          21.743         0.87482         0.79081
v  Pressure                    -461.16           11354          6083.7          4455.3
v  k                        1.5582e-07         0.20679       0.0070184        0.007497
v  epsilon                   3.465e-05          885.27          4.1792          3.9026
v  turbulent_viscosity       1.367e-10        0.047521       0.0047083       0.0035113
v  CourantNb                  0.081868           16800          207.52          141.59
v  FourierNb                    5.8492          1248.4          63.069           34.14
v  total_pressure           4.9954e+05      5.1135e+05      5.0608e+05      5.0446e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.6567           16869          270.59          175.73


 TIME FOR THE TIME STEP               55:        0.31695E+01

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


 INSTANT    0.560000000E+01   TIME STEP NUMBER              56
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.144096153E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283672E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24558E+02 0.72963E+00
   Friction velocity        uet   :  0.94882E-02 0.18580E+01
   Friction velocity        uk    :  0.10734E-01 0.18477E+01
   Dimensionless distance   yplus :  0.13912E+00 0.13455E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        395
   Nb of faces within the viscous sub-layer     :       3282
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.16006E+01    1566   0.99695E+00   0.47912E-01 
c  VelocityY    0.16006E+01    1566   0.99695E+00   0.00000E+00 
c  VelocityZ    0.16006E+01    1566   0.99695E+00   0.00000E+00 
c  Pressure     0.32392E+00     609   0.80733E-02   0.11854E+00 
c  k            0.48865E-01     176   0.88173E-04   0.18062E-04 
c  epsilon      0.12355E+03     113   0.10107E-03   0.91793E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.7891e-05                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -19.495          9.0627        -0.09745        -0.08759
v  Velocity[Y]                  -9.969          18.925         0.38325         0.29284
v  Velocity[Z]                 -13.145           7.649          0.1033      -0.0061031
v  ǁVelocityǁ                0.0031407          22.763         0.89244         0.80039
v  Pressure                     -516.9           11837          6220.9          4548.9
v  k                        4.7497e-07         0.20686       0.0071466       0.0076015
v  epsilon                  2.9825e-05          1202.5           4.359          4.0427
v  turbulent_viscosity      5.8321e-10        0.047498       0.0047046       0.0035067
v  CourantNb                  0.087208           17977          211.36          144.27
v  FourierNb                    5.8447          1248.4          63.072          34.142
v  total_pressure           4.9948e+05      5.1184e+05      5.0622e+05      5.0455e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.2438           18046          274.43          178.41


 TIME FOR THE TIME STEP               56:        0.30487E+01

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


 INSTANT    0.570000000E+01   TIME STEP NUMBER              57
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.110227739E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283789E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23760E+02 0.73184E+00
   Friction velocity        uet   :  0.15472E-01 0.19146E+01
   Friction velocity        uk    :  0.15448E-01 0.19033E+01
   Dimensionless distance   yplus :  0.14031E+00 0.12915E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        413
   Nb of faces within the viscous sub-layer     :       3285
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.70242E+00    1886   0.99033E+00   0.54815E-01 
c  VelocityY    0.70242E+00    1886   0.99033E+00   0.00000E+00 
c  VelocityZ    0.70242E+00    1886   0.99033E+00   0.00000E+00 
c  Pressure     0.34346E+00     609   0.80783E-02   0.11862E+00 
c  k            0.56396E-01     169   0.87403E-04   0.17806E-04 
c  epsilon      0.14045E+03      98   0.79737E-04   0.87606E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -19.848          9.4218       -0.096466       -0.088146
v  Velocity[Y]                 -10.508          21.901         0.39421         0.29679
v  Velocity[Z]                 -13.599           7.949         0.10312      -0.0056847
v  ǁVelocityǁ                0.0064404          23.609         0.90538         0.80778
v  Pressure                    -569.95           12350          6370.7          4651.6
v  k                        4.6026e-07         0.20678       0.0072411       0.0076659
v  epsilon                  2.7687e-05          917.52          4.6065          4.2079
v  turbulent_viscosity      1.6024e-08         0.04752       0.0046867       0.0034986
v  CourantNb                   0.11789           19159          217.13          147.31
v  FourierNb                    5.8455          1248.4           63.04          34.132
v  total_pressure           4.9943e+05      5.1235e+05      5.0637e+05      5.0465e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.0453           19229          280.17          181.44


 TIME FOR THE TIME STEP               57:        0.34823E+01

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


 INSTANT    0.580000000E+01   TIME STEP NUMBER              58
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.117098550E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283833E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28482E+02 0.73500E+00
   Friction velocity        uet   :  0.98923E-02 0.19904E+01
   Friction velocity        uk    :  0.98760E-02 0.19786E+01
   Dimensionless distance   yplus :  0.14951E+00 0.13971E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        419
   Nb of faces within the viscous sub-layer     :       3258
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.18638E+01    1719   0.99637E+00   0.45250E-01 
c  VelocityY    0.18638E+01    1719   0.99637E+00   0.00000E+00 
c  VelocityZ    0.18638E+01    1719   0.99637E+00   0.00000E+00 
c  Pressure     0.36274E+00     608   0.80283E-02   0.11836E+00 
c  k            0.63668E-01     176   0.74956E-04   0.20055E-04 
c  epsilon      0.15791E+03     120   0.57961E-04   0.93796E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.3525e-05                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -22.153          9.8105        -0.10041       -0.089547
v  Velocity[Y]                 -11.573          22.316         0.39409         0.29873
v  Velocity[Z]                 -14.486          8.4894          0.1041      -0.0065794
v  ǁVelocityǁ                0.0053061          25.854         0.92661         0.82431
v  Pressure                    -629.74           12897          6522.9          4755.8
v  k                        4.4775e-07         0.20684       0.0073527       0.0077453
v  epsilon                  1.8617e-05          1094.3          4.8582          4.3783
v  turbulent_viscosity      1.7069e-07        0.047497       0.0046405       0.0034703
v  CourantNb                   0.15016           20381          222.21          150.22
v  FourierNb                     5.847          1248.4          62.958          34.101
v  total_pressure           4.9937e+05       5.129e+05      5.0652e+05      5.0476e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.1514           20451          285.17          184.32


 TIME FOR THE TIME STEP               58:        0.32678E+01

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


 INSTANT    0.590000000E+01   TIME STEP NUMBER              59
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.235464968E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283868E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29527E+02 0.73700E+00
   Friction velocity        uet   :  0.75206E-02 0.21438E+01
   Friction velocity        uk    :  0.75083E-02 0.21299E+01
   Dimensionless distance   yplus :  0.11013E+00 0.14029E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        435
   Nb of faces within the viscous sub-layer     :       3200
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.14762E+01    1998   0.99540E+00   0.59951E-01 
c  VelocityY    0.14762E+01    1998   0.99540E+00   0.00000E+00 
c  VelocityZ    0.14762E+01    1998   0.99540E+00   0.00000E+00 
c  Pressure     0.38049E+00     608   0.80213E-02   0.11715E+00 
c  k            0.74514E-01     176   0.71148E-04   0.23524E-04 
c  epsilon      0.18272E+03     105   0.54941E-04   0.96608E+02 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -22.79          10.349       -0.097447       -0.089678
v  Velocity[Y]                 -11.935          24.272         0.40361         0.30252
v  Velocity[Z]                 -15.387          9.1971         0.10259      -0.0070378
v  ǁVelocityǁ                0.0070821          27.026         0.93377         0.82737
v  Pressure                    -790.02           13471          6685.8          4867.7
v  k                         3.501e-07         0.22937       0.0075213        0.007903
v  epsilon                  1.7753e-05          1096.7          5.2167          4.6405
v  turbulent_viscosity      5.4555e-09        0.047517       0.0045889       0.0034463
v  CourantNb                  0.065292           21585          228.73          154.25
v  FourierNb                    5.8485          1248.4          62.867          34.063
v  total_pressure           4.9921e+05      5.1347e+05      5.0669e+05      5.0487e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           9.909           21656           291.6          188.32


 TIME FOR THE TIME STEP               59:        0.36394E+01

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


 INSTANT    0.600000000E+01   TIME STEP NUMBER              60
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.162352410E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283884E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30753E+02 0.73622E+00
   Friction velocity        uet   :  0.85856E-02 0.22414E+01
   Friction velocity        uk    :  0.12488E-01 0.22271E+01
   Dimensionless distance   yplus :  0.18837E+00 0.14015E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        446
   Nb of faces within the viscous sub-layer     :       3212
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.23553E+01    1904   0.99776E+00   0.76088E-01 
c  VelocityY    0.23553E+01    1904   0.99776E+00   0.00000E+00 
c  VelocityZ    0.23553E+01    1904   0.99776E+00   0.00000E+00 
c  Pressure     0.40627E+00     607   0.79491E-02   0.11809E+00 
c  k            0.89206E-01     167   0.57400E-04   0.30242E-04 
c  epsilon      0.21485E+03     109   0.49912E-04   0.12038E+03 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.6477e-05                             1
a  epsilon      -0.0035822                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -25.054          10.869        -0.10213       -0.090789
v  Velocity[Y]                 -13.479          24.648         0.40925         0.30653
v  Velocity[Z]                 -16.238          9.6142         0.10192      -0.0075304
v  ǁVelocityǁ                0.0046649          29.412         0.96098         0.84358
v  Pressure                    -1094.7           14080          6851.2          4981.1
v  k                        2.6222e-07         0.24938       0.0077043       0.0080082
v  epsilon                  1.2105e-05          1290.5          5.5397          4.8626
v  turbulent_viscosity      4.3772e-07        0.047497       0.0045666       0.0034443
v  CourantNb                   0.19252           23227          232.76          156.65
v  FourierNb                    5.8556          1248.4           62.82          34.057
v  total_pressure           4.9891e+05      5.1408e+05      5.0685e+05      5.0498e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.1293           23299          295.58           190.7


 TIME FOR THE TIME STEP               60:        0.35422E+01

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


 INSTANT    0.610000000E+01   TIME STEP NUMBER              61
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.187025983E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283855E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35588E+02 0.74492E+00
   Friction velocity        uet   :  0.14524E-01 0.23500E+01
   Friction velocity        uk    :  0.14436E-01 0.23342E+01
   Dimensionless distance   yplus :  0.17555E+00 0.14397E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        470
   Nb of faces within the viscous sub-layer     :       3175
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.13446E+01    2190   0.99206E+00   0.67921E-01 
c  VelocityY    0.13446E+01    2190   0.99206E+00   0.00000E+00 
c  VelocityZ    0.13446E+01    2190   0.99206E+00   0.00000E+00 
c  Pressure     0.42714E+00     606   0.79643E-02   0.11714E+00 
c  k            0.10567E+00     164   0.62107E-04   0.38793E-04 
c  epsilon      0.25033E+03     101   0.46085E-04   0.14056E+03 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -0.0421                             4


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -25.923          11.377        -0.10211       -0.091878
v  Velocity[Y]                 -13.694          27.144         0.41469         0.30959
v  Velocity[Z]                 -17.002          10.008        0.099342      -0.0076466
v  ǁVelocityǁ                0.0065963          30.343         0.96684         0.84684
v  Pressure                    -1443.8           14736          7032.7          5105.4
v  k                        2.2137e-07          0.2803       0.0079584       0.0082039
v  epsilon                  7.9816e-06            1109          5.9901           5.186
v  turbulent_viscosity      1.8092e-07        0.047517       0.0045467       0.0034348
v  CourantNb                  0.075625           24231          241.14          161.14
v  FourierNb                    5.8572          1248.6          62.781          34.044
v  total_pressure           4.9856e+05      5.1474e+05      5.0703e+05      5.0511e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.3103           24304          303.92          195.18


 TIME FOR THE TIME STEP               61:        0.39109E+01

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


 INSTANT    0.620000000E+01   TIME STEP NUMBER              62
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.173741744E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283870E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37408E+02 0.76512E+00
   Friction velocity        uet   :  0.14688E-01 0.24590E+01
   Friction velocity        uk    :  0.14524E-01 0.24425E+01
   Dimensionless distance   yplus :  0.16179E+00 0.14626E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        485
   Nb of faces within the viscous sub-layer     :       3178
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          8 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.35122E+01    2176   0.99837E+00   0.98618E-01 
c  VelocityY    0.35122E+01    2176   0.99837E+00   0.00000E+00 
c  VelocityZ    0.35122E+01    2176   0.99837E+00   0.00000E+00 
c  Pressure     0.45448E+00     606   0.79804E-02   0.11771E+00 
c  k            0.12800E+00     157   0.48290E-04   0.46763E-04 
c  epsilon      0.29552E+03     107   0.52642E-04   0.19700E+03 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -8.0647e-05                             1
a  epsilon      -0.0074496                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -29.036          11.742        -0.10747       -0.093716
v  Velocity[Y]                 -15.495          26.902         0.42025         0.31401
v  Velocity[Z]                  -18.71          10.602        0.099733      -0.0085705
v  ǁVelocityǁ                0.0063631          33.974         0.99822         0.86722
v  Pressure                    -1769.9           15434          7215.5          5230.4
v  k                        1.9787e-07         0.31041       0.0082549       0.0083798
v  epsilon                  8.9912e-06          1622.1          6.5216          5.5302
v  turbulent_viscosity      2.3897e-07         0.34492       0.0045676       0.0034514
v  CourantNb                   0.43873           26220          245.14          163.81
v  FourierNb                    5.8569            1293          62.807           34.05
v  total_pressure           4.9823e+05      5.1543e+05      5.0722e+05      5.0523e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.9089           26295          307.95          197.86


 TIME FOR THE TIME STEP               62:        0.39057E+01

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


 INSTANT    0.630000000E+01   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.149103640E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283928E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44757E+02 0.76482E+00
   Friction velocity        uet   :  0.70923E-02 0.25798E+01
   Friction velocity        uk    :  0.70756E-02 0.25044E+01
   Dimensionless distance   yplus :  0.79766E-01 0.15102E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        502
   Nb of faces within the viscous sub-layer     :       3146
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.13755E+01    2459   0.99147E+00   0.10828E+00 
c  VelocityY    0.13755E+01    2459   0.99147E+00   0.00000E+00 
c  VelocityZ    0.13755E+01    2459   0.99147E+00   0.00000E+00 
c  Pressure     0.48036E+00     606   0.79459E-02   0.11739E+00 
c  k            0.15856E+00     163   0.43930E-04   0.74350E-04 
c  epsilon      0.35869E+03     108   0.42571E-04   0.30309E+03 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -29.329          12.509        -0.10302       -0.093514
v  Velocity[Y]                 -15.601          29.316          0.4346         0.31818
v  Velocity[Z]                  -19.21          11.312        0.098881      -0.0080867
v  ǁVelocityǁ                0.0083197          34.374          1.0097          0.8721
v  Pressure                    -2156.5           16166          7422.3          5372.9
v  k                         1.722e-07          0.3558       0.0086739       0.0087127
v  epsilon                  6.5247e-06          1309.4          7.2245          6.0471
v  turbulent_viscosity      1.2976e-07        0.047513       0.0045658       0.0034513
v  CourantNb                   0.28646           27663          254.75          169.16
v  FourierNb                    5.8603          1248.5          62.798          34.054
v  total_pressure           4.9784e+05      5.1617e+05      5.0742e+05      5.0537e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.0606           27739          317.54          203.22


 TIME FOR THE TIME STEP               63:        0.42827E+01

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


 INSTANT    0.640000000E+01   TIME STEP NUMBER              64
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.929754979E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284010E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45272E+02 0.77419E+00
   Friction velocity        uet   :  0.19512E-01 0.26159E+01
   Friction velocity        uk    :  0.19423E-01 0.25601E+01
   Dimensionless distance   yplus :  0.20388E+00 0.15079E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        518
   Nb of faces within the viscous sub-layer     :       3118
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          9 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.38977E+01    2284   0.99788E+00   0.99889E-01 
c  VelocityY    0.38977E+01    2284   0.99788E+00   0.00000E+00 
c  VelocityZ    0.38977E+01    2284   0.99788E+00   0.00000E+00 
c  Pressure     0.51009E+00     601   0.78843E-02   0.11774E+00 
c  k            0.19762E+00     164   0.44085E-04   0.10348E-03 
c  epsilon      0.43659E+03     112   0.32824E-04   0.37749E+03 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.0963e-05                             2
a  epsilon      -0.0010832                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -32.746          12.992        -0.10894        -0.09499
v  Velocity[Y]                 -17.754          32.154         0.44072         0.32217
v  Velocity[Z]                 -20.574          12.319        0.099928      -0.0086821
v  ǁVelocityǁ                0.0049785           38.47          1.0426         0.89396
v  Pressure                    -2559.3           16941          7620.1          5507.5
v  k                        2.2887e-07         0.46161       0.0091881       0.0090506
v  epsilon                  1.0017e-05          1594.6          8.0086          6.5952
v  turbulent_viscosity       2.744e-07        0.047493       0.0045992       0.0034639
v  CourantNb                  0.044136           29593          260.62          172.38
v  FourierNb                    5.8671          1248.7           62.87          34.082
v  total_pressure           4.9744e+05      5.1694e+05      5.0762e+05      5.0551e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.6918           29673          323.49          206.46


 TIME FOR THE TIME STEP               64:        0.40543E+01

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


 INSTANT    0.650000000E+01   TIME STEP NUMBER              65
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.733379655E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283912E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53732E+02 0.78575E+00
   Friction velocity        uet   :  0.14328E-01 0.28862E+01
   Friction velocity        uk    :  0.14199E-01 0.27189E+01
   Dimensionless distance   yplus :  0.15592E+00 0.15789E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        528
   Nb of faces within the viscous sub-layer     :       3118
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.31140E+01    2499   0.99706E+00   0.12589E+00 
c  VelocityY    0.31140E+01    2499   0.99706E+00   0.00000E+00 
c  VelocityZ    0.31140E+01    2499   0.99706E+00   0.00000E+00 
c  Pressure     0.53465E+00     605   0.79380E-02   0.11648E+00 
c  k            0.24853E+00     171   0.49786E-04   0.19879E-03 
c  epsilon      0.53501E+03     116   0.33434E-04   0.59902E+03 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -33.533          13.596        -0.11054        -0.09631
v  Velocity[Y]                 -17.727          33.392         0.44159          0.3253
v  Velocity[Z]                 -22.162           12.72        0.095033        -0.01033
v  ǁVelocityǁ                0.0086307           39.16          1.0553         0.90079
v  Pressure                    -2969.6           17761          7846.3          5662.4
v  k                        1.8771e-07         0.55812       0.0098707       0.0095366
v  epsilon                  8.0453e-06          1620.6          9.0618          7.3385
v  turbulent_viscosity      6.0664e-08        0.047512       0.0046019       0.0034706
v  CourantNb                   0.23523           31075          270.55          178.02
v  FourierNb                    5.8697          1266.7          62.862          34.082
v  total_pressure           4.9703e+05      5.1776e+05      5.0785e+05      5.0566e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           8.606           31158          333.41           212.1


 TIME FOR THE TIME STEP               65:        0.43425E+01

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


 INSTANT    0.660000000E+01   TIME STEP NUMBER              66
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.188306376E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284095E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55105E+02 0.78523E+00
   Friction velocity        uet   :  0.75143E-02 0.29530E+01
   Friction velocity        uk    :  0.74773E-02 0.27858E+01
   Dimensionless distance   yplus :  0.77344E-01 0.15812E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        544
   Nb of faces within the viscous sub-layer     :       3082
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.50219E+01    2580   0.99852E+00   0.16848E+00 
c  VelocityY    0.50219E+01    2580   0.99852E+00   0.00000E+00 
c  VelocityZ    0.50219E+01    2580   0.99852E+00   0.00000E+00 
c  Pressure     0.57303E+00     602   0.78525E-02   0.11789E+00 
c  k            0.32631E+00     177   0.45476E-04   0.26032E-03 
c  epsilon      0.68340E+03     120   0.24895E-04   0.80134E+03 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -9.0677e-05                             4
a  epsilon       -0.006708                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -37.253          13.891        -0.11869       -0.097528
v  Velocity[Y]                 -20.328          33.966         0.45541         0.33078
v  Velocity[Z]                 -22.628          13.421          0.0957      -0.0094448
v  ǁVelocityǁ                 0.004131          43.635           1.097         0.92602
v  Pressure                    -3409.4           18646          8073.3          5817.8
v  k                        3.0908e-07         0.71445        0.010803        0.010156
v  epsilon                  1.2579e-05          1795.8          10.401          8.2361
v  turbulent_viscosity      3.2061e-07        0.047492       0.0046548       0.0035091
v  CourantNb                   0.31198           33513          277.09          181.95
v  FourierNb                    5.8706          1266.9          62.929           34.11
v  total_pressure           4.9659e+05      5.1865e+05      5.0807e+05      5.0582e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.4315           33601          340.01          216.06


 TIME FOR THE TIME STEP               66:        0.44722E+01

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


 INSTANT    0.670000000E+01   TIME STEP NUMBER              67
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.173129994E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284136E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64168E+02 0.79641E+00
   Friction velocity        uet   :  0.14633E-01 0.32383E+01
   Friction velocity        uk    :  0.14480E-01 0.29773E+01
   Dimensionless distance   yplus :  0.16358E+00 0.16436E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        550
   Nb of faces within the viscous sub-layer     :       3060
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.26984E+01    2888   0.99270E+00   0.14975E+00 
c  VelocityY    0.26984E+01    2888   0.99270E+00   0.00000E+00 
c  VelocityZ    0.26984E+01    2888   0.99270E+00   0.00000E+00 
c  Pressure     0.60156E+00     593   0.78982E-02   0.11668E+00 
c  k            0.41728E+00     184   0.63066E-04   0.62135E-03 
c  epsilon      0.85709E+03     125   0.29933E-04   0.17927E+04 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8712e-06                             1
a  epsilon     -0.00026217                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -38.339          14.731        -0.10846        -0.09833
v  Velocity[Y]                 -20.677          37.926         0.46552         0.33541
v  Velocity[Z]                 -24.317          14.291        0.092772       -0.010235
v  ǁVelocityǁ                0.0081852          45.004          1.1035         0.93286
v  Pressure                    -3911.3           19587            8329          5992.9
v  k                        2.7598e-07          0.8848        0.012054        0.011053
v  epsilon                  1.0673e-05          2149.3          12.347          9.5957
v  turbulent_viscosity      9.0451e-09        0.047509       0.0046731       0.0035309
v  CourantNb                  0.077906           35596          289.59          188.43
v  FourierNb                    5.8691          1250.3          62.948          34.139
v  total_pressure           4.9609e+05      5.1959e+05      5.0833e+05      5.0599e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.0587           36846          352.53          222.57


 TIME FOR THE TIME STEP               67:        0.49006E+01

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


 INSTANT    0.680000000E+01   TIME STEP NUMBER              68
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.841250293E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284920E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66743E+02 0.20133E+01
   Friction velocity        uet   :  0.13228E-01 0.33521E+01
   Friction velocity        uk    :  0.13183E-01 0.30468E+01
   Dimensionless distance   yplus :  0.21447E+00 0.16487E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        579
   Nb of faces within the viscous sub-layer     :       3016
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.72532E+01    2580   0.10026E+01   0.19639E+00 
c  VelocityY    0.72532E+01    2580   0.10026E+01   0.00000E+00 
c  VelocityZ    0.72532E+01    2580   0.10026E+01   0.00000E+00 
c  Pressure     0.64334E+00     593   0.78123E-02   0.11771E+00 
c  k            0.57065E+00     192   0.76563E-04   0.13458E-02 
c  epsilon      0.11385E+04     130   0.30437E-04   0.33445E+04 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.2277e-06                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -42.303          15.897        -0.12445        -0.10006
v  Velocity[Y]                 -23.566          38.787         0.47427         0.33998
v  Velocity[Z]                 -26.389          15.665         0.09295       -0.010851
v  ǁVelocityǁ                0.0080266          49.929           1.147         0.96008
v  Pressure                    -4387.8           20566          8576.6          6159.9
v  k                        2.7313e-07          1.1367        0.014143        0.012543
v  epsilon                  1.3606e-05          2377.3           14.98          11.548
v  turbulent_viscosity      2.4086e-07         0.04749       0.0046927       0.0035538
v  CourantNb                 0.0033209           39325          294.53          192.14
v  FourierNb                    5.8557          1297.1          62.961          34.157
v  total_pressure           4.9561e+05      5.2057e+05      5.0858e+05      5.0616e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           9.019           40622          357.49           226.3


 TIME FOR THE TIME STEP               68:        0.44557E+01

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


 INSTANT    0.690000000E+01   TIME STEP NUMBER              69
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.115848762E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285111E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70126E+02 0.46978E+01
   Friction velocity        uet   :  0.21490E-01 0.36673E+01
   Friction velocity        uk    :  0.21448E-01 0.32517E+01
   Dimensionless distance   yplus :  0.26856E+00 0.17007E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        588
   Nb of faces within the viscous sub-layer     :       3025
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30495E+01    3105   0.99607E+00   0.20785E+00 
c  VelocityY    0.30495E+01    3105   0.99607E+00   0.00000E+00 
c  VelocityZ    0.30495E+01    3105   0.99607E+00   0.00000E+00 
c  Pressure     0.67763E+00     602   0.78699E-02   0.11694E+00 
c  k            0.80860E+00     200   0.11133E-03   0.29329E-02 
c  epsilon      0.15665E+04     136   0.36656E-04   0.76088E+04 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.1373e-06                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -43.564          16.117        -0.13144        -0.10073
v  Velocity[Y]                 -23.679          41.441         0.48248         0.34513
v  Velocity[Z]                 -27.377          16.014        0.085868       -0.011647
v  ǁVelocityǁ                0.0031489          51.075           1.169         0.97037
v  Pressure                    -4942.6           21638          8861.5          6353.8
v  k                        2.5056e-07          1.6638         0.01687        0.014459
v  epsilon                  8.6318e-06          3269.1          18.821          14.274
v  turbulent_viscosity      1.0214e-08        0.047508       0.0048586       0.0036676
v  CourantNb                   0.15855           43484             308          199.37
v  FourierNb                    5.8453          1252.5          63.214          34.281
v  total_pressure           4.9506e+05      5.2164e+05      5.0886e+05      5.0635e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.2728           44737          371.21          233.65


 TIME FOR THE TIME STEP               69:        0.52202E+01

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


 INSTANT    0.700000000E+01   TIME STEP NUMBER              70
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.161621496E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284402E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75290E+02 0.68492E+01
   Friction velocity        uet   :  0.10857E-01 0.37788E+01
   Friction velocity        uk    :  0.10844E-01 0.33117E+01
   Dimensionless distance   yplus :  0.15086E+00 0.17743E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        604
   Nb of faces within the viscous sub-layer     :       3002
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.83717E+01    2922   0.99959E+00   0.20329E+00 
c  VelocityY    0.83717E+01    2922   0.99959E+00   0.00000E+00 
c  VelocityZ    0.83717E+01    2922   0.99959E+00   0.00000E+00 
c  Pressure     0.72206E+00     591   0.77772E-02   0.11766E+00 
c  k            0.11715E+01     208   0.11532E-03   0.59117E-02 
c  epsilon      0.22294E+04     141   0.37778E-04   0.14406E+05 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -48.069          17.238        -0.13476        -0.10311
v  Velocity[Y]                 -27.152           43.06         0.49978         0.35007
v  Velocity[Z]                 -28.869          16.807        0.095764       -0.011687
v  ǁVelocityǁ                0.0052798          56.622          1.2224          1.0071
v  Pressure                    -5502.7           22763            9147          6547.6
v  k                        2.6288e-07          2.1351        0.021405         0.01766
v  epsilon                  1.3035e-05          4225.4          24.574          18.341
v  turbulent_viscosity      2.0647e-08         0.10803       0.0050685       0.0037996
v  CourantNb                 0.0094507           48108          317.75          204.73
v  FourierNb                    5.8422          1253.4          63.529          34.422
v  total_pressure            4.945e+05      5.2276e+05      5.0915e+05      5.0655e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.2437           49362          381.28          239.15


 TIME FOR THE TIME STEP               70:        0.49648E+01

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


 INSTANT    0.710000000E+01   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.226286605E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285261E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.78739E+02 0.12646E+02
   Friction velocity        uet   :  0.14609E-01 0.41350E+01
   Friction velocity        uk    :  0.14599E-01 0.35223E+01
   Dimensionless distance   yplus :  0.19024E+00 0.17922E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        600
   Nb of faces within the viscous sub-layer     :       2928
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.64222E+01    3230   0.99822E+00   0.31940E+00 
c  VelocityY    0.64222E+01    3230   0.99822E+00   0.00000E+00 
c  VelocityZ    0.64222E+01    3230   0.99822E+00   0.00000E+00 
c  Pressure     0.75596E+00     602   0.78399E-02   0.11617E+00 
c  k            0.17031E+01     217   0.14315E-03   0.16715E-01 
c  epsilon      0.35331E+04     147   0.10104E-02   0.11463E+07 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.3002e-06                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -49.38          18.117        -0.12333        -0.10475
v  Velocity[Y]                 -27.166          46.967         0.50093         0.35593
v  Velocity[Z]                 -31.501          18.581        0.083511       -0.013685
v  ǁVelocityǁ                 0.005736          58.144          1.2322           1.017
v  Pressure                    -6079.9           23950          9480.6          6776.1
v  k                        1.4826e-07          3.1468        0.029093        0.022796
v  epsilon                  5.3039e-06           97943          52.368          29.127
v  turbulent_viscosity      4.3439e-08         0.08545       0.0053464       0.0040392
v  CourantNb                  0.059546           53087          333.57           213.5
v  FourierNb                    5.8522          1255.4          63.892          34.637
v  total_pressure           4.9392e+05      5.2395e+05      5.0948e+05      5.0678e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.6961           54342          397.46          248.14


 TIME FOR THE TIME STEP               71:        0.53777E+01

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


 INSTANT    0.720000000E+01   TIME STEP NUMBER              72
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.277281447E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284637E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98020E+02 0.19906E+02
   Friction velocity        uet   :  0.89286E-02 0.42950E+01
   Friction velocity        uk    :  0.89202E-02 0.36324E+01
   Dimensionless distance   yplus :  0.10644E+00 0.18885E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        607
   Nb of faces within the viscous sub-layer     :       2903
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10465E+02    2902   0.99952E+00   0.34511E+00 
c  VelocityY    0.10465E+02    2902   0.99952E+00   0.00000E+00 
c  VelocityZ    0.10465E+02    2902   0.99952E+00   0.00000E+00 
c  Pressure     0.81208E+00     601   0.76857E-02   0.11785E+00 
c  k            0.26968E+01     224   0.14878E-03   0.37747E-01 
c  epsilon      0.61035E+04     150   0.32662E-03   0.99727E+06 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.3309e-06                             3
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -54.97          18.591        -0.13567        -0.10523
v  Velocity[Y]                 -31.158          48.847          0.5233         0.36257
v  Velocity[Z]                 -32.139          19.761        0.082033       -0.013059
v  ǁVelocityǁ                 0.001461          64.958          1.2802          1.0477
v  Pressure                    -6699.3           25245          9813.3          7002.3
v  k                        4.7005e-08          4.4448        0.040521        0.031086
v  epsilon                  6.6964e-06           36100          49.675          35.526
v  turbulent_viscosity       5.254e-08          0.1212       0.0054947       0.0042188
v  CourantNb                   0.16411           61396          340.38          218.55
v  FourierNb                    5.8532            1267          64.014          34.779
v  total_pressure            4.933e+05      5.2525e+05      5.0981e+05        5.07e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.2205           62657           404.4          253.33


 TIME FOR THE TIME STEP               72:        0.49470E+01

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


 INSTANT    0.730000000E+01   TIME STEP NUMBER              73
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.226177616E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284635E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10881E+03 0.25206E+02
   Friction velocity        uet   :  0.10572E-01 0.47591E+01
   Friction velocity        uk    :  0.10561E-01 0.37615E+01
   Dimensionless distance   yplus :  0.19955E+00 0.19977E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        583
   Nb of faces within the viscous sub-layer     :       2901
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.50036E+01    3416   0.99078E+00   0.27546E+00 
c  VelocityY    0.50036E+01    3416   0.99078E+00   0.00000E+00 
c  VelocityZ    0.50036E+01    3416   0.99078E+00   0.00000E+00 
c  Pressure     0.85518E+00     603   0.78122E-02   0.11708E+00 
c  k            0.41298E+01     233   0.21494E-03   0.10481E+00 
c  epsilon      0.78351E+04     159   0.18544E-03   0.28594E+06 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -1.875e-06                             1
a  epsilon       -0.001798                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -56.021          20.658        -0.15076         -0.1084
v  Velocity[Y]                 -30.917          52.836         0.52809          0.3672
v  Velocity[Z]                 -34.542          20.148        0.078532       -0.013888
v  ǁVelocityǁ                 0.008184          65.771          1.3139          1.0672
v  Pressure                    -7374.4           26604           10195          7262.9
v  k                        7.3084e-08          6.7718        0.059458        0.044037
v  epsilon                  6.1349e-06           41081           74.27          52.846
v  turbulent_viscosity      3.5131e-10         0.16724       0.0067036       0.0049756
v  CourantNb                   0.29895           68008          356.03          226.76
v  FourierNb                    5.8625          1249.1          65.931          35.623
v  total_pressure           4.9263e+05       5.266e+05      5.1019e+05      5.0726e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           9.104           69257          421.96          262.39


 TIME FOR THE TIME STEP               73:        0.56434E+01

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


 INSTANT    0.740000000E+01   TIME STEP NUMBER              74
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.717218862E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284813E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14004E+03 0.31268E+02
   Friction velocity        uet   :  0.17804E-01 0.49062E+01
   Friction velocity        uk    :  0.17768E-01 0.40289E+01
   Dimensionless distance   yplus :  0.20208E+00 0.21760E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        586
   Nb of faces within the viscous sub-layer     :       2863
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.15669E+02    3136   0.99950E+00   0.39890E+00 
c  VelocityY    0.15669E+02    3136   0.99950E+00   0.00000E+00 
c  VelocityZ    0.15669E+02    3136   0.99950E+00   0.00000E+00 
c  Pressure     0.91093E+00     607   0.77893E-02   0.11776E+00 
c  k            0.67502E+01     244   0.26854E-03   0.27759E+00 
c  epsilon      0.12656E+05     167   0.28225E-03   0.77410E+06 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -62.81          21.798         -0.1567        -0.11126
v  Velocity[Y]                 -35.525          56.024         0.53337         0.37205
v  Velocity[Z]                 -37.906           22.11        0.074037       -0.016855
v  ǁVelocityǁ                 0.014695          74.057          1.3752          1.1102
v  Pressure                      -8010           28080           10589          7530.1
v  k                        1.9922e-07          9.8867           0.101        0.069754
v  epsilon                    9.41e-06           46045          121.38          84.721
v  turbulent_viscosity      6.1517e-08         0.24017       0.0084358       0.0060419
v  CourantNb                   0.46667           74441           369.5          234.47
v  FourierNb                    5.9475          1267.1          68.619          36.838
v  total_pressure           4.9199e+05      5.2808e+05      5.1059e+05      5.0753e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.4447           75690          438.12          271.31


 TIME FOR THE TIME STEP               74:        0.52780E+01

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


 INSTANT    0.750000000E+01   TIME STEP NUMBER              75
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.116265539E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285227E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14565E+03 0.35301E+02
   Friction velocity        uet   :  0.19140E-01 0.55085E+01
   Friction velocity        uk    :  0.19104E-01 0.41724E+01
   Dimensionless distance   yplus :  0.27544E+00 0.26264E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        560
   Nb of faces within the viscous sub-layer     :       2801
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.62123E+01    3534   0.99483E+00   0.45509E+00 
c  VelocityY    0.62123E+01    3534   0.99483E+00   0.00000E+00 
c  VelocityZ    0.62123E+01    3534   0.99483E+00   0.00000E+00 
c  Pressure     0.96132E+00     603   0.78148E-02   0.11726E+00 
c  k            0.11268E+02     249   0.36659E-03   0.71569E+00 
c  epsilon      0.21276E+05     172   0.45485E-03   0.24916E+07 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -63.737          23.631        -0.15785          -0.113
v  Velocity[Y]                 -35.522          59.711         0.56351         0.37818
v  Velocity[Z]                 -38.795          22.951        0.068076       -0.016268
v  ǁVelocityǁ                 0.013376          74.989          1.4018          1.1258
v  Pressure                    -8795.5           29634           11044          7842.3
v  k                        1.7335e-07          15.143         0.15155         0.10481
v  epsilon                  7.6701e-06           46650          196.37          137.81
v  turbulent_viscosity      3.2413e-09         0.37329         0.01373       0.0087677
v  CourantNb                   0.50279           82080          387.79          244.81
v  FourierNb                    6.0119          1267.2          77.784           40.31
v  total_pressure            4.912e+05      5.2963e+05      5.1104e+05      5.0784e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.2185           83330          465.57          285.12


 TIME FOR THE TIME STEP               75:        0.58139E+01

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


 INSTANT    0.760000000E+01   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.318445676E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285167E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18582E+03 0.37965E+02
   Friction velocity        uet   :  0.11491E-01 0.56638E+01
   Friction velocity        uk    :  0.11450E-01 0.43045E+01
   Dimensionless distance   yplus :  0.22975E+00 0.32723E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        574
   Nb of faces within the viscous sub-layer     :       2840
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.17511E+02    2956   0.99978E+00   0.32050E+00 
c  VelocityY    0.17511E+02    2956   0.99978E+00   0.00000E+00 
c  VelocityZ    0.17511E+02    2956   0.99978E+00   0.00000E+00 
c  Pressure     0.10275E+01     603   0.77145E-02   0.11836E+00 
c  k            0.18872E+02     253   0.50833E-03   0.16256E+01 
c  epsilon      0.37217E+05     174   0.64948E-03   0.76081E+07 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -71.054          24.262        -0.16425         -0.1159
v  Velocity[Y]                 -40.796          64.155         0.58468         0.38282
v  Velocity[Z]                 -41.203          25.121        0.065249       -0.019196
v  ǁVelocityǁ                 0.011499          84.067          1.4557          1.1565
v  Pressure                    -9562.6           31309           11507            8156
v  k                        2.0613e-07          22.249         0.24285         0.16597
v  epsilon                  8.8868e-06           69776          333.12          235.13
v  turbulent_viscosity      2.0911e-07         0.58378        0.016901        0.011132
v  CourantNb                   0.33177           89832          399.66          251.84
v  FourierNb                    6.0257          1562.7          82.079          42.696
v  total_pressure           4.9044e+05      5.3131e+05      5.1151e+05      5.0816e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.9249           91081          481.74          294.53


 TIME FOR THE TIME STEP               76:        0.50326E+01

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


 INSTANT    0.770000000E+01   TIME STEP NUMBER              77
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.244420367E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285181E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19056E+03 0.42559E+02
   Friction velocity        uet   :  0.14025E-01 0.62631E+01
   Friction velocity        uk    :  0.13867E-01 0.46457E+01
   Dimensionless distance   yplus :  0.17929E+00 0.43063E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        538
   Nb of faces within the viscous sub-layer     :       2795
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.13219E+02    3123   0.99781E+00   0.43551E+00 
c  VelocityY    0.13219E+02    3123   0.99781E+00   0.00000E+00 
c  VelocityZ    0.13219E+02    3123   0.99781E+00   0.00000E+00 
c  Pressure     0.10804E+01     606   0.78251E-02   0.11741E+00 
c  k            0.31319E+02     258   0.62031E-03   0.38606E+01 
c  epsilon      0.10459E+06     172   0.72555E-03   0.41938E+09 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -72.569          26.628        -0.18777        -0.11999
v  Velocity[Y]                 -40.706          69.012         0.58175         0.38737
v  Velocity[Z]                 -44.358          25.753        0.061796       -0.020115
v  ǁVelocityǁ                0.0094873            85.4          1.5217          1.1989
v  Pressure                     -10388           33066           12024          8506.2
v  k                        1.9389e-07          34.111         0.39803         0.25887
v  epsilon                  6.2276e-06      2.7664e+06          885.19          486.43
v  turbulent_viscosity      1.7214e-07         0.85664        0.024224         0.01558
v  CourantNb                  0.097028           98919          418.85          261.65
v  FourierNb                    6.0426          2205.6           93.67          47.761
v  total_pressure           4.8961e+05      5.3307e+05      5.1202e+05      5.0851e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.4111      1.0017e+05          512.52          309.41


 TIME FOR THE TIME STEP               77:        0.52612E+01

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


 INSTANT    0.780000000E+01   TIME STEP NUMBER              78
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.528970884E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285455E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11829E+03 0.50894E+02
   Friction velocity        uet   :  0.98751E-02 0.70024E+01
   Friction velocity        uk    :  0.14780E-01 0.45971E+01
   Dimensionless distance   yplus :  0.22734E+00 0.52485E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        544
   Nb of faces within the viscous sub-layer     :       2693
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.22829E+02    3144   0.99958E+00   0.48390E+00 
c  VelocityY    0.22829E+02    3144   0.99958E+00   0.00000E+00 
c  VelocityZ    0.22829E+02    3144   0.99958E+00   0.00000E+00 
c  Pressure     0.11584E+01     608   0.77399E-02   0.11884E+00 
c  k            0.52379E+02     263   0.63603E-03   0.68966E+01 
c  epsilon      0.27725E+06     168   0.44677E-03   0.42040E+09 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.5811e-06                             2
a  epsilon       -0.018241                             4


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -81.397          28.132        -0.20046        -0.12175
v  Velocity[Y]                 -46.513          73.275         0.59592         0.39421
v  Velocity[Z]                 -46.547          28.045        0.057143       -0.023478
v  ǁVelocityǁ                 0.012276          95.988          1.5864          1.2306
v  Pressure                     -11236           34999           12574          8878.6
v  k                        1.0314e-07          52.044         0.61626         0.39441
v  epsilon                  1.4737e-05       9.034e+05            1033           707.8
v  turbulent_viscosity      3.1503e-07          1.1743        0.037753        0.021883
v  CourantNb                   0.33944      1.0826e+05          440.72          273.95
v  FourierNb                    6.0936          3128.8          117.66          56.454
v  total_pressure           4.8876e+05        5.35e+05      5.1257e+05      5.0888e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.3487      1.0951e+05          558.39           330.4


 TIME FOR THE TIME STEP               78:        0.52664E+01

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


 INSTANT    0.790000000E+01   TIME STEP NUMBER              79
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.106291385E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285696E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13748E+03 0.59519E+02
   Friction velocity        uet   :  0.10310E-01 0.71130E+01
   Friction velocity        uk    :  0.14280E-01 0.48153E+01
   Dimensionless distance   yplus :  0.20701E+00 0.61592E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        504
   Nb of faces within the viscous sub-layer     :       2676
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10390E+02    3389   0.99288E+00   0.45499E+00 
c  VelocityY    0.10390E+02    3389   0.99288E+00   0.00000E+00 
c  VelocityZ    0.10390E+02    3389   0.99288E+00   0.00000E+00 
c  Pressure     0.12213E+01     605   0.78050E-02   0.11822E+00 
c  k            0.81501E+02     266   0.68264E-03   0.11610E+02 
c  epsilon      0.24566E+06     173   0.11396E-02   0.17578E+09 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -82.407          31.047          -0.201        -0.12548
v  Velocity[Y]                 -46.779          77.921         0.60042         0.40115
v  Velocity[Z]                 -48.826          29.704        0.043831       -0.022626
v  ǁVelocityǁ                0.0061238          97.362          1.6238          1.2692
v  Pressure                     -12218           36980           13174          9287.5
v  k                        3.1191e-09          76.393         0.86892         0.53938
v  epsilon                  1.4523e-06      1.1571e+06          1693.3          1130.2
v  turbulent_viscosity      4.6208e-11           1.572         0.05435        0.030332
v  CourantNb                   0.34707      1.2007e+05          462.87          284.56
v  FourierNb                    6.1827          4004.3          146.09          67.336
v  total_pressure           4.8778e+05      5.3698e+05      5.1317e+05      5.0929e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.1644      1.2131e+05          608.96          351.89


 TIME FOR THE TIME STEP               79:        0.56360E+01

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


 INSTANT    0.800000000E+01   TIME STEP NUMBER              80
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.180580105E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285681E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17065E+03 0.61549E+02
   Friction velocity        uet   :  0.13266E-01 0.82714E+01
   Friction velocity        uk    :  0.13211E-01 0.49459E+01
   Dimensionless distance   yplus :  0.11420E+00 0.68170E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        486
   Nb of faces within the viscous sub-layer     :       2561
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.32542E+02    3005   0.99911E+00   0.62500E+00 
c  VelocityY    0.32542E+02    3005   0.99911E+00   0.00000E+00 
c  VelocityZ    0.32542E+02    3005   0.99911E+00   0.00000E+00 
c  Pressure     0.13025E+01     603   0.77694E-02   0.11899E+00 
c  k            0.12329E+03     253   0.58182E-03   0.14317E+02 
c  epsilon      0.41132E+06     168   0.97637E-03   0.33036E+09 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -92.231          31.155        -0.22887        -0.13053
v  Velocity[Y]                 -53.426          82.905         0.61894         0.40714
v  Velocity[Z]                  -53.89          32.492        0.038322       -0.026065
v  ǁVelocityǁ                0.0024122           109.3          1.6885          1.3106
v  Pressure                     -13412           39096           13752            9674
v  k                          3.36e-07          102.87          1.1621         0.72546
v  epsilon                  1.4707e-05      1.1249e+06          2614.4          1760.3
v  turbulent_viscosity       2.927e-12           1.975        0.067797        0.037276
v  CourantNb                   0.15479       1.311e+05          477.32           295.4
v  FourierNb                    6.2714          4979.9          168.55          76.235
v  total_pressure           4.8659e+05       5.391e+05      5.1375e+05      5.0967e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           8.971      1.3234e+05          645.87          371.63


 TIME FOR THE TIME STEP               80:        0.50915E+01

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


 INSTANT    0.810000000E+01   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.121390360E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285803E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17871E+03 0.69677E+02
   Friction velocity        uet   :  0.21213E-01 0.84311E+01
   Friction velocity        uk    :  0.29233E-01 0.54229E+01
   Dimensionless distance   yplus :  0.20311E+00 0.71453E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        422
   Nb of faces within the viscous sub-layer     :       2498
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.14425E+02    3261   0.99682E+00   0.80772E+00 
c  VelocityY    0.14425E+02    3261   0.99682E+00   0.00000E+00 
c  VelocityZ    0.14425E+02    3261   0.99682E+00   0.00000E+00 
c  Pressure     0.13830E+01     591   0.78068E-02   0.11919E+00 
c  k            0.17606E+03     272   0.55546E-03   0.22289E+02 
c  epsilon      0.66870E+06     171   0.85954E-03   0.57467E+09 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -1.6793e-05                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -93.247          34.429        -0.24782        -0.13275
v  Velocity[Y]                 -53.253          91.085         0.65852         0.41982
v  Velocity[Z]                 -54.364          33.176        0.047891       -0.026605
v  ǁVelocityǁ                 0.023379          110.22          1.7789          1.3633
v  Pressure                     -14695           41324           14397           10113
v  k                        4.6711e-07          134.07          1.5373         0.93432
v  epsilon                  1.6793e-05      1.4364e+06          3876.4          2554.3
v  turbulent_viscosity      2.6413e-07          2.3354        0.078136        0.043414
v  CourantNb                   0.94868      1.4479e+05          500.65          307.78
v  FourierNb                    6.2794          5589.9          184.49          83.453
v  total_pressure            4.853e+05      5.4132e+05       5.144e+05      5.1011e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.2628      1.4603e+05          685.14          391.23


 TIME FOR THE TIME STEP               81:        0.55073E+01

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


 INSTANT    0.820000000E+01   TIME STEP NUMBER              82
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.153796497E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273286991E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22279E+03 0.71418E+02
   Friction velocity        uet   :  0.19733E-01 0.98699E+01
   Friction velocity        uk    :  0.19689E-01 0.61269E+01
   Dimensionless distance   yplus :  0.26729E+00 0.82407E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        429
   Nb of faces within the viscous sub-layer     :       2371
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.37255E+02    3149   0.99999E+00   0.64416E+00 
c  VelocityY    0.37255E+02    3149   0.99999E+00   0.00000E+00 
c  VelocityZ    0.37255E+02    3149   0.99999E+00   0.00000E+00 
c  Pressure     0.14732E+01     592   0.77124E-02   0.11973E+00 
c  k            0.23982E+03     245   0.55530E-03   0.24701E+02 
c  epsilon      0.10235E+07     162   0.80347E-03   0.93066E+09 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon        -0.40763                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -105.33          36.633        -0.24338        -0.13527
v  Velocity[Y]                 -60.748          94.156         0.66537         0.42721
v  Velocity[Z]                 -58.932          37.529        0.040313       -0.031565
v  ǁVelocityǁ                 0.004398          124.62          1.8335          1.4165
v  Pressure                     -16030           43752           15055           10555
v  k                        1.1719e-06          166.18          1.8695           1.151
v  epsilon                  7.2535e-05      1.4832e+06          5415.2          3586.8
v  turbulent_viscosity      1.5662e-07           2.557        0.091033        0.049873
v  CourantNb                   0.65241      1.5808e+05          529.01          322.66
v  FourierNb                    6.4265          6220.7          207.04          91.848
v  total_pressure           4.8397e+05      5.4375e+05      5.1505e+05      5.1056e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.7772      1.5933e+05          736.04          414.51


 TIME FOR THE TIME STEP               82:        0.52793E+01

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


 INSTANT    0.830000000E+01   TIME STEP NUMBER              83
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.194168249E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273287576E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23522E+03 0.81298E+02
   Friction velocity        uet   :  0.98270E-02 0.10069E+02
   Friction velocity        uk    :  0.98258E-02 0.68094E+01
   Dimensionless distance   yplus :  0.12996E+00 0.93214E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        382
   Nb of faces within the viscous sub-layer     :       2347
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.26227E+02    3347   0.99715E+00   0.10354E+01 
c  VelocityY    0.26227E+02    3347   0.99715E+00   0.00000E+00 
c  VelocityZ    0.26227E+02    3347   0.99715E+00   0.00000E+00 
c  Pressure     0.15520E+01     603   0.78410E-02   0.11893E+00 
c  k            0.31480E+03     267   0.50637E-03   0.30529E+02 
c  epsilon      0.14974E+07     160   0.81914E-03   0.13203E+10 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -0.00014932                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -104.9          39.398        -0.29584        -0.14035
v  Velocity[Y]                  -60.72          109.38          0.6722         0.43295
v  Velocity[Z]                  -64.24          37.063        0.021046       -0.027662
v  ǁVelocityǁ                 0.015179          124.35          1.9596          1.4789
v  Pressure                     -17481           46271           15784           11051
v  k                        8.4761e-07          195.14          2.3362          1.4002
v  epsilon                  0.00014932      1.9177e+06          7295.1          4751.4
v  turbulent_viscosity       4.634e-07          2.8148        0.095874        0.053986
v  CourantNb                   0.17398       1.744e+05          549.38          336.06
v  FourierNb                    6.3269          6474.3          212.76          95.728
v  total_pressure           4.8252e+05      5.4627e+05      5.1578e+05      5.1105e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.1542      1.7565e+05          762.13          431.79


 TIME FOR THE TIME STEP               83:        0.55836E+01

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


 INSTANT    0.840000000E+01   TIME STEP NUMBER              84
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.285858655E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273286493E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29808E+03 0.81737E+02
   Friction velocity        uet   :  0.20383E-01 0.11660E+02
   Friction velocity        uk    :  0.21135E-01 0.73001E+01
   Dimensionless distance   yplus :  0.24601E+00 0.98962E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        378
   Nb of faces within the viscous sub-layer     :       2142
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.47539E+02    3231   0.99986E+00   0.13119E+01 
c  VelocityY    0.47539E+02    3231   0.99986E+00   0.00000E+00 
c  VelocityZ    0.47539E+02    3231   0.99986E+00   0.00000E+00 
c  Pressure     0.16713E+01     592   0.77064E-02   0.12076E+00 
c  k            0.40827E+03     256   0.40879E-03   0.33090E+02 
c  epsilon      0.21757E+07     153   0.53880E-03   0.17197E+10 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00043223                             1
a  epsilon         -1.7917                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -119.32          41.016        -0.28866        -0.14544
v  Velocity[Y]                 -70.288          111.92          0.6869         0.44652
v  Velocity[Z]                 -65.795          42.163        0.029245       -0.035629
v  ǁVelocityǁ                 0.020303          142.08          2.0136          1.5165
v  Pressure                     -19008           49015           16519           11544
v  k                        2.1809e-06          227.46          2.7634          1.6448
v  epsilon                  0.00012575      2.2646e+06          9573.6          6176.8
v  turbulent_viscosity      3.5227e-08          3.0575         0.12312        0.066435
v  CourantNb                    0.1615       1.908e+05             589          355.51
v  FourierNb                    6.4369            6951          261.65          112.99
v  total_pressure           4.8099e+05      5.4901e+05      5.1652e+05      5.1154e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.4877      1.9204e+05          850.65           468.5


 TIME FOR THE TIME STEP               84:        0.53921E+01

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


 INSTANT    0.850000000E+01   TIME STEP NUMBER              85
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.182550283E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273288477E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30813E+03 0.93536E+02
   Friction velocity        uet   :  0.10907E-01 0.11909E+02
   Friction velocity        uk    :  0.19661E-01 0.78556E+01
   Dimensionless distance   yplus :  0.26755E+00 0.10056E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        319
   Nb of faces within the viscous sub-layer     :       2225
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.22963E+02    3780   0.99720E+00   0.10809E+01 
c  VelocityY    0.22963E+02    3780   0.99720E+00   0.00000E+00 
c  VelocityZ    0.22963E+02    3780   0.99720E+00   0.00000E+00 
c  Pressure     0.17637E+01     591   0.77646E-02   0.12014E+00 
c  k            0.50025E+03     250   0.40178E-03   0.31578E+02 
c  epsilon      0.29352E+07     152   0.69867E-03   0.24947E+10 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00011353                             5
a  epsilon       -0.027258                             5


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -121.28            44.7        -0.30791         -0.1484
v  Velocity[Y]                 -69.963          132.05         0.70075         0.45943
v  Velocity[Z]                 -69.631          42.842        0.011778       -0.034364
v  ǁVelocityǁ                 0.013503          143.79          2.0832          1.5682
v  Pressure                     -20686           51896           17339           12102
v  k                        2.2851e-06          264.54          3.0535          1.7997
v  epsilon                  0.00036189      3.1814e+06           11916          7552.8
v  turbulent_viscosity      1.5399e-06          3.1005          0.1272        0.067612
v  CourantNb                   0.09658      2.1108e+05          610.52          367.37
v  FourierNb                     6.402          6885.7          269.39          115.41
v  total_pressure           4.7931e+05       5.519e+05      5.1734e+05       5.121e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.0974      2.1232e+05          879.91          482.77


 TIME FOR THE TIME STEP               85:        0.61791E+01

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


 INSTANT    0.860000000E+01   TIME STEP NUMBER              86
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.601030525E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273288418E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38802E+03 0.95696E+02
   Friction velocity        uet   :  0.13246E-01 0.13902E+02
   Friction velocity        uk    :  0.29607E-01 0.85571E+01
   Dimensionless distance   yplus :  0.41180E+00 0.10811E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        279
   Nb of faces within the viscous sub-layer     :       2116
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.60919E+02    3446   0.99994E+00   0.14808E+01 
c  VelocityY    0.60919E+02    3446   0.99994E+00   0.00000E+00 
c  VelocityZ    0.60919E+02    3446   0.99994E+00   0.00000E+00 
c  Pressure     0.18807E+01     588   0.77303E-02   0.12076E+00 
c  k            0.61868E+03     251   0.35242E-03   0.34815E+02 
c  epsilon      0.39590E+07     146   0.45587E-03   0.26514E+10 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.0581e-05                             1
a  epsilon         -1.1124                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -135.66          44.969        -0.30169        -0.15288
v  Velocity[Y]                 -78.735          135.12         0.76096         0.47017
v  Velocity[Z]                 -73.768          45.995        0.012552       -0.037426
v  ǁVelocityǁ                 0.021744          160.33           2.228          1.6783
v  Pressure                     -22445           54994           18157           12655
v  k                        4.1692e-06          288.23          3.4006          2.0659
v  epsilon                  0.00042015      3.4985e+06           14450          9252.2
v  turbulent_viscosity      9.4857e-08          3.2451         0.12154        0.065084
v  CourantNb                  0.061377      2.2892e+05           635.8          382.68
v  FourierNb                    6.4727          7175.7          259.22          111.83
v  total_pressure           4.7755e+05      5.5499e+05      5.1816e+05      5.1266e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.5068      2.3016e+05          895.02          494.52


 TIME FOR THE TIME STEP               86:        0.57020E+01

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


 INSTANT    0.870000000E+01   TIME STEP NUMBER              87
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.298246660E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273287512E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40559E+03 0.10687E+03
   Friction velocity        uet   :  0.50406E-02 0.14172E+02
   Friction velocity        uk    :  0.33952E-01 0.88617E+01
   Dimensionless distance   yplus :  0.31770E+00 0.11101E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        215
   Nb of faces within the viscous sub-layer     :       1934
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30798E+02    3799   0.99678E+00   0.13372E+01 
c  VelocityY    0.30798E+02    3799   0.99678E+00   0.00000E+00 
c  VelocityZ    0.30798E+02    3799   0.99678E+00   0.00000E+00 
c  Pressure     0.19882E+01     596   0.78107E-02   0.12030E+00 
c  k            0.74457E+03     275   0.33335E-03   0.41689E+02 
c  epsilon      0.51759E+07     146   0.45989E-03   0.38906E+10 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00014706                             4
a  epsilon      -0.0092973                             4


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -136.96          50.104        -0.30068        -0.15624
v  Velocity[Y]                 -79.547          159.08         0.80423         0.48167
v  Velocity[Z]                 -78.941          49.259       0.0083267         -0.0362
v  ǁVelocityǁ                 0.020465           162.4          2.2654          1.6891
v  Pressure                     -24345           58223           19095           13301
v  k                        9.0321e-07          325.97          3.8446          2.3025
v  epsilon                   0.0011524      3.9881e+06           17598           11114
v  turbulent_viscosity      3.3816e-07          3.3083         0.13127        0.074787
v  CourantNb                   0.36804      2.5229e+05          678.01          406.42
v  FourierNb                    6.6329          6891.2             271          119.73
v  total_pressure           4.7566e+05      5.5822e+05      5.1909e+05       5.133e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.681      2.5354e+05             949          526.15


 TIME FOR THE TIME STEP               87:        0.62207E+01

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


 INSTANT    0.880000000E+01   TIME STEP NUMBER              88
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.354373197E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273290014E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51612E+03 0.10878E+03
   Friction velocity        uet   :  0.20801E-01 0.16489E+02
   Friction velocity        uk    :  0.26823E-01 0.94457E+01
   Dimensionless distance   yplus :  0.33033E+00 0.11777E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        191
   Nb of faces within the viscous sub-layer     :       1990
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         10 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.78030E+02    3626   0.99976E+00   0.16914E+01 
c  VelocityY    0.78030E+02    3626   0.99976E+00   0.00000E+00 
c  VelocityZ    0.78030E+02    3626   0.99976E+00   0.00000E+00 
c  Pressure     0.21307E+01     591   0.77039E-02   0.12146E+00 
c  k            0.90263E+03     227   0.29204E-03   0.47862E+02 
c  epsilon      0.67577E+07     139   0.45225E-03   0.49219E+10 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00056516                             1
a  epsilon       -0.015654                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -153.87          52.751        -0.31256        -0.16523
v  Velocity[Y]                 -89.912          162.55         0.80617         0.49513
v  Velocity[Z]                 -83.194          54.315       -0.014534       -0.044803
v  ǁVelocityǁ                 0.015539          182.24          2.4375          1.8102
v  Pressure                     -26376           61686           20010           13922
v  k                        3.0243e-06          373.97          4.3522           2.614
v  epsilon                   0.0011748      5.1044e+06           21095           13388
v  turbulent_viscosity      8.6872e-09          3.5156         0.13607         0.07862
v  CourantNb                    1.3086      2.7606e+05          698.67          417.57
v  FourierNb                    5.9358          7125.8           277.2          123.47
v  total_pressure           4.7362e+05      5.6169e+05      5.2001e+05      5.1392e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            9.06       2.773e+05          975.87          541.04


 TIME FOR THE TIME STEP               88:        0.59418E+01

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


 INSTANT    0.890000000E+01   TIME STEP NUMBER              89
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.135960461E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273289257E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53801E+03 0.12214E+03
   Friction velocity        uet   :  0.12378E-01 0.16795E+02
   Friction velocity        uk    :  0.20011E-01 0.10218E+02
   Dimensionless distance   yplus :  0.21195E+00 0.12715E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        178
   Nb of faces within the viscous sub-layer     :       1806
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.38518E+02    3824   0.99780E+00   0.19699E+01 
c  VelocityY    0.38518E+02    3824   0.99780E+00   0.00000E+00 
c  VelocityZ    0.38518E+02    3824   0.99780E+00   0.00000E+00 
c  Pressure     0.22528E+01     594   0.77903E-02   0.12095E+00 
c  k            0.10729E+04     261   0.26990E-03   0.57473E+02 
c  epsilon      0.86338E+07     139   0.41042E-03   0.67076E+10 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.9328e-05                             3
a  epsilon       -0.011804                             2


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -155.7          56.303         -0.3335        -0.16813
v  Velocity[Y]                 -90.728          190.89         0.84242         0.50469
v  Velocity[Z]                 -88.675           59.43       -0.011967       -0.041294
v  ǁVelocityǁ                  0.01852           194.6          2.5103          1.8534
v  Pressure                     -28568           65348           21067           14654
v  k                        3.7496e-06          420.79          4.8324          2.9078
v  epsilon                  0.00036366      6.1539e+06           25289           15907
v  turbulent_viscosity      2.1064e-07          3.7527         0.15368        0.086345
v  CourantNb                   0.71461      3.0447e+05           750.2          445.11
v  FourierNb                    5.9902          7467.8          309.86          134.47
v  total_pressure           4.7143e+05      5.6535e+05      5.2107e+05      5.1465e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          13.203      3.0572e+05          1060.1          579.57


 TIME FOR THE TIME STEP               89:        0.62089E+01

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


 INSTANT    0.900000000E+01   TIME STEP NUMBER              90
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.216713975E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273291109E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66495E+03 0.12444E+03
   Friction velocity        uet   :  0.48805E-02 0.19559E+02
   Friction velocity        uk    :  0.30722E-01 0.10865E+02
   Dimensionless distance   yplus :  0.26291E+00 0.13203E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        182
   Nb of faces within the viscous sub-layer     :       1837
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10056E+03    3710   0.10002E+01   0.19095E+01 
c  VelocityY    0.10056E+03    3710   0.10002E+01   0.00000E+00 
c  VelocityZ    0.10056E+03    3710   0.10002E+01   0.00000E+00 
c  Pressure     0.24169E+01     592   0.77378E-02   0.12222E+00 
c  k            0.12868E+04     216   0.25208E-03   0.66298E+02 
c  epsilon      0.11115E+08     136   0.33961E-03   0.80969E+10 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.7812e-06                             1
a  epsilon         -2.4561                            12


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -176.12          58.881        -0.34352        -0.17803
v  Velocity[Y]                 -102.83          197.74         0.85354         0.52213
v  Velocity[Z]                  -94.44          65.291       -0.030506       -0.049079
v  ǁVelocityǁ                 0.013324          208.55          2.6647          1.9577
v  Pressure                     -30859           69324           22147           15391
v  k                        7.9372e-07          477.44          5.4376          3.2865
v  epsilon                  0.00067876      7.1604e+06           30068           18995
v  turbulent_viscosity      1.0845e-07           3.923         0.14958        0.088983
v  CourantNb                   0.23766      3.3041e+05          779.61          462.18
v  FourierNb                    6.2916          7825.2          296.53          133.55
v  total_pressure           4.6914e+05      5.6932e+05      5.2215e+05      5.1539e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.747      3.3165e+05          1076.1          595.73


 TIME FOR THE TIME STEP               90:        0.60660E+01

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


 INSTANT    0.910000000E+01   TIME STEP NUMBER              91
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.568674315E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273291182E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70201E+03 0.14058E+03
   Friction velocity        uet   :  0.40432E-02 0.20190E+02
   Friction velocity        uk    :  0.24383E-01 0.11582E+02
   Dimensionless distance   yplus :  0.27347E+00 0.13753E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        174
   Nb of faces within the viscous sub-layer     :       1766
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.48032E+02    3912   0.99865E+00   0.21669E+01 
c  VelocityY    0.48032E+02    3912   0.99865E+00   0.00000E+00 
c  VelocityZ    0.48032E+02    3912   0.99865E+00   0.00000E+00 
c  Pressure     0.25517E+01     609   0.77801E-02   0.12152E+00 
c  k            0.15225E+04     256   0.31037E-03   0.97179E+02 
c  epsilon      0.14083E+08     144   0.45185E-03   0.14204E+11 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.1289e-05                             8
a  epsilon        -0.17041                            11


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -176.59          64.658        -0.37901        -0.18691
v  Velocity[Y]                 -102.85          229.78         0.90374          0.5353
v  Velocity[Z]                 -100.24          70.709       -0.041641       -0.045357
v  ǁVelocityǁ                 0.016339          233.64          2.7534          1.9955
v  Pressure                     -33310           73514           23380           16247
v  k                        1.5809e-06          529.96          6.1077          3.6536
v  epsilon                  5.1351e-05      9.0911e+06           35885           22481
v  turbulent_viscosity      1.3664e-09          4.1334         0.16532        0.095708
v  CourantNb                  0.093121      3.6808e+05          830.72          488.98
v  FourierNb                     6.703          8248.9          326.64          143.22
v  total_pressure           4.6669e+05      5.7351e+05      5.2338e+05      5.1625e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.799      3.6932e+05          1157.4           632.2


 TIME FOR THE TIME STEP               91:        0.63383E+01

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


 INSTANT    0.920000000E+01   TIME STEP NUMBER              92
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.609334833E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273289424E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89053E+03 0.14159E+03
   Friction velocity        uet   :  0.48672E-02 0.23149E+02
   Friction velocity        uk    :  0.31402E-01 0.12334E+02
   Dimensionless distance   yplus :  0.29437E+00 0.14714E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        180
   Nb of faces within the viscous sub-layer     :       1856
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         13 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.12919E+03    3876   0.99985E+00   0.27610E+01 
c  VelocityY    0.12919E+03    3876   0.99985E+00   0.00000E+00 
c  VelocityZ    0.12919E+03    3876   0.99985E+00   0.00000E+00 
c  Pressure     0.27310E+01     591   0.76944E-02   0.12252E+00 
c  k            0.18019E+04     216   0.23503E-03   0.97729E+02 
c  epsilon      0.17832E+08     135   0.30516E-03   0.14976E+11 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0011528                             2
a  epsilon      -0.0087203                             3


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -199.17          67.718        -0.36202        -0.19069
v  Velocity[Y]                 -116.54           237.7         0.90573         0.55511
v  Velocity[Z]                 -105.08           78.87       -0.039824       -0.054562
v  ǁVelocityǁ                 0.015066          242.99          2.9818          2.1619
v  Pressure                     -35961           77974           24563           17048
v  k                         3.651e-06             598          6.8888          4.1366
v  epsilon                  4.6413e-07      1.0486e+07           42409           26647
v  turbulent_viscosity      1.2306e-08          4.1492         0.17017        0.099938
v  CourantNb                   0.34102      4.0023e+05          866.14          506.87
v  FourierNb                    6.3186          8295.3          331.61          147.12
v  total_pressure           4.6404e+05      5.7797e+05      5.2456e+05      5.1705e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.1511      4.0147e+05          1197.7          653.99


 TIME FOR THE TIME STEP               92:        0.62958E+01

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


 INSTANT    0.930000000E+01   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.424777673E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273291575E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93424E+03 0.15960E+03
   Friction velocity        uet   :  0.71951E-02 0.23875E+02
   Friction velocity        uk    :  0.26339E-01 0.12968E+02
   Dimensionless distance   yplus :  0.15655E+00 0.15522E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        177
   Nb of faces within the viscous sub-layer     :       1602
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.63465E+02    4003   0.99904E+00   0.32320E+01 
c  VelocityY    0.63465E+02    4003   0.99904E+00   0.00000E+00 
c  VelocityZ    0.63465E+02    4003   0.99904E+00   0.00000E+00 
c  Pressure     0.28908E+01     609   0.77520E-02   0.12210E+00 
c  k            0.21091E+04     293   0.26428E-03   0.12422E+03 
c  epsilon      0.22191E+08     139   0.35804E-03   0.21148E+11 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.9454e-06                             1
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -201.09          72.024        -0.39756        -0.19873
v  Velocity[Y]                 -117.45          278.61          1.0018         0.56893
v  Velocity[Z]                 -112.48          84.629       -0.058829       -0.049173
v  ǁVelocityǁ                 0.010835          283.68          3.0342          2.1891
v  Pressure                     -38821           82652           25908           17976
v  k                        1.9454e-06           660.2          7.6435          4.5958
v  epsilon                  0.00076193      1.2302e+07           49887           31221
v  turbulent_viscosity      3.4989e-07          4.3339         0.20284         0.11569
v  CourantNb                   0.37181      4.4506e+05          932.87          543.65
v  FourierNb                    6.8493            8637          390.78          167.99
v  total_pressure           4.6118e+05      5.8265e+05      5.2591e+05      5.1798e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           12.34       4.463e+05          1323.6          711.64


 TIME FOR THE TIME STEP               93:        0.64730E+01

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


 INSTANT    0.940000000E+01   TIME STEP NUMBER              94
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.395393722E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273290022E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11480E+04 0.16197E+03
   Friction velocity        uet   :  0.13846E-01 0.27774E+02
   Friction velocity        uk    :  0.36538E-01 0.13576E+02
   Dimensionless distance   yplus :  0.32420E+00 0.16064E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        197
   Nb of faces within the viscous sub-layer     :       1613
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.16555E+03    3928   0.10000E+01   0.37017E+01 
c  VelocityY    0.16555E+03    3928   0.10000E+01   0.00000E+00 
c  VelocityZ    0.16555E+03    3928   0.10000E+01   0.00000E+00 
c  Pressure     0.31020E+01     592   0.77181E-02   0.12332E+00 
c  k            0.25154E+04     258   0.22964E-03   0.17184E+03 
c  epsilon      0.27966E+08     134   0.29524E-03   0.28958E+11 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -1.3995                             6


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -226.42          77.553        -0.42172        -0.20542
v  Velocity[Y]                 -132.66          289.27          0.9395         0.59152
v  Velocity[Z]                 -120.01          94.908       -0.079592       -0.057114
v  ǁVelocityǁ                 0.016473          294.87          3.3041          2.3629
v  Pressure                     -41838           87698           27271           18904
v  k                        2.1655e-06          732.78          8.7081          5.2185
v  epsilon                  0.00017306      1.4321e+07           59295           37221
v  turbulent_viscosity      1.3903e-08          4.5335         0.21306         0.12561
v  CourantNb                   0.21939       4.829e+05          960.11          560.01
v  FourierNb                    6.3685          9060.8          402.36          176.47
v  total_pressure           4.5816e+05       5.877e+05      5.2727e+05       5.189e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.5758      4.8414e+05          1362.5          736.48


 TIME FOR THE TIME STEP               94:        0.63789E+01

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


 INSTANT    0.950000000E+01   TIME STEP NUMBER              95
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.113187074E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273293499E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12246E+04 0.18200E+03
   Friction velocity        uet   :  0.11407E-01 0.28679E+02
   Friction velocity        uk    :  0.23737E-01 0.14473E+02
   Dimensionless distance   yplus :  0.30825E+00 0.16925E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        203
   Nb of faces within the viscous sub-layer     :       1348
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.85364E+02    4085   0.10000E+01   0.43584E+01 
c  VelocityY    0.85364E+02    4085   0.10000E+01   0.00000E+00 
c  VelocityZ    0.85364E+02    4085   0.10000E+01   0.00000E+00 
c  Pressure     0.32767E+01     603   0.77997E-02   0.12257E+00 
c  k            0.29614E+04     273   0.26983E-03   0.25018E+03 
c  epsilon      0.34823E+08     135   0.34434E-03   0.53365E+11 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon      -0.0072541                             3


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -229.82          84.393        -0.43479        -0.21431
v  Velocity[Y]                 -139.62          334.04          1.0134         0.61262
v  Velocity[Z]                 -126.46          103.86       -0.096135       -0.054326
v  ǁVelocityǁ                 0.011649          340.83          3.3334          2.4103
v  Pressure                     -45134           93004           28793           19951
v  k                        3.4485e-06          828.22          9.9071          5.8369
v  epsilon                  0.00033382      1.8109e+07           71457           44221
v  turbulent_viscosity      2.1461e-06          4.7308         0.24516         0.13637
v  CourantNb                   0.17934       5.357e+05          1041.3          600.91
v  FourierNb                    6.5618          9367.7          465.24          195.35
v  total_pressure           4.5487e+05        5.93e+05      5.2879e+05      5.1995e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           13.59      5.3694e+05          1506.5          796.26


 TIME FOR THE TIME STEP               95:        0.65793E+01

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


 INSTANT    0.960000000E+01   TIME STEP NUMBER              96
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.911551314E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273290572E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15306E+04 0.18609E+03
   Friction velocity        uet   :  0.13427E-01 0.32745E+02
   Friction velocity        uk    :  0.32111E-01 0.15524E+02
   Dimensionless distance   yplus :  0.30714E+00 0.18010E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        222
   Nb of faces within the viscous sub-layer     :       1417
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.21180E+03    4033   0.10003E+01   0.47925E+01 
c  VelocityY    0.21180E+03    4033   0.10003E+01   0.00000E+00 
c  VelocityZ    0.21180E+03    4033   0.10003E+01   0.00000E+00 
c  Pressure     0.35233E+01     587   0.76615E-02   0.12407E+00 
c  k            0.35805E+04     232   0.25722E-03   0.25602E+03 
c  epsilon      0.44471E+08     133   0.34702E-03   0.59359E+11 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00026368                             6
a  epsilon        -0.55863                            18


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -257.01          88.425        -0.46485        -0.23104
v  Velocity[Y]                 -156.97          350.13          1.0757         0.63082
v  Velocity[Z]                 -133.23          112.52        -0.09536       -0.065334
v  ǁVelocityǁ                 0.015545          356.76          3.6723          2.5846
v  Pressure                     -48673           98623           30228           20920
v  k                        5.9459e-06          917.88          10.812          6.6243
v  epsilon                   0.0010895      2.0347e+07           83382           52747
v  turbulent_viscosity      1.8213e-06          5.0103         0.25789         0.14458
v  CourantNb                    0.3787       5.823e+05          1067.6          620.98
v  FourierNb                    6.7251           10394          483.23           204.6
v  total_pressure           4.5133e+05      5.9862e+05      5.3023e+05      5.2092e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.758      5.8354e+05          1550.8          825.57


 TIME FOR THE TIME STEP               96:        0.65203E+01

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


 INSTANT    0.970000000E+01   TIME STEP NUMBER              97
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.359844643E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273291189E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15779E+04 0.20748E+03
   Friction velocity        uet   :  0.51230E-02 0.34365E+02
   Friction velocity        uk    :  0.33291E-01 0.16192E+02
   Dimensionless distance   yplus :  0.23998E+00 0.18723E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        197
   Nb of faces within the viscous sub-layer     :       1399
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10795E+03    4117   0.10011E+01   0.51598E+01 
c  VelocityY    0.10795E+03    4117   0.10011E+01   0.00000E+00 
c  VelocityZ    0.10795E+03    4117   0.10011E+01   0.00000E+00 
c  Pressure     0.37201E+01     605   0.77379E-02   0.12325E+00 
c  k            0.42375E+04     286   0.28057E-03   0.41813E+03 
c  epsilon      0.55848E+08     135   0.39810E-03   0.10866E+12 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00015195                             7
a  epsilon       -0.063645                            10


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -260.33          93.243         -0.4774        -0.23287
v  Velocity[Y]                 -168.36           402.4           1.119         0.65197
v  Velocity[Z]                 -142.51          122.07        -0.16902       -0.061725
v  ǁVelocityǁ                 0.030249          409.09          3.7347          2.6844
v  Pressure                     -52439      1.0457e+05           31949           22106
v  k                        5.7114e-06          1043.5          12.395          7.4307
v  epsilon                  0.00038472      2.4094e+07      1.0099e+05           63151
v  turbulent_viscosity      1.2614e-07          5.2845         0.28192         0.16238
v  CourantNb                   0.31655      6.4934e+05          1165.4          664.78
v  FourierNb                     6.516           10496          521.27          222.01
v  total_pressure           4.4756e+05      6.0457e+05      5.3195e+05      5.2211e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.818      6.5058e+05          1686.7          886.78


 TIME FOR THE TIME STEP               97:        0.66257E+01

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


 INSTANT    0.980000000E+01   TIME STEP NUMBER              98
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.373352246E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273291317E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20177E+04 0.21140E+03
   Friction velocity        uet   :  0.40317E-02 0.38859E+02
   Friction velocity        uk    :  0.23000E-01 0.17067E+02
   Dimensionless distance   yplus :  0.30486E+00 0.20286E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        288
   Nb of faces within the viscous sub-layer     :       1158
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.27364E+03    3996   0.99978E+00   0.67215E+01 
c  VelocityY    0.27364E+03    3996   0.99978E+00   0.00000E+00 
c  VelocityZ    0.27364E+03    3996   0.99978E+00   0.00000E+00 
c  Pressure     0.39947E+01     592   0.76790E-02   0.12451E+00 
c  k            0.51289E+04     328   0.26862E-03   0.51385E+03 
c  epsilon      0.71503E+08     140   0.30593E-03   0.14275E+12 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -289.06          101.19          -0.477         -0.2433
v  Velocity[Y]                 -188.31          418.46          1.0839         0.67404
v  Velocity[Z]                 -152.47          138.02        -0.16803        -0.06739
v  ǁVelocityǁ                 0.035235          427.78           4.162          2.9292
v  Pressure                     -56370      1.1098e+05           33689           23291
v  k                        6.1631e-05          1178.7          14.534          8.7036
v  epsilon                   0.0030909      2.9415e+07      1.2187e+05           76669
v  turbulent_viscosity      1.5041e-07          5.6359         0.32036         0.17671
v  CourantNb                     1.253      7.0109e+05          1197.9          692.79
v  FourierNb                    6.2973           11909           590.9          245.66
v  total_pressure           4.4363e+05      6.1098e+05      5.3369e+05      5.2329e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          13.958      7.0233e+05          1788.8          938.45


 TIME FOR THE TIME STEP               98:        0.64840E+01

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


 INSTANT    0.990000000E+01   TIME STEP NUMBER              99
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.336846183E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273295793E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21123E+04 0.23430E+03
   Friction velocity        uet   :  0.48963E-02 0.40316E+02
   Friction velocity        uk    :  0.26932E-01 0.18426E+02
   Dimensionless distance   yplus :  0.38002E+00 0.22050E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        257
   Nb of faces within the viscous sub-layer     :        910
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.14395E+03    4379   0.99868E+00   0.83270E+01 
c  VelocityY    0.14395E+03    4379   0.99868E+00   0.00000E+00 
c  VelocityZ    0.14395E+03    4379   0.99868E+00   0.00000E+00 
c  Pressure     0.42396E+01     603   0.78306E-02   0.12424E+00 
c  k            0.61288E+04     357   0.28726E-03   0.74271E+03 
c  epsilon      0.90615E+08     140   0.40742E-03   0.24513E+12 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -296.01          109.15        -0.59939        -0.25757
v  Velocity[Y]                 -200.16          483.47          1.1407         0.70091
v  Velocity[Z]                 -162.51          145.89        -0.17128        -0.05992
v  ǁVelocityǁ                 0.019253          491.97          4.3164          3.0186
v  Pressure                     -60644      1.1782e+05           35589           24603
v  k                        7.9913e-06          1317.9          16.622           9.733
v  epsilon                  0.00038004      3.6513e+07      1.4821e+05           91681
v  turbulent_viscosity      3.7314e-06          6.0679         0.42131         0.22104
v  CourantNb                    1.7418       7.786e+05          1319.6          750.14
v  FourierNb                    6.6231           11963          775.77          309.11
v  total_pressure           4.3936e+05      6.1782e+05      5.3559e+05       5.246e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           12.04      7.7984e+05          2095.4          1059.2


 TIME FOR THE TIME STEP               99:        0.70280E+01

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


 INSTANT    0.100000000E+02   TIME STEP NUMBER             100
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.174111980E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273292454E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25490E+04 0.24186E+03
   Friction velocity        uet   :  0.99762E-02 0.46307E+02
   Friction velocity        uk    :  0.25091E-01 0.19525E+02
   Dimensionless distance   yplus :  0.28181E+00 0.22560E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        249
   Nb of faces within the viscous sub-layer     :        875
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on         82


 Write intermediate restart files
   checkpoint at iteration        100, Physical time    0.10000E+02


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

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

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

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


 Time for restart files:    0.10927E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.35329E+03    4141   0.10003E+01   0.84951E+01 
c  VelocityY    0.35329E+03    4141   0.10003E+01   0.00000E+00 
c  VelocityZ    0.35329E+03    4141   0.10003E+01   0.00000E+00 
c  Pressure     0.45566E+01     569   0.76879E-02   0.12559E+00 
c  k            0.73543E+04     291   0.28209E-03   0.91964E+03 
c  epsilon      0.11584E+09     135   0.40731E-03   0.31869E+12 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.002044                             3
a  epsilon         -4.7336                            24


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -334.82          113.69        -0.60171        -0.26496
v  Velocity[Y]                 -226.89          506.21          1.1964          0.7446
v  Velocity[Z]                 -171.44          162.65        -0.21393       -0.084053
v  ǁVelocityǁ                 0.038035          515.37          4.7138          3.3443
v  Pressure                     -65372      1.2497e+05           37213           25679
v  k                        7.8034e-05            1522          18.651          11.107
v  epsilon                   0.0091541      4.0902e+07        1.76e+05      1.1061e+05
v  turbulent_viscosity       3.653e-07          6.3805         0.42295          0.2265
v  CourantNb                   0.23484      8.4887e+05          1384.9          785.73
v  FourierNb                    6.3694           13506          771.59          311.91
v  total_pressure           4.3463e+05      6.2497e+05      5.3721e+05      5.2568e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.783      8.5011e+05          2156.5          1097.6


 TIME FOR THE TIME STEP              100:        0.66718E+01

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


 INSTANT    0.101000000E+02   TIME STEP NUMBER             101
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.127294973E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273293929E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27574E+04 0.27274E+03
   Friction velocity        uet   :  0.10843E-02 0.48149E+02
   Friction velocity        uk    :  0.47474E-01 0.20611E+02
   Dimensionless distance   yplus :  0.36605E+00 0.23748E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        245
   Nb of faces within the viscous sub-layer     :        617
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.18652E+03    4355   0.99894E+00   0.11235E+02 
c  VelocityY    0.18652E+03    4355   0.99894E+00   0.00000E+00 
c  VelocityZ    0.18652E+03    4355   0.99894E+00   0.00000E+00 
c  Pressure     0.47968E+01     591   0.76992E-02   0.12426E+00 
c  k            0.88252E+04     329   0.32014E-03   0.14058E+04 
c  epsilon      0.14785E+09     149   0.38727E-03   0.52325E+12 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -334.97          122.04        -0.56223         -0.2792
v  Velocity[Y]                 -242.62          579.59          1.3675         0.74743
v  Velocity[Z]                 -179.27          179.71        -0.16596       -0.071022
v  ǁVelocityǁ                 0.019308          591.22          4.7378          3.3615
v  Pressure                     -70288      1.3258e+05           39276           27087
v  k                        0.00036162          1697.8          20.913          12.482
v  epsilon                    0.059489      5.1403e+07      2.1305e+05      1.3329e+05
v  turbulent_viscosity       1.183e-06          6.7952          0.4361         0.23589
v  CourantNb                   0.58194      9.4191e+05          1494.4           848.7
v  FourierNb                    6.6769           13577          793.31          321.05
v  total_pressure           4.2971e+05      6.3258e+05      5.3928e+05      5.2709e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          13.135      9.4316e+05          2287.7          1169.8


 TIME FOR THE TIME STEP              101:        0.73327E+01

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


 INSTANT    0.102000000E+02   TIME STEP NUMBER             102
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.954413349E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273297221E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34257E+04 0.27434E+03
   Friction velocity        uet   :  0.50645E-02 0.54495E+02
   Friction velocity        uk    :  0.45961E-01 0.21955E+02
   Dimensionless distance   yplus :  0.20215E+00 0.26265E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        376
   Nb of faces within the viscous sub-layer     :        753
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.45150E+03    4284   0.10004E+01   0.13044E+02 
c  VelocityY    0.45150E+03    4284   0.10004E+01   0.00000E+00 
c  VelocityZ    0.45150E+03    4284   0.10004E+01   0.00000E+00 
c  Pressure     0.51634E+01     589   0.76916E-02   0.12574E+00 
c  k            0.10738E+05     364   0.26146E-03   0.13412E+04 
c  epsilon      0.19078E+09     136   0.32466E-03   0.62061E+12 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00012139                             2
a  epsilon         -3.1853                            17


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                    -378          130.41        -0.57546        -0.29505
v  Velocity[Y]                 -271.51          608.16          1.4802         0.78299
v  Velocity[Z]                 -194.86          195.44        -0.19762       -0.095333
v  ǁVelocityǁ                 0.031896          619.74          5.1409          3.5885
v  Pressure                     -75590       1.407e+05           41294           28453
v  k                        0.00010285          1955.1          22.844          13.816
v  epsilon                  0.00078155      6.1934e+07      2.5419e+05      1.5956e+05
v  turbulent_viscosity      3.2737e-06          7.3293         0.42359         0.23757
v  CourantNb                   0.31998      1.0148e+06          1529.1          872.62
v  FourierNb                    6.3543           15059          761.09          316.17
v  total_pressure           4.2441e+05       6.407e+05      5.4129e+05      5.2845e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.585      1.0161e+06          2290.2          1188.8


 TIME FOR THE TIME STEP              102:        0.68645E+01

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


 INSTANT    0.103000000E+02   TIME STEP NUMBER             103
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.534680484E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273296251E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34855E+04 0.30876E+03
   Friction velocity        uet   :  0.20142E-02 0.57361E+02
   Friction velocity        uk    :  0.29648E-01 0.23609E+02
   Dimensionless distance   yplus :  0.32825E+00 0.27296E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        318
   Nb of faces within the viscous sub-layer     :        714
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.23196E+03    4266   0.10015E+01   0.13913E+02 
c  VelocityY    0.23196E+03    4266   0.10015E+01   0.00000E+00 
c  VelocityZ    0.23196E+03    4266   0.10015E+01   0.00000E+00 
c  Pressure     0.54664E+01     609   0.77005E-02   0.12511E+00 
c  k            0.12935E+05     261   0.32904E-03   0.23390E+04 
c  epsilon      0.24446E+09     139   0.45847E-03   0.11798E+13 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon       -0.058845                             1


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -380.83          140.51         -0.6665        -0.31735
v  Velocity[Y]                 -291.35          697.23            1.42         0.80136
v  Velocity[Z]                 -201.57          213.53        -0.17063       -0.078238
v  ǁVelocityǁ                 0.028642          708.98          5.2535          3.6374
v  Pressure                     -81011      1.4954e+05           43850           30215
v  k                         2.914e-05          2239.2          26.936          15.905
v  epsilon                   0.0033849      7.7611e+07      3.1088e+05      1.9323e+05
v  turbulent_viscosity      3.7986e-06          50.433         0.36103         0.21015
v  CourantNb                   0.10075      1.1332e+06          1656.6          929.85
v  FourierNb                    6.3304           54988          646.89          276.46
v  total_pressure           4.1899e+05      6.4954e+05      5.4385e+05      5.3021e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.3998      1.1344e+06          2303.5          1206.3


 TIME FOR THE TIME STEP              103:        0.68597E+01

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


 INSTANT    0.104000000E+02   TIME STEP NUMBER             104
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.453671717E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273296447E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44462E+04 0.31252E+03
   Friction velocity        uet   :  0.83764E-02 0.64756E+02
   Friction velocity        uk    :  0.37480E-01 0.25339E+02
   Dimensionless distance   yplus :  0.51717E+00 0.29769E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        361
   Nb of faces within the viscous sub-layer     :        937
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.58437E+03    4325   0.10001E+01   0.14801E+02 
c  VelocityY    0.58437E+03    4325   0.10001E+01   0.00000E+00 
c  VelocityZ    0.58437E+03    4325   0.10001E+01   0.00000E+00 
c  Pressure     0.58832E+01     587   0.76196E-02   0.12651E+00 
c  k            0.15702E+05     274   0.27369E-03   0.22866E+04 
c  epsilon      0.31566E+09     136   0.34796E-03   0.14750E+13 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0002692                             3
a  epsilon          -2.956                            38


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -430.19          145.93        -0.74729        -0.35029
v  Velocity[Y]                 -327.75          729.65          1.4626         0.84333
v  Velocity[Z]                 -217.47          236.62        -0.30434        -0.11293
v  ǁVelocityǁ                 0.041907           745.1          5.9712          4.1633
v  Pressure                     -87175      1.5867e+05           46109           31724
v  k                        2.6771e-05          2551.4          30.616          18.206
v  epsilon                    0.005721      9.0635e+07      3.7399e+05      2.3402e+05
v  turbulent_viscosity      2.8009e-07          8.4045         0.44216         0.24479
v  CourantNb                   0.20339      1.2277e+06          1718.8          964.21
v  FourierNb                    6.7339           17162          791.89          327.53
v  total_pressure           4.1283e+05      6.5867e+05      5.4611e+05      5.3172e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.567      1.2289e+06          2510.7          1291.7


 TIME FOR THE TIME STEP              104:        0.69119E+01

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


 INSTANT    0.105000000E+02   TIME STEP NUMBER             105
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.144405208E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273297036E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46744E+04 0.35330E+03
   Friction velocity        uet   :  0.88868E-02 0.67556E+02
   Friction velocity        uk    :  0.21683E-01 0.26830E+02
   Dimensionless distance   yplus :  0.25059E+00 0.31066E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :        505
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.32210E+03    4583   0.10007E+01   0.18954E+02 
c  VelocityY    0.32210E+03    4583   0.10007E+01   0.00000E+00 
c  VelocityZ    0.32210E+03    4583   0.10007E+01   0.00000E+00 
c  Pressure     0.62226E+01     592   0.77135E-02   0.12573E+00 
c  k            0.18912E+05     280   0.29376E-03   0.31998E+04 
c  epsilon      0.40620E+09     137   0.44650E-03   0.24649E+13 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -436.3           157.6        -0.74267        -0.33608
v  Velocity[Y]                 -351.18          838.96          1.5703         0.87461
v  Velocity[Z]                 -231.94          254.35         -0.3756       -0.094143
v  ǁVelocityǁ                 0.022416          853.98          5.9218          4.1093
v  Pressure                     -93503      1.6852e+05           48789           33561
v  k                        0.00014942          2928.4          34.322          20.254
v  epsilon                    0.032124      1.1079e+08      4.5514e+05      2.8171e+05
v  turbulent_viscosity      1.9201e-08          8.9082         0.55949          0.3056
v  CourantNb                    1.7786        1.36e+06          1911.8          1067.7
v  FourierNb                    6.3675           17421          999.13          404.17
v  total_pressure            4.065e+05      6.6852e+05      5.4879e+05      5.3356e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          13.363      1.3613e+06          2910.9          1471.9


 TIME FOR THE TIME STEP              105:        0.73043E+01

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


 INSTANT    0.106000000E+02   TIME STEP NUMBER             106
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.985301237E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273303557E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56735E+04 0.36011E+03
   Friction velocity        uet   :  0.14430E-02 0.77097E+02
   Friction velocity        uk    :  0.42809E-01 0.28527E+02
   Dimensionless distance   yplus :  0.46044E+00 0.33107E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        497
   Nb of faces within the viscous sub-layer     :        526
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         31 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.74625E+03    4353   0.10000E+01   0.20943E+02 
c  VelocityY    0.74625E+03    4353   0.10000E+01   0.00000E+00 
c  VelocityZ    0.74625E+03    4353   0.10000E+01   0.00000E+00 
c  Pressure     0.67124E+01     591   0.76201E-02   0.12736E+00 
c  k            0.23091E+05     373   0.31047E-03   0.43781E+04 
c  epsilon      0.52789E+09     156   0.41649E-03   0.33771E+13 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -24.253                             9


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -485.85          168.07        -0.75604        -0.35883
v  Velocity[Y]                 -389.08          878.38           1.577         0.90556
v  Velocity[Z]                 -244.99          286.61        -0.31316        -0.10395
v  ǁVelocityǁ                  0.01521          895.23          6.6283          4.5231
v  Pressure                -1.0021e+05      1.7909e+05           51585           35463
v  k                        4.8764e-05          3288.6          40.273          24.069
v  epsilon                   0.0026142      1.3528e+08      5.5166e+05      3.4516e+05
v  turbulent_viscosity      1.2684e-06          9.6182         0.51706         0.29325
v  CourantNb                   0.20659      1.4764e+06          1941.6          1088.4
v  FourierNb                    6.7044           19377          909.36          380.59
v  total_pressure           3.9979e+05      6.7909e+05      5.5158e+05      5.3546e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          13.612      1.4776e+06            2851            1469


 TIME FOR THE TIME STEP              106:        0.69722E+01

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


 INSTANT    0.107000000E+02   TIME STEP NUMBER             107
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.533531958E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273302142E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60501E+04 0.40050E+03
   Friction velocity        uet   :  0.94397E-02 0.80337E+02
   Friction velocity        uk    :  0.44894E-01 0.30749E+02
   Dimensionless distance   yplus :  0.63671E+00 0.35950E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :        543
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.42487E+03    5088   0.99869E+00   0.21475E+02 
c  VelocityY    0.42487E+03    5088   0.99869E+00   0.00000E+00 
c  VelocityZ    0.42487E+03    5088   0.99869E+00   0.00000E+00 
c  Pressure     0.70980E+01     594   0.77466E-02   0.12651E+00 
c  k            0.27601E+05     353   0.30860E-03   0.54977E+04 
c  epsilon      0.67424E+09     137   0.37299E-03   0.49120E+13 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon        -0.24833                             4


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -495.94          180.16        -0.86394        -0.38125
v  Velocity[Y]                 -418.64          1006.8          1.6175         0.92771
v  Velocity[Z]                 -259.22          311.66        -0.39036        -0.11722
v  ǁVelocityǁ                  0.01656          1026.9          6.6806          4.6519
v  Pressure                -1.0755e+05      1.9023e+05           54838           37684
v  k                        1.5182e-05          3678.2          44.841          26.096
v  epsilon                  0.00055327      1.6907e+08      6.6746e+05      4.0905e+05
v  turbulent_viscosity      3.0858e-07          10.014         0.77728         0.42726
v  CourantNb                   0.96595       1.634e+06          2145.8          1182.3
v  FourierNb                    7.4041           19616          1361.8          551.13
v  total_pressure           3.9245e+05      6.9023e+05      5.5484e+05      5.3768e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          14.646      1.6353e+06          3507.5          1733.4


 TIME FOR THE TIME STEP              107:        0.80174E+01

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


 INSTANT    0.108000000E+02   TIME STEP NUMBER             108
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.379633368E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273306699E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74760E+04 0.41145E+03
   Friction velocity        uet   :  0.32186E-02 0.91173E+02
   Friction velocity        uk    :  0.46942E-01 0.32789E+02
   Dimensionless distance   yplus :  0.63765E+00 0.36960E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        460
   Nb of faces within the viscous sub-layer     :        377
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.96514E+03    4540   0.10005E+01   0.21550E+02 
c  VelocityY    0.96514E+03    4540   0.10005E+01   0.00000E+00 
c  VelocityZ    0.96514E+03    4540   0.10005E+01   0.00000E+00 
c  Pressure     0.76603E+01     571   0.75475E-02   0.12818E+00 
c  k            0.33487E+05     273   0.28196E-03   0.60397E+04 
c  epsilon      0.87171E+09     135   0.36297E-03   0.58550E+13 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -1.4364                             5


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -555.18          188.72        -0.90471        -0.41541
v  Velocity[Y]                  -469.3          1059.7          1.7365           1.009
v  Velocity[Z]                 -275.94          337.17        -0.48096        -0.13793
v  ǁVelocityǁ                 0.033908          1079.2          7.4371          5.0914
v  Pressure                -1.1562e+05      2.0181e+05           57393           39364
v  k                        5.6428e-05            4211          50.369          29.905
v  epsilon                  0.00013918      1.9282e+08      7.8596e+05       4.903e+05
v  turbulent_viscosity      4.3835e-06          10.752         0.65436          0.3594
v  CourantNb                  0.019291      1.7691e+06          2197.7          1226.1
v  FourierNb                      6.35           21851          1149.1          469.37
v  total_pressure           3.8438e+05      7.0181e+05      5.5739e+05      5.3936e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.391      1.7703e+06          3346.8          1695.5


 TIME FOR THE TIME STEP              108:        0.72343E+01

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


 INSTANT    0.109000000E+02   TIME STEP NUMBER             109
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.137452556E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273304085E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76457E+04 0.45917E+03
   Friction velocity        uet   :  0.11650E-02 0.96163E+02
   Friction velocity        uk    :  0.49583E-01 0.34527E+02
   Dimensionless distance   yplus :  0.58500E+00 0.38632E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        407
   Nb of faces within the viscous sub-layer     :        335
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.55527E+03    5028   0.10022E+01   0.34702E+02 
c  VelocityY    0.55527E+03    5028   0.10022E+01   0.00000E+00 
c  VelocityZ    0.55527E+03    5028   0.10022E+01   0.00000E+00 
c  Pressure     0.81003E+01     592   0.76882E-02   0.12729E+00 
c  k            0.40024E+05     350   0.30401E-03   0.10777E+05 
c  epsilon      0.11098E+10     148   0.39620E-03   0.11438E+14 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -561.69          203.86         -1.0859        -0.42385
v  Velocity[Y]                 -504.16          1213.7          1.9739          1.0177
v  Velocity[Z]                 -294.28          372.13        -0.39336        -0.10804
v  ǁVelocityǁ                 0.025004          1234.4          7.8837          5.3212
v  Pressure                -1.2376e+05      2.1455e+05           60913           41776
v  k                        0.00010166          4769.8          57.791          34.294
v  epsilon                     0.12888      2.3407e+08      9.6652e+05      5.9871e+05
v  turbulent_viscosity      4.7631e-06          11.477         0.75559         0.41135
v  CourantNb                    2.0366      1.9757e+06          2416.6          1327.1
v  FourierNb                    7.0218           22753          1327.6          535.08
v  total_pressure           3.7624e+05      7.1455e+05      5.6091e+05      5.4178e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          19.596      1.9769e+06          3744.2          1862.2


 TIME FOR THE TIME STEP              109:        0.79008E+01

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


 INSTANT    0.110000000E+02   TIME STEP NUMBER             110
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.449505377E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273308778E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96766E+04 0.46658E+03
   Friction velocity        uet   :  0.40610E-02 0.10862E+03
   Friction velocity        uk    :  0.56002E-01 0.36594E+02
   Dimensionless distance   yplus :  0.64526E+00 0.42400E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        614
   Nb of faces within the viscous sub-layer     :        330
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.12444E+04    4711   0.10002E+01   0.49604E+02 
c  VelocityY    0.12444E+04    4711   0.10002E+01   0.00000E+00 
c  VelocityZ    0.12444E+04    4711   0.10002E+01   0.00000E+00 
c  Pressure     0.87317E+01     568   0.75779E-02   0.12868E+00 
c  k            0.48412E+05     362   0.27968E-03   0.11130E+05 
c  epsilon      0.14267E+10     138   0.36986E-03   0.14603E+14 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -51.015                             8


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -635.76          215.96         -0.9115        -0.46339
v  Velocity[Y]                 -557.61          1269.7          1.9224           1.099
v  Velocity[Z]                 -310.32          412.04        -0.38119        -0.15326
v  ǁVelocityǁ                 0.036817          1296.9          8.4828          5.9379
v  Pressure                -1.3296e+05      2.2777e+05           63880           43723
v  k                        3.0499e-06          5495.9          66.505          39.109
v  epsilon                    0.019515      2.8425e+08      1.1728e+06      7.2507e+05
v  turbulent_viscosity      4.1433e-07          11.969         0.81311         0.46029
v  CourantNb                   0.72131       2.126e+06          2573.9          1409.4
v  FourierNb                    6.2977           24718            1406          579.85
v  total_pressure           3.6704e+05      7.2777e+05      5.6388e+05      5.4372e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          13.231      2.1272e+06            3980          1989.2


 TIME FOR THE TIME STEP              110:        0.74840E+01

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


 INSTANT    0.111000000E+02   TIME STEP NUMBER             111
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.165440841E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273303050E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98233E+04 0.52730E+03
   Friction velocity        uet   :  0.10475E-01 0.11386E+03
   Friction velocity        uk    :  0.56552E-01 0.39592E+02
   Dimensionless distance   yplus :  0.41995E+00 0.45117E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        745
   Nb of faces within the viscous sub-layer     :        253
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.74736E+03    5106   0.10022E+01   0.46037E+02 
c  VelocityY    0.74736E+03    5106   0.10022E+01   0.00000E+00 
c  VelocityZ    0.74736E+03    5106   0.10022E+01   0.00000E+00 
c  Pressure     0.92445E+01     589   0.76585E-02   0.12786E+00 
c  k            0.58474E+05     278   0.30038E-03   0.13561E+05 
c  epsilon      0.18390E+10     136   0.40104E-03   0.22879E+14 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -656.5          234.91         -1.0843        -0.51379
v  Velocity[Y]                 -602.87            1455           2.261          1.1184
v  Velocity[Z]                 -328.79          442.63        -0.24591        -0.11956
v  ǁVelocityǁ                 0.022025            1481          8.5511          5.8176
v  Pressure                -1.4252e+05      2.4217e+05           67473           46133
v  k                        4.3631e-05            6095           72.92          42.913
v  epsilon                   0.0014375      3.6343e+08      1.4078e+06       8.653e+05
v  turbulent_viscosity       2.085e-10          12.916         0.86854         0.48016
v  CourantNb                    1.4904       2.369e+06          2750.1            1522
v  FourierNb                    6.3089           25374          1513.8          612.55
v  total_pressure           3.5748e+05      7.4217e+05      5.6747e+05      5.4613e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          19.839      2.3703e+06          4263.9          2134.6


 TIME FOR THE TIME STEP              111:        0.83315E+01

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


 INSTANT    0.112000000E+02   TIME STEP NUMBER             112
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.958089768E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273308102E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11729E+05 0.54663E+03
   Friction velocity        uet   :  0.55287E-02 0.12999E+03
   Friction velocity        uk    :  0.80823E-01 0.42375E+02
   Dimensionless distance   yplus :  0.59330E+00 0.47010E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        661
   Nb of faces within the viscous sub-layer     :        207
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.16145E+04    4720   0.10001E+01   0.51928E+02 
c  VelocityY    0.16145E+04    4720   0.10001E+01   0.00000E+00 
c  VelocityZ    0.16145E+04    4720   0.10001E+01   0.00000E+00 
c  Pressure     0.99993E+01     572   0.75377E-02   0.12973E+00 
c  k            0.70760E+05     268   0.29258E-03   0.19572E+05 
c  epsilon      0.23762E+10     137   0.40961E-03   0.31304E+14 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -723.48          241.04         -1.0882        -0.55128
v  Velocity[Y]                 -673.37          1527.7          2.3088          1.1656
v  Velocity[Z]                 -344.53          487.21         -0.4498        -0.19317
v  ǁVelocityǁ                 0.024582          1554.8          9.4641          6.5189
v  Pressure                -1.5271e+05      2.5742e+05           70985           48483
v  k                        7.3322e-05          7134.8          84.192          49.883
v  epsilon                   0.0053812      4.1986e+08      1.7016e+06      1.0549e+06
v  turbulent_viscosity      2.7732e-06          14.155         0.75647         0.43508
v  CourantNb                    4.8743      2.5679e+06          2839.1          1551.1
v  FourierNb                    6.7082           28425          1300.2           543.9
v  total_pressure           3.4729e+05      7.5742e+05      5.7099e+05      5.4848e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          19.263      2.5691e+06          4139.3            2095


 TIME FOR THE TIME STEP              112:        0.74343E+01

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


 INSTANT    0.113000000E+02   TIME STEP NUMBER             113
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.131406435E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273315043E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12479E+05 0.60164E+03
   Friction velocity        uet   :  0.90154E-02 0.13580E+03
   Friction velocity        uk    :  0.61612E-01 0.44843E+02
   Dimensionless distance   yplus :  0.41769E+00 0.50371E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        641
   Nb of faces within the viscous sub-layer     :        341
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10063E+04    5002   0.10023E+01   0.75509E+02 
c  VelocityY    0.10063E+04    5002   0.10023E+01   0.00000E+00 
c  VelocityZ    0.10063E+04    5002   0.10023E+01   0.00000E+00 
c  Pressure     0.10616E+02     594   0.76384E-02   0.12922E+00 
c  k            0.85630E+05     298   0.36614E-03   0.29274E+05 
c  epsilon      0.30561E+10     144   0.43057E-03   0.54876E+14 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -745.39          263.64         -1.1874        -0.58981
v  Velocity[Y]                 -726.04          1743.8          2.4311          1.1963
v  Velocity[Z]                 -375.68          545.69        -0.48894        -0.13648
v  ǁVelocityǁ                 0.055695          1779.6          9.9749          6.8399
v  Pressure                -1.6317e+05      2.7405e+05           75319           51471
v  k                         0.0003601          8161.7          95.927          56.653
v  epsilon                    0.046998      5.1202e+08      2.0832e+06      1.2843e+06
v  turbulent_viscosity      2.1275e-06           15.08         0.89252         0.50757
v  CourantNb                   0.70338      2.8558e+06          3103.3            1694
v  FourierNb                    6.8065           29955          1537.2          633.77
v  total_pressure           3.3683e+05      7.7405e+05      5.7532e+05      5.5147e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          15.088       2.857e+06          4640.5          2327.8


 TIME FOR THE TIME STEP              113:        0.78615E+01

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


 INSTANT    0.114000000E+02   TIME STEP NUMBER             114
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.156608444E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273318625E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15715E+05 0.62305E+03
   Friction velocity        uet   :  0.60643E-02 0.15301E+03
   Friction velocity        uk    :  0.64707E-01 0.47790E+02
   Dimensionless distance   yplus :  0.44704E+00 0.55945E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        808
   Nb of faces within the viscous sub-layer     :        161
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.20792E+04    4855   0.99995E+00   0.77568E+02 
c  VelocityY    0.20792E+04    4855   0.99995E+00   0.00000E+00 
c  VelocityZ    0.20792E+04    4855   0.99995E+00   0.00000E+00 
c  Pressure     0.11439E+02     588   0.74787E-02   0.13052E+00 
c  k            0.10539E+06     265   0.30416E-03   0.31948E+05 
c  epsilon      0.39958E+10     138   0.38176E-03   0.69979E+14 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon          -12.41                             3


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -818.21          276.77          -1.264        -0.64405
v  Velocity[Y]                 -810.56          1842.4          2.6052          1.2564
v  Velocity[Z]                 -391.14           584.9        -0.59434        -0.19564
v  ǁVelocityǁ                 0.050798          1876.4          10.263          7.0499
v  Pressure                -1.7465e+05      2.9148e+05           79374           54239
v  k                        8.0444e-05          9218.2           108.2          64.392
v  epsilon                    0.010246      6.2976e+08      2.5151e+06      1.5603e+06
v  turbulent_viscosity      1.5505e-05          16.001         0.84923         0.50261
v  CourantNb                 0.0091729      3.0669e+06          3278.8          1793.6
v  FourierNb                    6.2049           31383          1433.6          612.09
v  total_pressure           3.2535e+05      7.9148e+05      5.7937e+05      5.5424e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.1315      3.0682e+06          4712.4          2405.7


 TIME FOR THE TIME STEP              114:        0.77485E+01

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


 INSTANT    0.115000000E+02   TIME STEP NUMBER             115
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.137431918E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273310735E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15717E+05 0.68383E+03
   Friction velocity        uet   :  0.22286E-02 0.16263E+03
   Friction velocity        uk    :  0.88145E-01 0.51721E+02
   Dimensionless distance   yplus :  0.55650E+00 0.57296E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        747
   Nb of faces within the viscous sub-layer     :        142
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.14321E+04    4996   0.10046E+01   0.82909E+02 
c  VelocityY    0.14321E+04    4996   0.10046E+01   0.00000E+00 
c  VelocityZ    0.14321E+04    4996   0.10046E+01   0.00000E+00 
c  Pressure     0.12128E+02     591   0.76332E-02   0.12979E+00 
c  k            0.12753E+06     286   0.30563E-03   0.46649E+05 
c  epsilon      0.51810E+10     141   0.42554E-03   0.12333E+15 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -829.32          302.24         -1.6281        -0.61184
v  Velocity[Y]                 -874.82          2093.5          2.7362          1.3609
v  Velocity[Z]                 -421.98           639.9         -0.4626        -0.16621
v  ǁVelocityǁ                 0.082301            2128          11.326          7.5422
v  Pressure                -1.8698e+05      3.0985e+05           84224           57529
v  k                        6.9267e-05           10636          126.74          73.404
v  epsilon                     0.13676      7.9356e+08      3.1219e+06      1.9001e+06
v  turbulent_viscosity      5.5937e-06           16.99         0.92661         0.52627
v  CourantNb                    5.2014       3.432e+06          3428.8          1860.1
v  FourierNb                    6.5027           33547          1585.1          657.26
v  total_pressure           3.1302e+05      8.0985e+05      5.8422e+05      5.5753e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          17.985      3.4332e+06          5013.9          2517.4


 TIME FOR THE TIME STEP              115:        0.78102E+01

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


 INSTANT    0.116000000E+02   TIME STEP NUMBER             116
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.134501066E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273317738E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19959E+05 0.69643E+03
   Friction velocity        uet   :  0.25154E-02 0.18211E+03
   Friction velocity        uk    :  0.53304E-01 0.55207E+02
   Dimensionless distance   yplus :  0.71459E+00 0.61304E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        999
   Nb of faces within the viscous sub-layer     :        102
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.26543E+04    4974   0.99988E+00   0.85793E+02 
c  VelocityY    0.26543E+04    4974   0.99988E+00   0.00000E+00 
c  VelocityZ    0.26543E+04    4974   0.99988E+00   0.00000E+00 
c  Pressure     0.13098E+02     575   0.74490E-02   0.13133E+00 
c  k            0.15579E+06     243   0.33435E-03   0.48209E+05 
c  epsilon      0.67451E+10     136   0.43394E-03   0.14298E+15 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -926.61          312.36         -1.5414         -0.6819
v  Velocity[Y]                 -975.49          2201.2          2.7675            1.37
v  Velocity[Z]                 -447.72           708.9        -0.68175        -0.22471
v  ǁVelocityǁ                 0.033454          2247.4          12.136          8.0477
v  Pressure                -2.0002e+05      3.2949e+05           88793           60591
v  k                        6.7155e-05           12046          138.18          83.248
v  epsilon                    0.061785      9.2941e+08      3.6633e+06      2.2872e+06
v  turbulent_viscosity      1.5385e-07          18.516          1.0378         0.58848
v  CourantNb                    1.0639      3.7041e+06          3767.2          2013.3
v  FourierNb                    6.7037           37126            1770          732.64
v  total_pressure           2.9998e+05      8.2949e+05      5.8879e+05      5.6059e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           16.43      3.7054e+06          5537.2          2745.9


 TIME FOR THE TIME STEP              116:        0.77547E+01

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


 INSTANT    0.117000000E+02   TIME STEP NUMBER             117
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.192636587E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273327287E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20444E+05 0.77616E+03
   Friction velocity        uet   :  0.14876E-01 0.19160E+03
   Friction velocity        uk    :  0.40897E-01 0.58702E+02
   Dimensionless distance   yplus :  0.52037E+00 0.65748E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        692
   Nb of faces within the viscous sub-layer     :        104
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.19140E+04    5312   0.10042E+01   0.12056E+03 
c  VelocityY    0.19140E+04    5312   0.10042E+01   0.00000E+00 
c  VelocityZ    0.19140E+04    5312   0.10042E+01   0.00000E+00 
c  Pressure     0.13908E+02     590   0.76363E-02   0.13073E+00 
c  k            0.18698E+06     297   0.31676E-03   0.80097E+05 
c  epsilon      0.86565E+10     139   0.37098E-03   0.22754E+15 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -947.5          338.03         -1.7612        -0.68271
v  Velocity[Y]                 -1040.2          2517.3           2.927          1.4505
v  Velocity[Z]                 -465.43          768.26         -0.2908        -0.19995
v  ǁVelocityǁ                 0.053399          2562.9          12.917          8.7509
v  Pressure                -2.1435e+05      3.4997e+05           94110           64199
v  k                        0.00057749           13570           160.4          94.016
v  epsilon                    0.013052      1.1359e+09      4.4988e+06       2.753e+06
v  turbulent_viscosity      8.5869e-07          19.622          1.1404         0.65663
v  CourantNb                   0.48136      4.1287e+06          4039.7          2143.6
v  FourierNb                    6.6256           38820          1933.6           804.8
v  total_pressure           2.8565e+05      8.4997e+05      5.9411e+05       5.642e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          16.912      4.1299e+06          5973.3          2948.4


 TIME FOR THE TIME STEP              117:        0.81925E+01

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


 INSTANT    0.118000000E+02   TIME STEP NUMBER             118
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.135580895E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273319390E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23957E+05 0.79878E+03
   Friction velocity        uet   :  0.24190E-02 0.21881E+03
   Friction velocity        uk    :  0.90033E-01 0.62299E+02
   Dimensionless distance   yplus :  0.64208E+00 0.69848E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        846
   Nb of faces within the viscous sub-layer     :         83
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.34562E+04    5113   0.10005E+01   0.16139E+03 
c  VelocityY    0.34562E+04    5113   0.10005E+01   0.00000E+00 
c  VelocityZ    0.34562E+04    5113   0.10005E+01   0.00000E+00 
c  Pressure     0.15053E+02     589   0.74774E-02   0.13249E+00 
c  k            0.22719E+06     261   0.30822E-03   0.83100E+05 
c  epsilon      0.11218E+11     136   0.38080E-03   0.28931E+15 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0082835                             1
a  epsilon         -399.55                            59


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1066.7          361.49         -1.4787        -0.78425
v  Velocity[Y]                 -1167.2          2644.1          2.9603          1.4999
v  Velocity[Z]                 -511.99          856.04        -0.60071        -0.23689
v  ǁVelocityǁ                 0.062806          2693.9          13.943          9.4783
v  Pressure                -2.2916e+05      3.7234e+05           99445           67784
v  k                         0.0018031           15474          176.22          105.94
v  epsilon                    0.021346      1.3539e+09      5.3189e+06      3.3123e+06
v  turbulent_viscosity      3.5278e-05          20.749          1.1617         0.65138
v  CourantNb                    1.1056      4.4432e+06          4280.7          2298.4
v  FourierNb                     6.708           41041          1982.3          813.75
v  total_pressure           2.7084e+05      8.7234e+05      5.9944e+05      5.6778e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.276      4.4444e+06            6263          3112.1


 TIME FOR THE TIME STEP              118:        0.79552E+01

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


 INSTANT    0.119000000E+02   TIME STEP NUMBER             119
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.205167751E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273320840E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24237E+05 0.89534E+03
   Friction velocity        uet   :  0.14646E-01 0.23054E+03
   Friction velocity        uk    :  0.70762E-01 0.66641E+02
   Dimensionless distance   yplus :  0.67496E+00 0.74853E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        668
   Nb of faces within the viscous sub-layer     :         67
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.27094E+04    5527   0.10051E+01   0.18568E+03 
c  VelocityY    0.27094E+04    5527   0.10051E+01   0.00000E+00 
c  VelocityZ    0.27094E+04    5527   0.10051E+01   0.00000E+00 
c  Pressure     0.16027E+02     588   0.75990E-02   0.13217E+00 
c  k            0.27161E+06     314   0.29604E-03   0.13786E+06 
c  epsilon      0.14345E+11     139   0.46236E-03   0.54417E+15 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1066.5          389.15         -1.9807        -0.80553
v  Velocity[Y]                 -1261.2          3012.5          3.9378          1.6169
v  Velocity[Z]                 -529.42          942.68        -0.67798        -0.22431
v  ǁVelocityǁ                 0.091492            3074          15.508          10.441
v  Pressure                 -2.456e+05      3.9529e+05      1.0492e+05           71495
v  k                        0.00058678           17340          209.07          121.62
v  epsilon                    0.019474      1.6826e+09      6.6047e+06      4.0168e+06
v  turbulent_viscosity      3.6554e-06          237.59          1.2385         0.70797
v  CourantNb                    3.8441      4.9376e+06          4623.7          2468.6
v  FourierNb                     6.384      2.2764e+05          2098.8          869.66
v  total_pressure            2.544e+05      8.9529e+05      6.0492e+05       5.715e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          21.446      4.9388e+06          6722.6          3338.3


 TIME FOR THE TIME STEP              119:        0.84839E+01

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


 INSTANT    0.120000000E+02   TIME STEP NUMBER             120
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.989104066E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273320198E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29111E+05 0.90024E+03
   Friction velocity        uet   :  0.12190E-01 0.26135E+03
   Friction velocity        uk    :  0.65743E-01 0.70889E+02
   Dimensionless distance   yplus :  0.25363E+00 0.78110E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        749
   Nb of faces within the viscous sub-layer     :         40
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.44716E+04    5318   0.99953E+00   0.20132E+03 
c  VelocityY    0.44716E+04    5318   0.99953E+00   0.00000E+00 
c  VelocityZ    0.44716E+04    5318   0.99953E+00   0.00000E+00 
c  Pressure     0.17299E+02     574   0.74193E-02   0.13347E+00 
c  k            0.32705E+06     257   0.27435E-03   0.11601E+06 
c  epsilon      0.18456E+11     134   0.36655E-03   0.55985E+15 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1231.4          407.59          -1.652        -0.91342
v  Velocity[Y]                 -1393.6          3186.1          3.0928          1.6582
v  Velocity[Z]                 -569.59            1005        -0.53009        -0.32713
v  ǁVelocityǁ                 0.076003          3243.1          15.291          10.444
v  Pressure                -2.6282e+05      4.2071e+05      1.1076e+05           75358
v  k                         0.0016725           19938          230.43          136.37
v  epsilon                    0.021803      1.9262e+09      7.7555e+06      4.7972e+06
v  turbulent_viscosity      8.0294e-05          23.245          1.4182          0.8101
v  CourantNb                   0.71107      5.3393e+06          5068.4          2696.7
v  FourierNb                    6.2325           45769          2401.9          990.29
v  total_pressure           2.3718e+05      9.2071e+05      6.1076e+05      5.7536e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          18.709      5.3405e+06          7470.3            3687


 TIME FOR THE TIME STEP              120:        0.82441E+01

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


 INSTANT    0.121000000E+02   TIME STEP NUMBER             121
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.708026450E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273341151E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28402E+05 0.10383E+04
   Friction velocity        uet   :  0.49928E-02 0.27913E+03
   Friction velocity        uk    :  0.75730E-01 0.75019E+02
   Dimensionless distance   yplus :  0.69001E+00 0.83333E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        646
   Nb of faces within the viscous sub-layer     :         33
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.36513E+04    5538   0.10060E+01   0.26145E+03 
c  VelocityY    0.36513E+04    5538   0.10060E+01   0.00000E+00 
c  VelocityZ    0.36513E+04    5538   0.10060E+01   0.00000E+00 
c  Pressure     0.18395E+02     590   0.75188E-02   0.13300E+00 
c  k            0.38959E+06     277   0.32424E-03   0.20199E+06 
c  epsilon      0.23460E+11     136   0.39147E-03   0.96015E+15 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                   -1219          438.41         -2.2618         -0.9404
v  Velocity[Y]                 -1512.9          3625.4          3.5962          1.7613
v  Velocity[Z]                 -589.41          1113.4        -0.44696        -0.22659
v  ǁVelocityǁ                  0.12591          3686.6          17.103          11.423
v  Pressure                -2.8067e+05      4.4774e+05      1.1759e+05           80018
v  k                        0.00075021           22047          253.25          151.63
v  epsilon                     0.14503      2.3642e+09      9.2536e+06      5.7131e+06
v  turbulent_viscosity       7.693e-05          25.098          1.4407         0.80229
v  CourantNb                   0.51363      5.9695e+06          5165.3          2748.8
v  FourierNb                    6.7581           49706          2456.4          998.83
v  total_pressure           2.1933e+05      9.4774e+05      6.1759e+05      5.8002e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.889      5.9707e+06          7621.7          3747.6


 TIME FOR THE TIME STEP              121:        0.85337E+01

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


 INSTANT    0.122000000E+02   TIME STEP NUMBER             122
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.282463822E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273333965E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34437E+05 0.10314E+04
   Friction velocity        uet   :  0.16098E-01 0.31537E+03
   Friction velocity        uk    :  0.99579E-01 0.79662E+02
   Dimensionless distance   yplus :  0.81988E+00 0.88502E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        677
   Nb of faces within the viscous sub-layer     :         58
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.58195E+04    5423   0.99990E+00   0.34227E+03 
c  VelocityY    0.58195E+04    5423   0.99990E+00   0.00000E+00 
c  VelocityZ    0.58195E+04    5423   0.99990E+00   0.00000E+00 
c  Pressure     0.19931E+02     591   0.74630E-02   0.13478E+00 
c  k            0.46928E+06     272   0.27615E-03   0.23533E+06 
c  epsilon      0.30053E+11     136   0.36422E-03   0.12786E+16 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1382.9          470.68         -1.8838         -1.0118
v  Velocity[Y]                   -1678          3828.9          3.6587          1.7584
v  Velocity[Z]                 -644.79            1239        -0.59556        -0.36129
v  ǁVelocityǁ                 0.095037          3910.6          17.847          12.224
v  Pressure                -2.9948e+05      4.7706e+05      1.2513e+05           85197
v  k                        0.00021226           25214          294.53          175.13
v  epsilon                   0.0079839      2.8827e+09      1.1186e+07      6.9118e+06
v  turbulent_viscosity      7.2303e-06          25.883          1.4061         0.82668
v  CourantNb                     2.102      6.4272e+06          5680.4          3003.1
v  FourierNb                    6.1194           50987            2353          991.02
v  total_pressure           2.0052e+05      9.7706e+05      6.2513e+05       5.852e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          14.262      6.4285e+06          8033.4          3994.1


 TIME FOR THE TIME STEP              122:        0.83270E+01

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


 INSTANT    0.123000000E+02   TIME STEP NUMBER             123
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.135712637E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273336009E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32077E+05 0.11685E+04
   Friction velocity        uet   :  0.21638E-01 0.33880E+03
   Friction velocity        uk    :  0.43528E-01 0.85617E+02
   Dimensionless distance   yplus :  0.66350E+00 0.93872E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        787
   Nb of faces within the viscous sub-layer     :         97
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.50359E+04    5964   0.10047E+01   0.29287E+03 
c  VelocityY    0.50359E+04    5964   0.10047E+01   0.00000E+00 
c  VelocityZ    0.50359E+04    5964   0.10047E+01   0.00000E+00 
c  Pressure     0.21175E+02     592   0.75229E-02   0.13403E+00 
c  k            0.56055E+06     228   0.28458E-03   0.26216E+06 
c  epsilon      0.38204E+11     137   0.40090E-03   0.20287E+16 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1379.3          509.36         -2.5614         -1.0023
v  Velocity[Y]                 -1812.3          4357.5          4.0893          1.8998
v  Velocity[Z]                 -671.22          1323.3         -0.6122        -0.27365
v  ǁVelocityǁ                   0.1168          4434.9          17.952          12.102
v  Pressure                -3.1963e+05       5.077e+05      1.3356e+05           90961
v  k                        0.00066248           28510          323.22          189.69
v  epsilon                     0.11169      3.5311e+09        1.34e+07      8.1886e+06
v  turbulent_viscosity       6.526e-05          27.881          1.6945         0.94797
v  CourantNb                   0.48917      7.1455e+06          5969.2          3172.9
v  FourierNb                    6.8887           54036          2882.4          1169.8
v  total_pressure           1.8037e+05      1.0077e+06      6.3356e+05      5.9096e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           14.12      7.1468e+06          8851.6          4342.7


 TIME FOR THE TIME STEP              123:        0.91282E+01

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


 INSTANT    0.124000000E+02   TIME STEP NUMBER             124
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.312888334E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273350699E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35424E+05 0.11697E+04
   Friction velocity        uet   :  0.67900E-02 0.38865E+03
   Friction velocity        uk    :  0.80526E-01 0.90684E+02
   Dimensionless distance   yplus :  0.96694E+00 0.10058E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        694
   Nb of faces within the viscous sub-layer     :         34
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.75123E+04    6027   0.99893E+00   0.26122E+03 
c  VelocityY    0.75123E+04    6027   0.99893E+00   0.00000E+00 
c  VelocityZ    0.75123E+04    6027   0.99893E+00   0.00000E+00 
c  Pressure     0.22942E+02     569   0.73351E-02   0.13571E+00 
c  k            0.67892E+06     271   0.25096E-03   0.28914E+06 
c  epsilon      0.49060E+11     135   0.34267E-03   0.23716E+16 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1552.5          524.71         -2.2724         -1.2014
v  Velocity[Y]                 -2013.4          4604.8          3.7323          2.0566
v  Velocity[Z]                  -722.5          1457.6         -1.0678        -0.40602
v  ǁVelocityǁ                  0.13526            4685          19.483          13.083
v  Pressure                -3.4243e+05      5.3943e+05      1.4039e+05           95411
v  k                        0.00046528           32654          372.55          220.13
v  epsilon                     0.99461      4.0389e+09      1.6021e+07      9.8664e+06
v  turbulent_viscosity      2.7572e-05          29.525          1.5252         0.87067
v  CourantNb                    2.6552      7.7451e+06          6172.6          3247.2
v  FourierNb                    7.0996           58351          2564.4          1064.2
v  total_pressure           1.5757e+05      1.0394e+06      6.4039e+05      5.9541e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          13.338      7.7464e+06            8737          4311.3


 TIME FOR THE TIME STEP              124:        0.91569E+01

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


 INSTANT    0.125000000E+02   TIME STEP NUMBER             125
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.351235370E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273340796E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34929E+05 0.13151E+04
   Friction velocity        uet   :  0.16062E-01 0.41420E+03
   Friction velocity        uk    :  0.98693E-01 0.95971E+02
   Dimensionless distance   yplus :  0.84110E+00 0.10627E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        790
   Nb of faces within the viscous sub-layer     :         29
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.72458E+04    5865   0.10055E+01   0.67551E+03 
c  VelocityY    0.72458E+04    5865   0.10055E+01   0.00000E+00 
c  VelocityZ    0.72458E+04    5865   0.10055E+01   0.00000E+00 
c  Pressure     0.24571E+02     590   0.75382E-02   0.13600E+00 
c  k            0.80872E+06     267   0.27818E-03   0.44095E+06 
c  epsilon      0.62160E+11     137   0.35766E-03   0.40111E+16 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1619.4          557.32         -2.8823         -1.1562
v  Velocity[Y]                 -2187.3          5226.5          4.5063          2.1692
v  Velocity[Z]                 -761.96          1646.2         -1.0698        -0.25404
v  ǁVelocityǁ                 0.076597          5336.2          22.287          15.591
v  Pressure                -3.6607e+05      5.7409e+05      1.4946e+05      1.0154e+05
v  k                         0.0012226           36776          410.87          242.45
v  epsilon                    0.067818      4.8999e+09      1.9297e+07      1.1787e+07
v  turbulent_viscosity       1.721e-06          31.824           2.023          1.1122
v  CourantNb                    3.9167      8.6143e+06          6690.4          3491.4
v  FourierNb                    6.8205           62683          3452.5          1384.6
v  total_pressure           1.3393e+05      1.0741e+06      6.4946e+05      6.0154e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          22.966      8.6156e+06           10143            4876


 TIME FOR THE TIME STEP              125:        0.89934E+01

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


 INSTANT    0.126000000E+02   TIME STEP NUMBER             126
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.317151708E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273347205E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41103E+05 0.13787E+04
   Friction velocity        uet   :  0.19131E-01 0.46893E+03
   Friction velocity        uk    :  0.58303E-01 0.10202E+03
   Dimensionless distance   yplus :  0.60309E+00 0.11617E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        834
   Nb of faces within the viscous sub-layer     :         23
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.97375E+04    5928   0.99982E+00   0.82819E+03 
c  VelocityY    0.97375E+04    5928   0.99982E+00   0.00000E+00 
c  VelocityZ    0.97375E+04    5928   0.99982E+00   0.00000E+00 
c  Pressure     0.26551E+02     571   0.72987E-02   0.13721E+00 
c  k            0.98361E+06     226   0.31087E-03   0.56274E+06 
c  epsilon      0.80160E+11     135   0.40390E-03   0.56307E+16 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -1476.4                            19


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1762.4          601.05         -2.2245         -1.4077
v  Velocity[Y]                 -2413.4          5554.9          4.6309           2.235
v  Velocity[Z]                  -808.6            1740         -1.1066        -0.43373
v  ǁVelocityǁ                  0.21252          5653.6          22.074          14.968
v  Pressure                -3.9173e+05      6.1043e+05      1.5734e+05      1.0675e+05
v  k                        0.00034423           41414          459.01          276.67
v  epsilon                    0.011427      5.9433e+09      2.2844e+07        1.42e+07
v  turbulent_viscosity      8.1108e-05          33.507          1.5339          0.9167
v  CourantNb                    1.3996      9.2359e+06            7391            3957
v  FourierNb                    6.9335           65919          2519.2          1085.5
v  total_pressure           1.0827e+05      1.1104e+06      6.5734e+05      6.0675e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          15.225      9.2372e+06          9910.2          5042.4


 TIME FOR THE TIME STEP              126:        0.90163E+01

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


 INSTANT    0.127000000E+02   TIME STEP NUMBER             127
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.995234385E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273363201E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37750E+05 0.14982E+04
   Friction velocity        uet   :  0.33235E-02 0.50883E+03
   Friction velocity        uk    :  0.82508E-01 0.10938E+03
   Dimensionless distance   yplus :  0.63225E+00 0.12050E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1313
   Nb of faces within the viscous sub-layer     :         15
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10207E+05    5746   0.10077E+01   0.62542E+03 
c  VelocityY    0.10207E+05    5746   0.10077E+01   0.00000E+00 
c  VelocityZ    0.10207E+05    5746   0.10077E+01   0.00000E+00 
c  Pressure     0.28212E+02     588   0.74618E-02   0.13639E+00 
c  k            0.11832E+07     241   0.32028E-03   0.11102E+07 
c  epsilon      0.10290E+12     139   0.40269E-03   0.11099E+17 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1797.4          655.45         -3.4186         -1.3259
v  Velocity[Y]                   -2621          6284.5          4.8298          2.4235
v  Velocity[Z]                 -856.29          1912.8        -0.40434        -0.32677
v  ǁVelocityǁ                  0.10309          6386.9          25.456           17.33
v  Pressure                -4.1873e+05      6.5411e+05      1.6768e+05      1.1366e+05
v  k                        0.00091189           47277          546.69          317.82
v  epsilon                     0.39218      7.5819e+09       2.875e+07      1.7417e+07
v  turbulent_viscosity      1.9096e-08          35.657           1.741          1.0364
v  CourantNb                    4.9376      1.0349e+07          7618.1          3970.5
v  FourierNb                    6.6899           69560          2864.6          1225.9
v  total_pressure                81267      1.1541e+06      6.6768e+05      6.1366e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          22.207       1.035e+07           10483          5196.4


 TIME FOR THE TIME STEP              127:        0.88617E+01

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


 INSTANT    0.128000000E+02   TIME STEP NUMBER             128
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.540743398E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273348147E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42645E+05 0.15346E+04
   Friction velocity        uet   :  0.78485E-02 0.57769E+03
   Friction velocity        uk    :  0.12301E+00 0.11730E+03
   Dimensionless distance   yplus :  0.97603E+00 0.12924E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1268
   Nb of faces within the viscous sub-layer     :         16
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.12752E+05    6130   0.99939E+00   0.85214E+03 
c  VelocityY    0.12752E+05    6130   0.99939E+00   0.00000E+00 
c  VelocityZ    0.12752E+05    6130   0.99939E+00   0.00000E+00 
c  Pressure     0.30672E+02     568   0.72833E-02   0.13840E+00 
c  k            0.14473E+07     245   0.30006E-03   0.86358E+06 
c  epsilon      0.13373E+12     137   0.37470E-03   0.11116E+17 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                   -2043          684.16         -2.9268         -1.6094
v  Velocity[Y]                 -2914.4          6642.8          5.5774          2.5259
v  Velocity[Z]                 -916.03          2113.9         -1.0514        -0.48951
v  ǁVelocityǁ                 0.084318          6778.5          26.685           18.11
v  Pressure                -4.4776e+05      7.1093e+05      1.7612e+05      1.1916e+05
v  k                         0.0028997           53862           603.3          360.63
v  epsilon                    0.022254      8.5081e+09       3.379e+07      2.0878e+07
v  turbulent_viscosity       3.304e-06          38.597          1.8997          1.1138
v  CourantNb                    2.9912      1.1161e+07          8536.4          4477.7
v  FourierNb                    6.9656           76471          3149.2            1328
v  total_pressure                52244      1.2109e+06      6.7612e+05      6.1916e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          13.819      1.1162e+07           11686          5805.7


 TIME FOR THE TIME STEP              128:        0.93018E+01

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


 INSTANT    0.129000000E+02   TIME STEP NUMBER             129
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.461609980E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273356704E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40194E+05 0.17368E+04
   Friction velocity        uet   :  0.36330E-01 0.62032E+03
   Friction velocity        uk    :  0.13790E+00 0.12370E+03
   Dimensionless distance   yplus :  0.10623E+01 0.13653E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1007
   Nb of faces within the viscous sub-layer     :         17
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.14449E+05    5980   0.10057E+01   0.15719E+04 
c  VelocityY    0.14449E+05    5980   0.10057E+01   0.00000E+00 
c  VelocityZ    0.14449E+05    5980   0.10057E+01   0.00000E+00 
c  Pressure     0.32775E+02     588   0.74864E-02   0.13823E+00 
c  k            0.17392E+07     280   0.29244E-03   0.16263E+07 
c  epsilon      0.17112E+12     141   0.44631E-03   0.21524E+17 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2044.9          726.33         -4.0154           -1.49
v  Velocity[Y]                   -3126          7556.6          6.0669          2.7294
v  Velocity[Z]                 -974.54          2318.2        -0.25774        -0.37511
v  ǁVelocityǁ                   0.0938          7696.5          30.503          20.202
v  Pressure                -4.7884e+05      7.6372e+05      1.8655e+05      1.2616e+05
v  k                          0.006503           60657          709.95          413.58
v  epsilon                      1.5891      1.0478e+10       4.176e+07      2.5355e+07
v  turbulent_viscosity      0.00016881          40.834          2.2242          1.2742
v  CourantNb                    1.2894      1.2451e+07            9054          4695.7
v  FourierNb                    6.4668           80544          3728.8          1536.6
v  total_pressure                21159      1.2637e+06      6.8655e+05      6.2616e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.2652      1.2452e+07           12783          6232.3


 TIME FOR THE TIME STEP              129:        0.91609E+01

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


 INSTANT    0.130000000E+02   TIME STEP NUMBER             130
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.101474221E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273356153E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41287E+05 0.17510E+04
   Friction velocity        uet   :  0.29803E-01 0.71045E+03
   Friction velocity        uk    :  0.76232E-01 0.13164E+03
   Dimensionless distance   yplus :  0.85845E+00 0.14569E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        667
   Nb of faces within the viscous sub-layer     :         23
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         49 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.16629E+05    6526   0.99931E+00   0.17658E+04 
c  VelocityY    0.16629E+05    6526   0.99931E+00   0.00000E+00 
c  VelocityZ    0.16629E+05    6526   0.99931E+00   0.00000E+00 
c  Pressure     0.35632E+02     574   0.72171E-02   0.14012E+00 
c  k            0.21193E+07     257   0.28303E-03   0.15625E+07 
c  epsilon      0.22204E+12     138   0.37152E-03   0.25887E+17 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2317.4          783.02         -3.0809         -1.7383
v  Velocity[Y]                 -3478.7          7990.6          6.1914          2.8293
v  Velocity[Z]                 -1026.3          2551.8        -0.93494        -0.57022
v  ǁVelocityǁ                 0.099259          8136.4          31.534          21.093
v  Pressure                -5.1088e+05      8.3364e+05      1.9781e+05      1.3384e+05
v  k                         0.0019508           69339          796.99          472.76
v  epsilon                    0.025592       1.274e+10      4.9858e+07       3.064e+07
v  turbulent_viscosity      0.00041094          43.643          2.3471          1.3749
v  CourantNb                      3.38      1.3392e+07           10155          5209.6
v  FourierNb                    6.6787           86215          3891.5          1631.5
v  total_pressure               -10885      1.3336e+06      6.9781e+05      6.3384e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          17.844      1.3393e+07           14046          6841.1


 TIME FOR THE TIME STEP              130:        0.98406E+01

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


 INSTANT    0.131000000E+02   TIME STEP NUMBER             131
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.853908191E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273393992E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35502E+05 0.19778E+04
   Friction velocity        uet   :  0.69039E-02 0.75069E+03
   Friction velocity        uk    :  0.20593E-01 0.14156E+03
   Dimensionless distance   yplus :  0.40231E+00 0.15514E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        724
   Nb of faces within the viscous sub-layer     :         28
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.20452E+05    6391   0.10068E+01   0.21928E+04 
c  VelocityY    0.20452E+05    6391   0.10068E+01   0.00000E+00 
c  VelocityZ    0.20452E+05    6391   0.10068E+01   0.00000E+00 
c  Pressure     0.38087E+02     591   0.74564E-02   0.13992E+00 
c  k            0.25365E+07     231   0.31859E-03   0.22120E+07 
c  epsilon      0.28445E+12     138   0.41920E-03   0.47006E+17 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2305.4           842.1         -4.1425         -1.8732
v  Velocity[Y]                 -3762.5          9059.2          10.424          2.9427
v  Velocity[Z]                   -1094          2815.1        -0.58758        -0.43545
v  ǁVelocityǁ                  0.37698          9237.6          39.601          25.978
v  Pressure                -5.4498e+05      8.9745e+05      2.1119e+05       1.428e+05
v  k                         0.0012221           77995          873.89           517.6
v  epsilon                     0.47898       1.613e+10      6.0325e+07       3.684e+07
v  turbulent_viscosity      0.00039371          46.536          2.7251          1.5717
v  CourantNb                   0.26722      1.4901e+07           10667            5458
v  FourierNb                     6.796           92206          4558.2          1878.7
v  total_pressure               -44984      1.3975e+06      7.1119e+05       6.428e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          16.925      1.4902e+07           15225          7336.8


 TIME FOR THE TIME STEP              131:        0.97199E+01

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


 INSTANT    0.132000000E+02   TIME STEP NUMBER             132
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.641000971E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273400805E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35474E+05 0.19753E+04
   Friction velocity        uet   :  0.31684E-01 0.85024E+03
   Friction velocity        uk    :  0.10133E+00 0.15131E+03
   Dimensionless distance   yplus :  0.10647E+01 0.16575E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        627
   Nb of faces within the viscous sub-layer     :          8
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         46 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.21632E+05    7263   0.99916E+00   0.22270E+04 
c  VelocityY    0.21632E+05    7263   0.99916E+00   0.00000E+00 
c  VelocityZ    0.21632E+05    7263   0.99916E+00   0.00000E+00 
c  Pressure     0.41263E+02     569   0.72425E-02   0.14125E+00 
c  k            0.31157E+07     243   0.26019E-03   0.26230E+07 
c  epsilon      0.37176E+12     136   0.34247E-03   0.50518E+17 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2655.9          915.39         -3.0196         -2.1581
v  Velocity[Y]                 -4174.7            9637          7.6064          3.0793
v  Velocity[Z]                 -1175.9          3021.3        -0.63163        -0.75903
v  ǁVelocityǁ                  0.12298          9809.3          32.589          22.662
v  Pressure                -5.8166e+05      9.8193e+05      2.2352e+05      1.5108e+05
v  k                        0.00047761           89649          1024.7          605.96
v  epsilon                       2.341      1.8573e+10      7.2984e+07      4.4678e+07
v  turbulent_viscosity      0.00012216          49.266          2.2333          1.3753
v  CourantNb                   0.55722      1.6128e+07           12729          6459.9
v  FourierNb                    6.4526           97272            3599          1580.6
v  total_pressure               -81663      1.4819e+06      7.2352e+05      6.5108e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          24.304      1.6129e+07           16328          8040.5


 TIME FOR THE TIME STEP              132:        0.10855E+02

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


 INSTANT    0.133000000E+02   TIME STEP NUMBER             133
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.543717212E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273384083E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30126E+05 0.22736E+04
   Friction velocity        uet   :  0.12272E-01 0.88730E+03
   Friction velocity        uk    :  0.11292E+00 0.16013E+03
   Dimensionless distance   yplus :  0.14838E+01 0.17533E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        672
   Nb of faces within the viscous sub-layer     :         14
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         54 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29496E+05    6397   0.10082E+01   0.21672E+04 
c  VelocityY    0.29496E+05    6397   0.10082E+01   0.00000E+00 
c  VelocityZ    0.29496E+05    6397   0.10082E+01   0.00000E+00 
c  Pressure     0.44057E+02     591   0.72912E-02   0.14086E+00 
c  k            0.37230E+07     234   0.32482E-03   0.37355E+07 
c  epsilon      0.47471E+12     138   0.44296E-03   0.95249E+17 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2628.8          960.71         -5.6841          -1.986
v  Velocity[Y]                 -4548.4           10894          8.5079            3.26
v  Velocity[Z]                 -1257.4          3373.2         -0.4203        -0.47608
v  ǁVelocityǁ                  0.11361           11080          37.941          24.517
v  Pressure                -6.2016e+05      1.0594e+06      2.3881e+05      1.6147e+05
v  k                        0.00014226      1.0239e+05          1123.7          663.85
v  epsilon                     0.10278       2.264e+10      8.7712e+07      5.3508e+07
v  turbulent_viscosity      1.7885e-06          53.585          2.8954          1.7333
v  CourantNb                   0.28309      1.8025e+07           11442          5925.2
v  FourierNb                    7.1339      1.0581e+05          4757.7          2014.9
v  total_pressure          -1.2016e+05      1.5594e+06      7.3881e+05      6.6147e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.567      1.8027e+07           16200          7940.1


 TIME FOR THE TIME STEP              133:        0.97254E+01

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


 INSTANT    0.134000000E+02   TIME STEP NUMBER             134
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.366423494E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273415881E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25509E+05 0.22589E+04
   Friction velocity        uet   :  0.13616E-01 0.98718E+03
   Friction velocity        uk    :  0.93243E-01 0.17095E+03
   Dimensionless distance   yplus :  0.10783E+01 0.18930E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        606
   Nb of faces within the viscous sub-layer     :         36
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         52 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.28922E+05    6728   0.99785E+00   0.36092E+04 
c  VelocityY    0.28922E+05    6728   0.99785E+00   0.00000E+00 
c  VelocityZ    0.28922E+05    6728   0.99785E+00   0.00000E+00 
c  Pressure     0.48032E+02     571   0.72642E-02   0.14296E+00 
c  k            0.45459E+07     286   0.26489E-03   0.47177E+07 
c  epsilon      0.61584E+12     141   0.37456E-03   0.12452E+18 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2971.1          1069.7          -3.165         -2.3568
v  Velocity[Y]                 -5031.8           11532          9.6753          3.4336
v  Velocity[Z]                 -1412.3          3680.1         0.72529        -0.73544
v  ǁVelocityǁ                 0.074434           11769          44.763          29.475
v  Pressure                -6.6283e+05      1.1604e+06      2.5302e+05      1.7106e+05
v  k                        0.00071009      1.1645e+05          1349.3          794.54
v  epsilon                     0.32963      2.7621e+10      1.0759e+08      6.5516e+07
v  turbulent_viscosity      3.7869e-06          57.278           2.575          1.5417
v  CourantNb                    4.6128      1.9353e+07           12991          6503.6
v  FourierNb                    6.8747      1.1321e+05          4195.4          1800.4
v  total_pressure          -1.6283e+05      1.6604e+06      7.5302e+05      6.7106e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          19.881      1.9355e+07           17186            8304


 TIME FOR THE TIME STEP              134:        0.10161E+02

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


 INSTANT    0.135000000E+02   TIME STEP NUMBER             135
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.267854323E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273402590E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17325E+05 0.25457E+04
   Friction velocity        uet   :  0.15784E-01 0.10029E+04
   Friction velocity        uk    :  0.13839E+00 0.18279E+03
   Dimensionless distance   yplus :  0.11761E+01 0.20118E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        634
   Nb of faces within the viscous sub-layer     :         11
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.41453E+05    7003   0.10067E+01   0.31645E+04 
c  VelocityY    0.41453E+05    7003   0.10067E+01   0.00000E+00 
c  VelocityZ    0.41453E+05    7003   0.10067E+01   0.00000E+00 
c  Pressure     0.51317E+02     589   0.74213E-02   0.14248E+00 
c  k            0.54241E+07     263   0.31069E-03   0.57483E+07 
c  epsilon      0.78626E+12     141   0.39596E-03   0.19495E+18 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3003.1          1104.7         -5.0762         -2.3435
v  Velocity[Y]                 -5434.2           13075          6.3936          3.7125
v  Velocity[Z]                 -1759.2          3947.7         -1.4031        -0.53233
v  ǁVelocityǁ                 0.081487           13302          44.404          28.506
v  Pressure                -7.0785e+05      1.2559e+06      2.7009e+05      1.8258e+05
v  k                        0.00033867      1.3111e+05          1482.1          852.49
v  epsilon                     0.10847      3.4309e+10      1.2899e+08      7.7671e+07
v  turbulent_viscosity       1.698e-05          60.787          3.3985          2.1007
v  CourantNb                    11.559      2.1547e+07           14875          7485.6
v  FourierNb                    6.4861      1.1959e+05          5523.8          2379.8
v  total_pressure          -2.0785e+05      1.7559e+06      7.7009e+05      6.8258e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          25.559      2.1549e+07           20399          9865.4


 TIME FOR THE TIME STEP              135:        0.10502E+02

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


 INSTANT    0.136000000E+02   TIME STEP NUMBER             136
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.618175627E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273408766E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11690E+05 0.25880E+04
   Friction velocity        uet   :  0.11725E-01 0.11020E+04
   Friction velocity        uk    :  0.15379E+00 0.19474E+03
   Dimensionless distance   yplus :  0.11972E+01 0.21443E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        529
   Nb of faces within the viscous sub-layer     :          8
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.37556E+05    7942   0.99839E+00   0.21732E+04 
c  VelocityY    0.37556E+05    7942   0.99839E+00   0.00000E+00 
c  VelocityZ    0.37556E+05    7942   0.99839E+00   0.00000E+00 
c  Pressure     0.55892E+02     581   0.71066E-02   0.14434E+00 
c  k            0.65890E+07     210   0.30221E-03   0.68335E+07 
c  epsilon      0.10166E+13     152   0.37421E-03   0.21721E+18 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3410.5          1296.3         -5.1299         -2.8103
v  Velocity[Y]                 -6029.2           13847          7.1486          3.7741
v  Velocity[Z]                 -1729.6          4406.5         -2.6061        -0.79124
v  ǁVelocityǁ                  0.14768           14092          42.257          28.156
v  Pressure                -7.5504e+05      1.3709e+06      2.8517e+05       1.927e+05
v  k                          0.001284      1.4941e+05          1617.2          962.93
v  epsilon                     0.56283      3.9303e+10      1.5079e+08      9.2884e+07
v  turbulent_viscosity      8.2669e-07          64.703          3.4121          1.8724
v  CourantNb                    1.9886      2.3414e+07           15237          7538.6
v  FourierNb                    10.536      1.2861e+05          5757.3          2315.1
v  total_pressure          -2.5504e+05      1.8709e+06      7.8517e+05       6.927e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          18.907      2.3416e+07           20994          9853.7


 TIME FOR THE TIME STEP              136:        0.11861E+02

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


 INSTANT    0.137000000E+02   TIME STEP NUMBER             137
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.611854596E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273392646E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50529E+04 0.29311E+04
   Friction velocity        uet   :  0.13922E-01 0.11142E+04
   Friction velocity        uk    :  0.11032E+00 0.20630E+03
   Dimensionless distance   yplus :  0.10235E+01 0.22686E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        840
   Nb of faces within the viscous sub-layer     :          7
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.60881E+05    7016   0.10091E+01   0.49074E+04 
c  VelocityY    0.60881E+05    7016   0.10091E+01   0.00000E+00 
c  VelocityZ    0.60881E+05    7016   0.10091E+01   0.00000E+00 
c  Pressure     0.59845E+02     589   0.75952E-02   0.14418E+00 
c  k            0.78254E+07     312   0.29182E-03   0.11296E+08 
c  epsilon      0.12875E+13     171   0.41639E-03   0.42324E+18 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3382.8          1430.2         -8.1355         -2.6167
v  Velocity[Y]                 -6613.7           15356          9.6982          3.8909
v  Velocity[Z]                 -1904.2          4869.3          -1.123        -0.74372
v  ǁVelocityǁ                   0.1896           15625          57.391          38.234
v  Pressure                -8.0738e+05      1.4801e+06      3.0305e+05      2.0481e+05
v  k                        0.00016059      1.6696e+05          1880.3          1105.8
v  epsilon                    0.082158      4.8248e+10      1.8559e+08      1.1258e+08
v  turbulent_viscosity      4.5531e-06          68.812          3.5694          1.9802
v  CourantNb                    7.8745      2.5974e+07           15127          7556.7
v  FourierNb                      7.82      1.3295e+05            5990          2429.4
v  total_pressure          -3.0738e+05      1.9801e+06      8.0305e+05      7.0481e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          16.954      2.5978e+07           21117          9986.1


 TIME FOR THE TIME STEP              137:        0.10529E+02

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


 INSTANT    0.138000000E+02   TIME STEP NUMBER             138
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.214636830E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273441673E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24989E+03 0.29167E+04
   Friction velocity        uet   :  0.22371E-01 0.11966E+04
   Friction velocity        uk    :  0.96453E-01 0.21847E+03
   Dimensionless distance   yplus :  0.10272E+01 0.24158E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        831
   Nb of faces within the viscous sub-layer     :         17
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.50312E+05    7612   0.99838E+00   0.69698E+04 
c  VelocityY    0.50312E+05    7612   0.99838E+00   0.00000E+00 
c  VelocityZ    0.50312E+05    7612   0.99838E+00   0.00000E+00 
c  Pressure     0.65134E+02     569   0.71893E-02   0.14587E+00 
c  k            0.95202E+07     266   0.29570E-03   0.11196E+08 
c  epsilon      0.16636E+13     191   0.34697E-03   0.49151E+18 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3861.7          1697.2         -3.9623         -2.9366
v  Velocity[Y]                 -7377.5           15834          9.4968          4.2632
v  Velocity[Z]                 -2111.7          5224.4       -0.003208         -1.0246
v  ǁVelocityǁ                  0.18777           16177          50.544           33.59
v  Pressure                -8.6094e+05      1.6093e+06      3.1979e+05      2.1622e+05
v  k                         0.0014093      1.8809e+05          2144.3          1274.7
v  epsilon                     0.78057      5.6782e+10      2.2203e+08      1.3627e+08
v  turbulent_viscosity      1.1096e-06          71.761          3.6062           2.124
v  CourantNb                    3.8478      2.8841e+07           18838          9476.8
v  FourierNb                    7.3302      1.4169e+05          5925.6          2494.1
v  total_pressure          -3.6094e+05      2.1093e+06      8.1979e+05      7.1622e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          16.596      2.8847e+07           24763           11971


 TIME FOR THE TIME STEP              138:        0.11414E+02

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


 INSTANT    0.139000000E+02   TIME STEP NUMBER             139
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.219569257E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273447308E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15618E+03 0.53066E+04
   Friction velocity        uet   :  0.52477E-02 0.11735E+04
   Friction velocity        uk    :  0.11174E+00 0.23300E+03
   Dimensionless distance   yplus :  0.13233E+01 0.25662E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        648
   Nb of faces within the viscous sub-layer     :         17
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.80214E+05    8198   0.10076E+01   0.67704E+04 
c  VelocityY    0.80214E+05    8198   0.10076E+01   0.00000E+00 
c  VelocityZ    0.80214E+05    8198   0.10076E+01   0.00000E+00 
c  Pressure     0.69322E+02     591   0.74714E-02   0.14482E+00 
c  k            0.11332E+08     268   0.32107E-03   0.16794E+08 
c  epsilon      0.21063E+13     205   0.45068E-03   0.93354E+18 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -4118.6          1803.2         -7.4268         -2.8272
v  Velocity[Y]                 -7894.2           17695          10.371          4.4843
v  Velocity[Z]                 -2521.5            5671         -1.4661        -0.66481
v  ǁVelocityǁ                  0.12784           18044          62.032          41.405
v  Pressure                -9.1728e+05      1.7408e+06      3.4301e+05      2.3209e+05
v  k                         0.0015026      2.1144e+05          2346.8          1391.6
v  epsilon                     0.20448      7.2079e+10      2.6853e+08      1.6378e+08
v  turbulent_viscosity      9.8983e-05          75.892          4.3386          2.4249
v  CourantNb                    3.0281       3.273e+07           18042          8921.7
v  FourierNb                    6.6389      1.5007e+05          7298.4          2945.9
v  total_pressure          -4.1728e+05      2.2408e+06      8.4301e+05      7.3209e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          36.146      3.2742e+07           25340           11868


 TIME FOR THE TIME STEP              139:        0.12159E+02

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


 INSTANT    0.140000000E+02   TIME STEP NUMBER             140
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.526067229E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273489353E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.79032E+02 0.95001E+04
   Friction velocity        uet   :  0.10331E-01 0.12717E+04
   Friction velocity        uk    :  0.10231E+00 0.24804E+03
   Dimensionless distance   yplus :  0.12599E+01 0.27978E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        276
   Nb of faces within the viscous sub-layer     :         13
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.75571E+05    8007   0.99938E+00   0.73182E+04 
c  VelocityY    0.75571E+05    8007   0.99938E+00   0.00000E+00 
c  VelocityZ    0.75571E+05    8007   0.99938E+00   0.00000E+00 
c  Pressure     0.76124E+02     555   0.72866E-02   0.14768E+00 
c  k            0.13895E+08     314   0.25116E-03   0.18961E+08 
c  epsilon      0.27396E+13     233   0.33996E-03   0.10410E+19 
---------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                   -4373          1968.1         -7.1658         -3.7245
v  Velocity[Y]                 -9080.3           18411           9.871          4.5557
v  Velocity[Z]                 -2440.3          6311.6         -1.1937         -1.0833
v  ǁVelocityǁ                  0.30906           18808          65.047          42.766
v  Pressure                -9.8028e+05      1.8964e+06      3.6102e+05       2.439e+05
v  k                        0.00021753      2.4116e+05          2807.6          1659.6
v  epsilon                     0.15443      8.4944e+10      3.2728e+08      2.0056e+08
v  turbulent_viscosity      9.0318e-05          80.378          3.5351          2.1216
v  CourantNb                    6.0368       3.591e+07           21011           10475
v  FourierNb                    7.1932      1.5924e+05          5712.5          2464.3
v  total_pressure          -4.8028e+05      2.3964e+06      8.6102e+05       7.439e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          17.557      3.5932e+07           26724           12939


 TIME FOR THE TIME STEP              140:        0.11979E+02

===============================================================


 INSTANT    0.141000000E+02   TIME STEP NUMBER             141
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.191514264E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273446211E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10136E+03 0.13413E+05
   Friction velocity        uet   :  0.12053E-01 0.12597E+04
   Friction velocity        uk    :  0.17245E+00 0.26582E+03
   Dimensionless distance   yplus :  0.20148E+01 0.28937E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        383
   Nb of faces within the viscous sub-layer     :          2
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10868E+06    7251   0.10068E+01   0.12073E+05 
c  VelocityY    0.10868E+06    7251   0.10068E+01   0.00000E+00 
c  VelocityZ    0.10868E+06    7251   0.10068E+01   0.00000E+00 
c  Pressure     0.81804E+02     641   0.81588E-02   0.14783E+00 
c  k            0.16409E+08     348   0.31894E-03   0.31237E+08 
c  epsilon      0.34591E+13     256   0.38713E-03   0.18407E+19 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                   -4997          2001.2         -9.0686         -3.1382
v  Velocity[Y]                 -9466.5           21260          5.4764          4.2595
v  Velocity[Z]                 -2708.2          6932.2          5.5625         -1.1673
v  ǁVelocityǁ                  0.37389           21684          80.394          53.925
v  Pressure                -1.0334e+06      2.0734e+06      4.0176e+05      2.7212e+05
v  k                          0.016133      2.7566e+05          3088.6          1786.3
v  epsilon                      3.7903      1.0516e+11      3.9776e+08      2.3897e+08
v  turbulent_viscosity      7.5612e-07          86.082          4.6535          2.7328
v  CourantNb                    15.929      3.9613e+07           22381           10960
v  FourierNb                    6.8252      1.6847e+05          7656.5          3206.1
v  total_pressure          -5.3341e+05      2.5734e+06      9.0176e+05      7.7212e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          38.447      3.9659e+07           30037           14166


 TIME FOR THE TIME STEP              141:        0.10924E+02

===============================================================


 INSTANT    0.142000000E+02   TIME STEP NUMBER             142
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.781109162E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273466323E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16551E+03 0.18195E+05
   Friction velocity        uet   :  0.19746E-01 0.13999E+04
   Friction velocity        uk    :  0.19929E+00 0.28245E+03
   Dimensionless distance   yplus :  0.16773E+01 0.30936E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        267
   Nb of faces within the viscous sub-layer     :          4
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10200E+06    9135   0.99943E+00   0.12331E+05 
c  VelocityY    0.10200E+06    9135   0.99943E+00   0.00000E+00 
c  VelocityZ    0.10200E+06    9135   0.99943E+00   0.00000E+00 
c  Pressure     0.89056E+02     535   0.72889E-02   0.14944E+00 
c  k            0.20290E+08     342   0.29320E-03   0.30812E+08 
c  epsilon      0.45310E+13     268   0.41513E-03   0.23035E+19 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -5258.1          2466.4         -6.2354         -3.9311
v  Velocity[Y]                  -10784           22016          11.846          5.4172
v  Velocity[Z]                 -2962.2          7570.3         -3.0368          -1.326
v  ǁVelocityǁ                  0.34596           22539          66.457          44.767
v  Pressure                -1.1087e+06      2.2374e+06      4.1555e+05      2.8068e+05
v  k                         0.0032263      3.1557e+05          3590.5            2088
v  epsilon                      15.457      1.1902e+11       4.847e+08      2.9067e+08
v  turbulent_viscosity      0.00051146          92.915          4.0402          2.3328
v  CourantNb                    0.2742      4.2626e+07           26182           13038
v  FourierNb                    9.4768      1.8361e+05          6635.6          2779.8
v  total_pressure          -6.0872e+05      2.7374e+06      9.1555e+05      7.8068e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          32.152      4.2717e+07           32817           15817


 TIME FOR THE TIME STEP              142:        0.13550E+02

===============================================================


 INSTANT    0.143000000E+02   TIME STEP NUMBER             143
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.268138274E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273044733E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12142E+03 0.20657E+05
   Friction velocity        uet   :  0.25571E-01 0.13850E+04
   Friction velocity        uk    :  0.23914E+00 0.30022E+03
   Dimensionless distance   yplus :  0.16043E+01 0.33080E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        184
   Nb of faces within the viscous sub-layer     :          4
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         24 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.15620E+06    7226   0.10087E+01   0.10348E+05 
c  VelocityY    0.15620E+06    7226   0.10087E+01   0.00000E+00 
c  VelocityZ    0.15620E+06    7226   0.10087E+01   0.00000E+00 
c  Pressure     0.97109E+02     642   0.92009E-02   0.15179E+00 
c  k            0.24576E+08     361   0.37421E-03   0.66608E+08 
c  epsilon      0.58759E+13     284   0.50885E-03   0.53259E+19 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -5863.2          2670.6         -8.1736         -3.4998
v  Velocity[Y]                  -11396           25325          7.5254          4.2907
v  Velocity[Z]                 -3256.4          8277.1         -2.6763         -1.1254
v  ǁVelocityǁ                  0.30966           25856           82.34          54.172
v  Pressure                 -1.169e+06      2.4824e+06      4.6677e+05      3.1669e+05
v  k                          0.060989       3.539e+05          4097.3          2398.9
v  epsilon                     0.45501      1.5198e+11      6.0663e+08       3.625e+08
v  turbulent_viscosity      1.0367e-05          100.44          4.8207          2.9041
v  CourantNb                    2.4159      4.7226e+07           23876           11702
v  FourierNb                    10.257      1.9841e+05          7876.4          3337.9
v  total_pressure          -6.6899e+05      2.9824e+06      9.6677e+05      8.1669e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          60.643      4.7408e+07           31752           15040


 TIME FOR THE TIME STEP              143:        0.10892E+02

===============================================================


 INSTANT    0.144000000E+02   TIME STEP NUMBER             144
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.814804889E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273485221E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16139E+03 0.24174E+05
   Friction velocity        uet   :  0.14286E-01 0.15414E+04
   Friction velocity        uk    :  0.17791E+00 0.32030E+03
   Dimensionless distance   yplus :  0.15238E+01 0.35289E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         48
   Nb of faces within the viscous sub-layer     :          3
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.13651E+06    8173   0.10002E+01   0.12297E+05 
c  VelocityY    0.13651E+06    8173   0.10002E+01   0.00000E+00 
c  VelocityZ    0.13651E+06    8173   0.10002E+01   0.00000E+00 
c  Pressure     0.10455E+03     550   0.73297E-02   0.15167E+00 
c  k            0.30186E+08     360   0.29929E-03   0.91579E+08 
c  epsilon      0.78830E+13     292   0.33791E-03   0.95610E+19 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -6263.8          3042.5         -10.221         -3.6795
v  Velocity[Y]                  -12895           26400          9.8822          5.7563
v  Velocity[Z]                 -3677.3          8859.6         -1.7234           -1.54
v  ǁVelocityǁ                  0.19265           26931          82.745          54.311
v  Pressure                -1.2518e+06      2.6637e+06      4.8214e+05      3.2671e+05
v  k                           0.11264       4.073e+05          5280.7          2972.3
v  epsilon                      66.085      1.8407e+11      8.0948e+08       4.693e+08
v  turbulent_viscosity      0.00032541          372.01           5.019          2.8545
v  CourantNb                      2.16      5.1366e+07           27997           13652
v  FourierNb                    15.124       2.846e+05          8324.2            3428
v  total_pressure          -7.5184e+05      3.1637e+06      9.8214e+05      8.2671e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           47.09      5.1651e+07           36321           17081


 TIME FOR THE TIME STEP              144:        0.12245E+02

===============================================================


 INSTANT    0.145000000E+02   TIME STEP NUMBER             145
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.128871955E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273067761E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55567E+02 0.25904E+05
   Friction velocity        uet   :  0.13339E-01 0.15381E+04
   Friction velocity        uk    :  0.21971E+00 0.34544E+03
   Dimensionless distance   yplus :  0.12251E+01 0.37726E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        124
   Nb of faces within the viscous sub-layer     :          4
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         48 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.22109E+06    8709   0.10063E+01   0.30357E+05 
c  VelocityY    0.22109E+06    8709   0.10063E+01   0.00000E+00 
c  VelocityZ    0.22109E+06    8709   0.10063E+01   0.00000E+00 
c  Pressure     0.11360E+03     623   0.10063E-01   0.15311E+00 
c  k            0.38244E+08     345   0.30350E-03   0.12871E+09 
c  epsilon      0.12380E+14     277   0.33859E-03   0.34417E+20 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -7009.4          2922.1         -8.8611          -4.237
v  Velocity[Y]                  -13704           30257          20.573          4.5752
v  Velocity[Z]                 -3595.7          9990.2         -2.3532         -1.2332
v  ǁVelocityǁ                  0.58849           30857          124.87          85.495
v  Pressure                 -1.331e+06      2.9669e+06      5.3079e+05         3.6e+05
v  k                          0.027681      4.6395e+05          6108.7            3482
v  epsilon                      4.2013      2.5322e+11      1.1393e+09      6.2805e+08
v  turbulent_viscosity       0.0026792          113.13           7.785          4.0049
v  CourantNb                     3.456      5.6883e+07           29168           14038
v  FourierNb                    11.192      4.5371e+05           13498            5131
v  total_pressure          -8.3096e+05      3.4669e+06      1.0308e+06         8.6e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          50.234      5.7337e+07           42666           19169


 TIME FOR THE TIME STEP              145:        0.12935E+02

===============================================================


 INSTANT    0.146000000E+02   TIME STEP NUMBER             146
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.131197685E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273525900E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15770E+03 0.27986E+05
   Friction velocity        uet   :  0.21565E-01 0.17189E+04
   Friction velocity        uk    :  0.20285E+00 0.36863E+03
   Dimensionless distance   yplus :  0.19134E+01 0.40179E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        142
   Nb of faces within the viscous sub-layer     :          3
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.19003E+06    7750   0.99868E+00   0.36535E+05 
c  VelocityY    0.19003E+06    7750   0.99868E+00   0.00000E+00 
c  VelocityZ    0.19003E+06    7750   0.99868E+00   0.00000E+00 
c  Pressure     0.12266E+03     516   0.73389E-02   0.15315E+00 
c  k            0.50629E+08     297   0.27674E-03   0.14636E+09 
c  epsilon      0.26258E+14     240   0.17881E-03   0.83799E+20 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -8122.8                             1


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -7193.2          3644.9         -10.656         -4.7824
v  Velocity[Y]                  -15517           31230          14.833          5.6632
v  Velocity[Z]                 -4463.2           10787          -4.187         -1.8217
v  ǁVelocityǁ                 0.030759           31965          96.186           64.29
v  Pressure                -1.4301e+06      3.1981e+06      5.5172e+05        3.74e+05
v  k                          0.023841      6.3547e+05          6490.3          3698.8
v  epsilon                      17.345      5.5012e+11      1.5024e+09      7.9105e+08
v  turbulent_viscosity      0.00016379          122.47          5.9324           3.634
v  CourantNb                    16.521        6.09e+07           38866           19681
v  FourierNb                    12.116      4.5741e+05          9590.8          4123.3
v  total_pressure          -9.3015e+05      3.6981e+06      1.0517e+06        8.74e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           49.57      6.1357e+07           48457           23804


 TIME FOR THE TIME STEP              146:        0.11634E+02

===============================================================


 INSTANT    0.147000000E+02   TIME STEP NUMBER             147
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.115685328E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273526064E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12649E+03 0.28953E+05
   Friction velocity        uet   :  0.20666E-01 0.17225E+04
   Friction velocity        uk    :  0.24360E+00 0.38628E+03
   Dimensionless distance   yplus :  0.18672E+01 0.42931E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        368
   Nb of faces within the viscous sub-layer     :          4
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30950E+06    7847   0.10062E+01   0.22823E+05 
c  VelocityY    0.30950E+06    7847   0.10062E+01   0.00000E+00 
c  VelocityZ    0.30950E+06    7847   0.10062E+01   0.00000E+00 
c  Pressure     0.13094E+03     644   0.94499E-02   0.15199E+00 
c  k            0.69471E+08     269   0.28483E-03   0.21143E+09 
c  epsilon      0.57876E+14     215   0.14125E-03   0.21632E+21 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -9020.2          3487.3         -12.625         -4.7355
v  Velocity[Y]                  -16314           36151         -9.1777          3.8237
v  Velocity[Z]                 -5135.5           11615         -3.4206         -1.4323
v  ǁVelocityǁ                  0.31241           36877          132.64          86.555
v  Pressure                -1.5045e+06       3.557e+06      6.2756e+05      4.2662e+05
v  k                         0.0043441      8.8602e+05          7468.4          4194.7
v  epsilon                      2.2374      1.1789e+12      2.1164e+09      1.0573e+09
v  turbulent_viscosity      0.00066549          129.96          5.5826          3.3166
v  CourantNb                    1.0381      6.7797e+07           33778           16348
v  FourierNb                    10.887       5.642e+05          9084.7          3856.6
v  total_pressure          -1.0045e+06       4.057e+06      1.1276e+06      9.2662e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          28.332      6.8361e+07           42862           20204


 TIME FOR THE TIME STEP              147:        0.11732E+02

===============================================================


 INSTANT    0.148000000E+02   TIME STEP NUMBER             148
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.264916518E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273617583E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61644E+03 0.31250E+05
   Friction velocity        uet   :  0.10377E-01 0.19686E+04
   Friction velocity        uk    :  0.29163E+00 0.41610E+03
   Dimensionless distance   yplus :  0.23158E+01 0.45639E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        487
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.26222E+06    8960   0.99973E+00   0.22138E+05 
c  VelocityY    0.26222E+06    8960   0.99973E+00   0.00000E+00 
c  VelocityZ    0.26222E+06    8960   0.99973E+00   0.00000E+00 
c  Pressure     0.14390E+03     533   0.72647E-02   0.15465E+00 
c  k            0.93273E+08     242   0.23484E-03   0.28604E+09 
c  epsilon      0.11786E+15     186   0.74169E-04   0.29656E+21 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k               -1.3871                             1
a  epsilon     -1.8429e+05                             5


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -8702.7          4264.5          -8.872         -4.6938
v  Velocity[Y]                  -18781           37375          13.119          6.8335
v  Velocity[Z]                 -5452.3           12864         -1.7829         -1.9932
v  ǁVelocityǁ                  0.48624           38173           94.44          63.357
v  Pressure                -1.7237e+06      3.8132e+06      6.3849e+05       4.324e+05
v  k                           0.21908      1.3598e+06          8976.1          4974.1
v  epsilon                      3.3992      1.7599e+12      2.7564e+09      1.3486e+09
v  turbulent_viscosity      0.00013693          140.58          6.0215          3.3951
v  CourantNb                     31.22      7.3824e+07           42798           20715
v  FourierNb                    9.9025      5.5364e+05          9943.8          4103.3
v  total_pressure          -1.2237e+06      4.3132e+06      1.1385e+06       9.324e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           67.81       7.437e+07           52742           24818


 TIME FOR THE TIME STEP              148:        0.13296E+02

===============================================================


 INSTANT    0.149000000E+02   TIME STEP NUMBER             149
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.178932605E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.272876205E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21700E+03 0.32631E+05
   Friction velocity        uet   :  0.71464E-02 0.20002E+04
   Friction velocity        uk    :  0.29138E+00 0.45950E+03
   Dimensionless distance   yplus :  0.24677E+01 0.48579E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        278
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.44796E+06    9440   0.10065E+01   0.71295E+05 
c  VelocityY    0.44796E+06    9440   0.10065E+01   0.00000E+00 
c  VelocityZ    0.44796E+06    9440   0.10065E+01   0.00000E+00 
c  Pressure     0.15938E+03     645   0.10239E-01   0.15871E+00 
c  k            0.12175E+09     279   0.21957E-03   0.32644E+09 
c  epsilon      0.19747E+15     172   0.62739E-04   0.38050E+21 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -10463          4524.2         -14.586         -5.5897
v  Velocity[Y]                  -19459           43311          29.114          2.8004
v  Velocity[Z]                 -5386.3           14344         -4.7796         -1.8433
v  ǁVelocityǁ                  0.41994           44202          183.79          125.38
v  Pressure                -1.7623e+06      4.2782e+06       7.288e+05      4.9624e+05
v  k                        0.00013614      1.8145e+06           10194          5851.5
v  epsilon                      2.6914      2.6612e+12      3.5926e+09      1.7319e+09
v  turbulent_viscosity      0.00034381          153.09          8.2545          4.3328
v  CourantNb                    13.136      8.0953e+07           35500           16932
v  FourierNb                    11.761      5.8138e+05           14173          5472.2
v  total_pressure          -1.2623e+06      4.7782e+06      1.2288e+06      9.9624e+05


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          76.737      8.1534e+07           49673           22404


 TIME FOR THE TIME STEP              149:        0.14003E+02

===============================================================


 INSTANT    0.150000000E+02   TIME STEP NUMBER             150
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.432692873E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273713498E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29128E+03 0.35132E+05
   Friction velocity        uet   :  0.49286E-01 0.23133E+04
   Friction velocity        uk    :  0.50692E+00 0.51438E+03
   Dimensionless distance   yplus :  0.26568E+01 0.51643E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        158
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on         82


 Write intermediate restart files
   checkpoint at iteration        150, Physical time    0.15000E+02


   ** Writing the main restart file
      -----------------------------

 Start writing
   End writing the dimensions                           
   End writing the options                              
   End writing the main variables                       
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
   End writing the mass fluxes                          
   End writing the boundary conditions                  
 End writing


 Time for restart files:    0.10902E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.35534E+06    8579   0.99786E+00   0.10682E+06 
c  VelocityY    0.35534E+06    8579   0.99786E+00   0.00000E+00 
c  VelocityZ    0.35534E+06    8579   0.99786E+00   0.00000E+00 
c  Pressure     0.17076E+03     536   0.72955E-02   0.15745E+00 
c  k            0.14609E+09     209   0.22351E-03   0.41377E+09 
c  epsilon      0.29755E+15     156   0.46791E-04   0.45167E+21 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -10440          5234.8         -13.647         -6.1107
v  Velocity[Y]                  -22248           44679          22.778           7.028
v  Velocity[Z]                 -6497.1           15244          5.4786          -2.272
v  ǁVelocityǁ                  0.59285           45710          136.14          89.977
v  Pressure                -2.0645e+06      4.5625e+06      7.3825e+05      5.0119e+05
v  k                         0.0089077      2.3661e+06           11207          6541.4
v  epsilon                      30.018       3.243e+12      4.2343e+09      2.0451e+09
v  turbulent_viscosity       1.552e-09          158.61          6.5554          4.4977
v  CourantNb                    20.275      8.8011e+07           56164           27993
v  FourierNb                    14.629      5.2363e+05           10106          4715.5
v  total_pressure          -1.5645e+06      5.0625e+06      1.2382e+06      1.0012e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          73.957      8.8535e+07           66269           32709


 TIME FOR THE TIME STEP              150:        0.12696E+02

===============================================================


 INSTANT    0.151000000E+02   TIME STEP NUMBER             151
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.198021480E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.272817447E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14985E+03 0.36806E+05
   Friction velocity        uet   :  0.44457E-02 0.23618E+04
   Friction velocity        uk    :  0.54238E+00 0.56968E+03
   Dimensionless distance   yplus :  0.33920E+01 0.55196E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        215
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.64328E+06    9009   0.10088E+01   0.71068E+05 
c  VelocityY    0.64328E+06    9009   0.10088E+01   0.00000E+00 
c  VelocityZ    0.64328E+06    9009   0.10088E+01   0.00000E+00 
c  Pressure     0.18303E+03     659   0.98237E-02   0.15651E+00 
c  k            0.17759E+09     202   0.27253E-03   0.61678E+09 
c  epsilon      0.40412E+15     143   0.47792E-04   0.28586E+21 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -12334          5695.1         -13.988         -5.1425
v  Velocity[Y]                  -23419           51545          14.789          2.7962
v  Velocity[Z]                 -6905.6           16914          1.7881         -2.6878
v  ǁVelocityǁ                  0.45745           52628          185.26          130.47
v  Pressure                -2.1352e+06      5.0882e+06      8.5918e+05      5.8715e+05
v  k                        0.00028857      1.8068e+06           11965          6789.6
v  epsilon                      22.959      3.6209e+12       4.898e+09      2.3621e+09
v  turbulent_viscosity      1.8385e-07          165.16          7.8041          4.8905
v  CourantNb                    6.6159      9.7667e+07           47288           22551
v  FourierNb                     12.68      5.3544e+05           12418          5468.5
v  total_pressure          -1.6352e+06      5.5882e+06      1.3592e+06      1.0872e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          49.674       9.819e+07           59706           28020


 TIME FOR THE TIME STEP              151:        0.13762E+02

===============================================================


 INSTANT    0.152000000E+02   TIME STEP NUMBER             152
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.143931108E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273628548E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43874E+03 0.39638E+05
   Friction velocity        uet   :  0.75452E-02 0.27354E+04
   Friction velocity        uk    :  0.64006E+00 0.55574E+03
   Dimensionless distance   yplus :  0.34288E+01 0.60148E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        433
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         32 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.37939E+06    9189   0.99925E+00   0.47051E+05 
c  VelocityY    0.37939E+06    9189   0.99925E+00   0.00000E+00 
c  VelocityZ    0.37939E+06    9189   0.99925E+00   0.00000E+00 
c  Pressure     0.19864E+03     518   0.71931E-02   0.15723E+00 
c  k            0.19874E+09     211   0.22530E-03   0.56620E+09 
c  epsilon      0.49138E+15     144   0.43736E-04   0.50929E+21 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -13025          6025.5         -14.761         -5.6842
v  Velocity[Y]                  -26604           53452          25.171          6.2132
v  Velocity[Z]                 -8343.3           18327          1.6793         -3.0349
v  ǁVelocityǁ                  0.40381           54592          144.56          94.321
v  Pressure                -2.4541e+06      5.4701e+06      8.8085e+05      6.0093e+05
v  k                         0.0014043      2.5359e+06           13572          7754.9
v  epsilon                      1.5669      4.4643e+12      5.6727e+09      2.7863e+09
v  turbulent_viscosity      2.6873e-08          175.78          7.0664          4.2098
v  CourantNb                    27.904       1.057e+08           58725           29280
v  FourierNb                     12.49      4.6638e+05           11413          4878.8
v  total_pressure          -1.9541e+06      5.9701e+06      1.3808e+06      1.1009e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          125.49      1.0617e+08           70137           34158


 TIME FOR THE TIME STEP              152:        0.13521E+02

===============================================================


 INSTANT    0.153000000E+02   TIME STEP NUMBER             153
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.202722502E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.272862638E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21943E+03 0.42133E+05
   Friction velocity        uet   :  0.17889E-01 0.28145E+04
   Friction velocity        uk    :  0.25157E+00 0.57535E+03
   Dimensionless distance   yplus :  0.20890E+01 0.62148E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        365
   Nb of faces within the viscous sub-layer     :          3
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.90390E+06    7980   0.10057E+01   0.12010E+06 
c  VelocityY    0.90390E+06    7980   0.10057E+01   0.00000E+00 
c  VelocityZ    0.90390E+06    7980   0.10057E+01   0.00000E+00 
c  Pressure     0.21409E+03     678   0.94984E-02   0.15699E+00 
c  k            0.23849E+09     221   0.21483E-03   0.73645E+09 
c  epsilon      0.60406E+15     141   0.54501E-04   0.50129E+21 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -14959          6568.5         -11.496           -6.05
v  Velocity[Y]                  -27756           61963         -5.6366          1.1555
v  Velocity[Z]                 -8745.1           19501          -15.17         -2.7357
v  ǁVelocityǁ                   1.0445           63054          186.88          128.21
v  Pressure                -2.5616e+06      6.0772e+06      1.0417e+06       7.182e+05
v  k                          0.014383       2.566e+06           16121          8963.2
v  epsilon                      21.119      5.1193e+12      6.7973e+09      3.3374e+09
v  turbulent_viscosity      1.8673e-07          189.57          8.2489          4.7826
v  CourantNb                    19.346       1.169e+08           52114           24398
v  FourierNb                    12.147      4.6594e+05           13526          5640.9
v  total_pressure          -2.0616e+06      6.5772e+06      1.5417e+06      1.2182e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          98.411      1.1737e+08           65640           30039


 TIME FOR THE TIME STEP              153:        0.11986E+02

===============================================================


 INSTANT    0.154000000E+02   TIME STEP NUMBER             154
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.917007130E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273793862E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39435E+03 0.48031E+05
   Friction velocity        uet   :  0.36210E-01 0.32693E+04
   Friction velocity        uk    :  0.47154E+00 0.62267E+03
   Dimensionless distance   yplus :  0.60868E+01 0.66247E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        431
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.70361E+06    9242   0.99901E+00   0.14741E+06 
c  VelocityY    0.70361E+06    9242   0.99901E+00   0.00000E+00 
c  VelocityZ    0.70361E+06    9242   0.99901E+00   0.00000E+00 
c  Pressure     0.23391E+03     500   0.70470E-02   0.15870E+00 
c  k            0.27781E+09     221   0.20724E-03   0.94776E+09 
c  epsilon      0.71560E+15     154   0.51352E-04   0.12376E+22 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -15509            7528         -18.511         -6.6539
v  Velocity[Y]                  -31824           63956          17.437          6.5301
v  Velocity[Z]                 -8141.1           22550         -5.8701         -3.3761
v  ǁVelocityǁ                  0.49109           65599          160.35          108.25
v  Pressure                 -2.938e+06      6.5388e+06       1.082e+06      7.4447e+05
v  k                          0.098155      3.1753e+06           18375           10502
v  epsilon                      295.37      7.3347e+12      8.0684e+09      4.0514e+09
v  turbulent_viscosity      1.9537e-05          199.51          11.191          5.8897
v  CourantNb                    71.446      1.2727e+08           62613           30387
v  FourierNb                    9.7718      4.9435e+05           19131            7432
v  total_pressure           -2.438e+06      7.0388e+06       1.582e+06      1.2445e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          126.84      1.2774e+08           81744           37819


 TIME FOR THE TIME STEP              154:        0.13591E+02

===============================================================


 INSTANT    0.155000000E+02   TIME STEP NUMBER             155
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.241057844E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273806056E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25953E+03 0.50916E+05
   Friction velocity        uet   :  0.42676E-01 0.33456E+04
   Friction velocity        uk    :  0.37666E+00 0.68885E+03
   Dimensionless distance   yplus :  0.32990E+01 0.70325E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        379
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.12839E+07    8810   0.10083E+01   0.11248E+06 
c  VelocityY    0.12839E+07    8810   0.10083E+01   0.00000E+00 
c  VelocityZ    0.12839E+07    8810   0.10083E+01   0.00000E+00 
c  Pressure     0.25022E+03     640   0.89537E-02   0.15732E+00 
c  k            0.33866E+09     221   0.23344E-03   0.13466E+10 
c  epsilon      0.92308E+15     150   0.57135E-04   0.13734E+22 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -18393          7691.8         -19.786         -6.6841
v  Velocity[Y]                  -33474           73851         -17.586          3.2192
v  Velocity[Z]                 -9758.8           23546         -11.093         -3.9661
v  ǁVelocityǁ                   1.3411           75314          216.84          141.46
v  Pressure                -3.1384e+06      7.1796e+06      1.2039e+06       8.287e+05
v  k                          0.039713      3.2119e+06           20189           11162
v  epsilon                      104.13      8.1236e+12      9.6469e+09      4.7423e+09
v  turbulent_viscosity       0.0021624          210.94          12.326          6.7163
v  CourantNb                    52.146      1.3964e+08           58683           27781
v  FourierNb                    8.9532      4.8879e+05           20788          8256.9
v  total_pressure          -2.6384e+06      7.6796e+06      1.7039e+06      1.3287e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          87.326      1.4013e+08           79472           36038


 TIME FOR THE TIME STEP              155:        0.13118E+02

===============================================================


 INSTANT    0.156000000E+02   TIME STEP NUMBER             156
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.211001921E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273770303E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14908E+04 0.58135E+05
   Friction velocity        uet   :  0.15884E-01 0.38678E+04
   Friction velocity        uk    :  0.31125E+00 0.71121E+03
   Dimensionless distance   yplus :  0.40553E+01 0.75685E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        475
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.97351E+06    8963   0.99944E+00   0.75163E+05 
c  VelocityY    0.97351E+06    8963   0.99944E+00   0.00000E+00 
c  VelocityZ    0.97351E+06    8963   0.99944E+00   0.00000E+00 
c  Pressure     0.27627E+03     532   0.70174E-02   0.16058E+00 
c  k            0.40193E+09     225   0.20555E-03   0.12591E+10 
c  epsilon      0.11207E+16     164   0.49382E-04   0.24819E+22 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -17546          8838.1         -22.383         -6.7803
v  Velocity[Y]                  -38325           76854           15.04          8.4946
v  Velocity[Z]                  -11035           26156         -8.0484         -3.4535
v  ǁVelocityǁ                  0.44646           78487          164.29          107.71
v  Pressure                 -3.615e+06      7.7063e+06      1.2288e+06      8.4138e+05
v  k                            0.0141      4.0431e+06           22028           12411
v  epsilon                      209.19      1.0936e+13      1.1502e+10       5.694e+09
v  turbulent_viscosity      4.2235e-05          228.66          11.145          6.0929
v  CourantNb                    10.493      1.5341e+08           73156           34306
v  FourierNb                    7.2181      5.7156e+05           18825          7459.5
v  total_pressure           -3.115e+06      8.2063e+06      1.7288e+06      1.3414e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           48.58      1.5394e+08           91981           41766


 TIME FOR THE TIME STEP              156:        0.13217E+02

===============================================================


 INSTANT    0.157000000E+02   TIME STEP NUMBER             157
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.242070338E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.272755949E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32133E+03 0.63138E+05
   Friction velocity        uet   :  0.20995E-01 0.39775E+04
   Friction velocity        uk    :  0.45778E+00 0.73198E+03
   Dimensionless distance   yplus :  0.17159E+01 0.80657E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        464
   Nb of faces within the viscous sub-layer     :          3
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.18495E+07   10000   0.10073E+01   0.40216E+06 
c  VelocityY    0.18495E+07   10000   0.10073E+01   0.00000E+00 
c  VelocityZ    0.18495E+07   10000   0.10073E+01   0.00000E+00 
c  Pressure     0.31195E+03     679   0.12603E-01   0.16733E+00 
c  k            0.50395E+09     419   0.23421E-03   0.36183E+10 
c  epsilon      0.15238E+16     240   0.53215E-04   0.42510E+22 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -22165          8100.8          -25.82         -7.0426
v  Velocity[Y]                  -40014           88188          107.98         -3.4271
v  Velocity[Z]                  -10637           29852          14.783         -2.2858
v  ǁVelocityǁ                     1.77           90173           474.1          318.62
v  Pressure                -3.6186e+06      8.7191e+06      1.4555e+06      1.0027e+06
v  k                         0.0062839      4.3198e+06           27423           16828
v  epsilon                      8.4665      1.2685e+13      1.5359e+10      7.8754e+09
v  turbulent_viscosity      3.6229e-05          249.17          12.223          6.4485
v  CourantNb                    19.644      1.6883e+08           64048           29285
v  FourierNb                     10.64      6.1513e+05           20801          8115.7
v  total_pressure          -3.1186e+06      9.2191e+06      1.9555e+06      1.5027e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          61.549      1.6943e+08           84849           37400


 TIME FOR THE TIME STEP              157:        0.14820E+02

===============================================================


 INSTANT    0.158000000E+02   TIME STEP NUMBER             158
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.182449012E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273973409E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44628E+03 0.72429E+05
   Friction velocity        uet   :  0.49178E-01 0.45486E+04
   Friction velocity        uk    :  0.81285E+00 0.79846E+03
   Dimensionless distance   yplus :  0.65718E+01 0.85074E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        104
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         47 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.91328E+06   10000   0.99175E+00   0.42674E+06 
c  VelocityY    0.91328E+06   10000   0.99175E+00   0.00000E+00 
c  VelocityZ    0.91328E+06   10000   0.99175E+00   0.00000E+00 
c  Pressure     0.33035E+03     519   0.75355E-02   0.16383E+00 
c  k            0.63079E+09     234   0.22453E-03   0.42405E+10 
c  epsilon      0.20344E+16     174   0.48195E-04   0.12510E+23 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k               -39.775                            36
a  epsilon     -1.4544e+07                            46


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -22355           10586         -24.783         -9.7234
v  Velocity[Y]                  -45100           91491          25.652          7.8495
v  Velocity[Z]                  -13665           31050          3.0213         -3.8939
v  ǁVelocityǁ                  0.93079           93586          213.16           141.3
v  Pressure                -4.2211e+06      9.3152e+06      1.4635e+06      1.0087e+06
v  k                          0.018476      6.7019e+06           29074           16987
v  epsilon                      143.96      2.0171e+13      1.8222e+10      8.9723e+09
v  turbulent_viscosity      1.3476e-07          255.39          8.3743          6.4154
v  CourantNb                    45.273      1.8162e+08      1.3421e+05           66222
v  FourierNb                    16.713      6.2843e+05           12257          6214.7
v  total_pressure          -3.7211e+06      9.8152e+06      1.9635e+06      1.5087e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          170.11      1.8225e+08      1.4647e+05           72437


 TIME FOR THE TIME STEP              158:        0.14728E+02

===============================================================


 INSTANT    0.159000000E+02   TIME STEP NUMBER             159
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.639275798E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.272447306E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24780E+03 0.77623E+05
   Friction velocity        uet   :  0.55479E-01 0.46527E+04
   Friction velocity        uk    :  0.56393E+00 0.86453E+03
   Dimensionless distance   yplus :  0.47145E+01 0.89691E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        460
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.26456E+07    9527   0.10081E+01   0.79457E+06 
c  VelocityY    0.26456E+07    9527   0.10081E+01   0.00000E+00 
c  VelocityZ    0.26456E+07    9527   0.10081E+01   0.00000E+00 
c  Pressure     0.35448E+03     660   0.99516E-02   0.16246E+00 
c  k            0.81036E+09     222   0.22792E-03   0.54848E+10 
c  epsilon      0.29906E+16     170   0.44049E-04   0.13470E+23 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0012296                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -26576          9448.6         -37.716         -9.4979
v  Velocity[Y]                  -48419      1.0494e+05          18.878         -0.5765
v  Velocity[Z]                  -11645           36065          24.576         -2.4676
v  ǁVelocityǁ                  0.47582      1.0754e+05          441.49          307.24
v  Pressure                -4.4321e+06       1.032e+07      1.6641e+06      1.1511e+06
v  k                         0.0012296      6.1148e+06           32673           18863
v  epsilon                      331.97      2.1874e+13      2.2467e+10      1.1263e+10
v  turbulent_viscosity      2.0027e-07          260.15          10.244          6.3826
v  CourantNb                    43.235      2.0304e+08           79266           36381
v  FourierNb                    11.979      7.2547e+05           16333          7144.1
v  total_pressure          -3.9321e+06       1.082e+07      2.1641e+06      1.6511e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          109.68      2.0376e+08           95599           43525


 TIME FOR THE TIME STEP              159:        0.14048E+02

===============================================================


 INSTANT    0.160000000E+02   TIME STEP NUMBER             160
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.175799062E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273957522E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32522E+04 0.87072E+05
   Friction velocity        uet   :  0.74974E-01 0.53204E+04
   Friction velocity        uk    :  0.57435E+00 0.10179E+04
   Dimensionless distance   yplus :  0.60930E+01 0.96778E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1042
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.19624E+07   10000   0.99661E+00   0.83408E+06 
c  VelocityY    0.19624E+07   10000   0.99661E+00   0.00000E+00 
c  VelocityZ    0.19624E+07   10000   0.99661E+00   0.00000E+00 
c  Pressure     0.39067E+03     604   0.74717E-02   0.16504E+00 
c  k            0.99199E+09     235   0.21615E-03   0.57682E+10 
c  epsilon      0.40758E+16     173   0.38165E-04   0.28152E+23 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -25028           13060          4.8456         -12.173
v  Velocity[Y]                  -55576      1.0991e+05          74.216          10.075
v  Velocity[Z]                  -16035           37798         0.78375         -4.0815
v  ǁVelocityǁ                   1.9341      1.1229e+05          342.28          234.35
v  Pressure                -5.2306e+06      1.0972e+07      1.6187e+06      1.1112e+06
v  k                         0.0004123      7.5887e+06           36723           21140
v  epsilon                      16.027      2.9018e+13      2.7389e+10      1.3223e+10
v  turbulent_viscosity      3.9631e-08          386.67          9.7995          6.0719
v  CourantNb                     23.76      2.1654e+08      1.3061e+05           65486
v  FourierNb                    8.5922      7.1985e+05           15425          6853.5
v  total_pressure          -4.7306e+06      1.1472e+07      2.1187e+06      1.6112e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          179.56      2.1726e+08      1.4603e+05           72340


 TIME FOR THE TIME STEP              160:        0.14771E+02

===============================================================


 INSTANT    0.161000000E+02   TIME STEP NUMBER             161
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.170119433E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.272538106E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20131E+04 0.93780E+05
   Friction velocity        uet   :  0.59459E-01 0.55070E+04
   Friction velocity        uk    :  0.57507E+00 0.11400E+04
   Dimensionless distance   yplus :  0.22424E+01 0.10030E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        639
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.37076E+07    8513   0.10075E+01   0.40740E+06 
c  VelocityY    0.37076E+07    8513   0.10075E+01   0.00000E+00 
c  VelocityZ    0.37076E+07    8513   0.10075E+01   0.00000E+00 
c  Pressure     0.41556E+03     672   0.97419E-02   0.16227E+00 
c  k            0.13049E+10     242   0.20337E-03   0.72577E+10 
c  epsilon      0.59873E+16     173   0.37544E-04   0.31524E+23 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon     -2.8113e+06                             1


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -31676           12252         -35.945         -12.103
v  Velocity[Y]                  -57314      1.2658e+05          3.6582         -3.0288
v  Velocity[Z]                  -17797           40762          13.392         -3.2733
v  ǁVelocityǁ                   1.1821      1.2897e+05          341.01          254.97
v  Pressure                -5.4984e+06      1.2158e+07      1.8911e+06      1.3087e+06
v  k                         0.0037757      7.7524e+06           43468           24006
v  epsilon                      16.743      3.2115e+13      3.4542e+10      1.6304e+10
v  turbulent_viscosity      1.6827e-07           294.9          13.261           8.748
v  CourantNb                    10.544      2.4329e+08      1.1284e+05           53468
v  FourierNb                    11.173      9.0156e+05           20854          9367.5
v  total_pressure          -4.9984e+06      1.2658e+07      2.3911e+06      1.8087e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          130.86      2.4416e+08      1.3369e+05           62836


 TIME FOR THE TIME STEP              161:        0.12662E+02

===============================================================


 INSTANT    0.162000000E+02   TIME STEP NUMBER             162
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.907367416E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274125004E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10564E+04 0.10755E+06
   Friction velocity        uet   :  0.14125E-01 0.63140E+04
   Friction velocity        uk    :  0.80136E+00 0.11201E+04
   Dimensionless distance   yplus :  0.56355E+01 0.11168E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        321
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         23 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.18014E+07   10000   0.99337E+00   0.33189E+06 
c  VelocityY    0.18014E+07   10000   0.99337E+00   0.00000E+00 
c  VelocityZ    0.18014E+07   10000   0.99337E+00   0.00000E+00 
c  Pressure     0.45506E+03     529   0.70957E-02   0.16389E+00 
c  k            0.16508E+10     242   0.20078E-03   0.84416E+10 
c  epsilon      0.83065E+16     178   0.35444E-04   0.89745E+23 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -32095           14897         -19.642         -12.718
v  Velocity[Y]                  -64977      1.3088e+05          32.794          9.8328
v  Velocity[Z]                  -18435           45126         -1.8563         -6.3277
v  ǁVelocityǁ                   1.0946      1.3402e+05          276.35          181.21
v  Pressure                -6.3658e+06      1.3004e+07      1.9099e+06      1.3168e+06
v  k                          0.074981      1.1856e+07           47528           27327
v  epsilon                      82.202      5.1248e+13      4.3435e+10       2.047e+10
v  turbulent_viscosity      8.9609e-08          318.82          15.854          9.1414
v  CourantNb                    1.7619       2.621e+08      1.1387e+05           56958
v  FourierNb                    7.7171      9.6868e+05           26349           10742
v  total_pressure          -5.8658e+06      1.3504e+07      2.4099e+06      1.8168e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          194.29      2.6305e+08      1.4022e+05           67700


 TIME FOR THE TIME STEP              162:        0.14729E+02

===============================================================


 INSTANT    0.163000000E+02   TIME STEP NUMBER             163
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.487633306E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.272311112E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16435E+04 0.11400E+06
   Friction velocity        uet   :  0.41113E-01 0.64412E+04
   Friction velocity        uk    :  0.49696E+00 0.13804E+04
   Dimensionless distance   yplus :  0.26546E+01 0.11521E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        284
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.54063E+07    9242   0.99822E+00   0.18386E+07 
c  VelocityY    0.54063E+07    9242   0.99822E+00   0.00000E+00 
c  VelocityZ    0.54063E+07    9242   0.99822E+00   0.00000E+00 
c  Pressure     0.49919E+03     659   0.10675E-01   0.16582E+00 
c  k            0.21625E+10     319   0.19631E-03   0.22808E+11 
c  epsilon      0.12298E+17     183   0.33909E-04   0.14155E+24 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -37074           14743         -57.376         -13.296
v  Velocity[Y]                  -68869      1.5113e+05          69.683         -1.9199
v  Velocity[Z]                  -16953           53004          31.979         -3.3302
v  ǁVelocityǁ                   1.9069      1.5509e+05          613.93          432.95
v  Pressure                 -6.667e+06      1.4464e+07      2.1825e+06      1.5089e+06
v  k                          0.090551      1.2765e+07           63457           35867
v  epsilon                      495.84      6.1572e+13      6.0583e+10      2.8864e+10
v  turbulent_viscosity      5.8357e-05          341.64          16.639          10.531
v  CourantNb                    61.371      2.9049e+08      1.0599e+05           47498
v  FourierNb                    7.0646        1.09e+06           26550           11609
v  total_pressure           -6.167e+06      1.4964e+07      2.6825e+06      2.0089e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          197.27      2.9158e+08      1.3254e+05           59107


 TIME FOR THE TIME STEP              163:        0.13669E+02

===============================================================


 INSTANT    0.164000000E+02   TIME STEP NUMBER             164
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.745315482E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274196480E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64678E+03 0.12931E+06
   Friction velocity        uet   :  0.12644E+00 0.74123E+04
   Friction velocity        uk    :  0.74300E+00 0.17033E+04
   Dimensionless distance   yplus :  0.76074E+01 0.12162E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         69
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.27458E+07   10000   0.99394E+00   0.20142E+07 
c  VelocityY    0.27458E+07   10000   0.99394E+00   0.00000E+00 
c  VelocityZ    0.27458E+07   10000   0.99394E+00   0.00000E+00 
c  Pressure     0.54189E+03     530   0.72561E-02   0.16590E+00 
c  k            0.27523E+10     246   0.17691E-03   0.31063E+11 
c  epsilon      0.17414E+17     179   0.27788E-04   0.28185E+24 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k               -3.2613                             1
a  epsilon     -2.4539e+07                             2


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -38119           18167         -23.373         -16.877
v  Velocity[Y]                  -78195      1.5726e+05          60.215          10.451
v  Velocity[Z]                  -26011           53628          7.8605         -4.0513
v  ǁVelocityǁ                   1.3923      1.6052e+05          382.54          257.09
v  Pressure                  -7.73e+06      1.5463e+07      2.1989e+06      1.5215e+06
v  k                         0.0087668      1.2568e+07           64728           37365
v  epsilon                      2391.3      6.7949e+13      7.3165e+10      3.3365e+10
v  turbulent_viscosity      3.1781e-05          946.76          14.127          9.3692
v  CourantNb                    16.218      3.1211e+08      1.8057e+05           90499
v  FourierNb                    15.114      1.1681e+06           21867           10034
v  total_pressure            -7.23e+06      1.5963e+07      2.6989e+06      2.0215e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          391.59      3.1327e+08      2.0244e+05      1.0053e+05


 TIME FOR THE TIME STEP              164:        0.14734E+02

===============================================================


 INSTANT    0.165000000E+02   TIME STEP NUMBER             165
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.234670559E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.272105924E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51419E+03 0.13906E+06
   Friction velocity        uet   :  0.11149E+00 0.76063E+04
   Friction velocity        uk    :  0.87228E+00 0.16566E+04
   Dimensionless distance   yplus :  0.51345E+01 0.12943E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        118
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.76153E+07    9152   0.10075E+01   0.99598E+06 
c  VelocityY    0.76153E+07    9152   0.10075E+01   0.00000E+00 
c  VelocityZ    0.76153E+07    9152   0.10075E+01   0.00000E+00 
c  Pressure     0.57943E+03     663   0.94238E-02   0.16384E+00 
c  k            0.38248E+10     246   0.16532E-03   0.31926E+11 
c  epsilon      0.26882E+17     179   0.26865E-04   0.43815E+24 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -45127           17367         -52.651         -13.786
v  Velocity[Y]                  -82374      1.8107e+05          64.131         -2.8652
v  Velocity[Z]                  -24619           59383          34.289          -1.436
v  ǁVelocityǁ                   5.5356      1.8469e+05          513.02          377.25
v  Pressure                -8.1486e+06       1.713e+07      2.5665e+06      1.7845e+06
v  k                         0.0061119      1.5896e+07           71449           40727
v  epsilon                      536.76      9.3684e+13      9.5007e+10      4.2723e+10
v  turbulent_viscosity        3.27e-08          384.72          15.858          10.922
v  CourantNb                     48.55      3.5077e+08      1.3661e+05           62820
v  FourierNb                      18.8      1.4648e+06           24347           11364
v  total_pressure          -7.6486e+06       1.763e+07      3.0665e+06      2.2845e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          135.12      3.5217e+08      1.6095e+05           74184


 TIME FOR THE TIME STEP              165:        0.13541E+02

===============================================================


 INSTANT    0.166000000E+02   TIME STEP NUMBER             166
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.671422303E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274599915E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25129E+04 0.15929E+06
   Friction velocity        uet   :  0.11001E+00 0.87116E+04
   Friction velocity        uk    :  0.80989E+00 0.16990E+04
   Dimensionless distance   yplus :  0.45181E+01 0.14067E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        585
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         27 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.36983E+07   10000   0.99676E+00   0.10383E+07 
c  VelocityY    0.36983E+07   10000   0.99676E+00   0.00000E+00 
c  VelocityZ    0.36983E+07   10000   0.99676E+00   0.00000E+00 
c  Pressure     0.64005E+03     571   0.74342E-02   0.16663E+00 
c  k            0.50661E+10     239   0.14803E-03   0.39373E+11 
c  epsilon      0.39851E+17     178   0.28048E-04   0.10223E+25 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -46071           21823         -6.3262         -19.462
v  Velocity[Y]                  -93830      1.8779e+05          32.941          14.595
v  Velocity[Z]                  -27082           64009          17.551         -3.1668
v  ǁVelocityǁ                   1.3427      1.9215e+05          465.79          294.85
v  Pressure                -9.4306e+06      1.8312e+07      2.5188e+06      1.7395e+06
v  k                          0.036618      2.6147e+07           86827           48390
v  epsilon                      378.99      1.6085e+14      1.2542e+11      5.5502e+10
v  turbulent_viscosity      3.8257e-08          411.61          15.048          9.7293
v  CourantNb                     111.7       3.769e+08      1.6721e+05           82235
v  FourierNb                    7.6005      1.5861e+06           23511           10602
v  total_pressure          -8.9306e+06      1.8812e+07      3.0188e+06      2.2395e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          214.03      3.7846e+08      1.9073e+05           92837


 TIME FOR THE TIME STEP              166:        0.14746E+02

===============================================================


 INSTANT    0.167000000E+02   TIME STEP NUMBER             167
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.556526076E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.272014285E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20503E+04 0.16761E+06
   Friction velocity        uet   :  0.63132E-01 0.89131E+04
   Friction velocity        uk    :  0.79510E+00 0.19896E+04
   Dimensionless distance   yplus :  0.54475E+01 0.14849E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        267
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.11073E+08    9361   0.10081E+01   0.28387E+07 
c  VelocityY    0.11073E+08    9361   0.10081E+01   0.00000E+00 
c  VelocityZ    0.11073E+08    9361   0.10081E+01   0.00000E+00 
c  Pressure     0.71313E+03     678   0.12396E-01   0.17060E+00 
c  k            0.67590E+10     407   0.12897E-03   0.72322E+11 
c  epsilon      0.60240E+17     214   0.24530E-04   0.13887E+25 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -52457           22346         -53.412         -16.624
v  Velocity[Y]                  -99114      2.1638e+05          53.887         -8.1361
v  Velocity[Z]                  -25380           75018          24.134         -5.8594
v  ǁVelocityǁ                   8.8103      2.2182e+05          871.67          616.88
v  Pressure                -9.5453e+06      2.0729e+07      2.9902e+06      2.0799e+06
v  k                           0.34531      3.0484e+07      1.1594e+05           66483
v  epsilon                      742.22      2.0911e+14      1.7286e+11      7.8451e+10
v  turbulent_viscosity      1.8398e-05             444          20.804          12.964
v  CourantNb                    114.78      4.1667e+08        1.66e+05           73369
v  FourierNb                    8.7914      1.7437e+06           33819           14385
v  total_pressure          -9.0453e+06      2.1229e+07      3.4902e+06      2.5799e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          332.26      4.1842e+08      1.9982e+05           87753


 TIME FOR THE TIME STEP              167:        0.13860E+02

===============================================================


 INSTANT    0.168000000E+02   TIME STEP NUMBER             168
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.536054533E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274812104E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30552E+03 0.18776E+06
   Friction velocity        uet   :  0.14711E+00 0.10246E+05
   Friction velocity        uk    :  0.10740E+01 0.23819E+04
   Dimensionless distance   yplus :  0.65412E+01 0.16693E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         25
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.51418E+07   10000   0.99372E+00   0.31814E+07 
c  VelocityY    0.51418E+07   10000   0.99372E+00   0.00000E+00 
c  VelocityZ    0.51418E+07   10000   0.99372E+00   0.00000E+00 
c  Pressure     0.76347E+03     545   0.72724E-02   0.16810E+00 
c  k            0.83852E+10     237   0.13577E-03   0.92402E+11 
c  epsilon      0.84888E+17     173   0.22885E-04   0.25722E+25 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -54864           26677         -44.379         -19.222
v  Velocity[Y]             -1.1194e+05      2.2498e+05          34.484          13.528
v  Velocity[Z]                  -36029           75509         -13.727          -4.166
v  ǁVelocityǁ                   1.5575       2.295e+05          504.51          335.21
v  Pressure                -1.1092e+07      2.2125e+07      2.9658e+06      2.0554e+06
v  k                            1.2829      3.1872e+07      1.1562e+05           64870
v  epsilon                      8188.2      2.4499e+14      2.0753e+11      8.9391e+10
v  turbulent_viscosity       0.0012824          465.78          19.711          13.647
v  CourantNb                    108.23      4.4724e+08      2.5599e+05      1.2709e+05
v  FourierNb                    29.265      1.7143e+06           30553           14055
v  total_pressure          -1.0592e+07      2.2625e+07      3.4658e+06      2.5554e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          366.49      4.4895e+08      2.8654e+05      1.4115e+05


 TIME FOR THE TIME STEP              168:        0.14736E+02

===============================================================


 INSTANT    0.169000000E+02   TIME STEP NUMBER             169
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.155338473E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.271964136E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34287E+03 0.20108E+06
   Friction velocity        uet   :  0.62010E-02 0.10523E+05
   Friction velocity        uk    :  0.14119E+01 0.24639E+04
   Dimensionless distance   yplus :  0.32983E+01 0.17647E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         91
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.15815E+08    9545   0.10066E+01   0.33279E+07 
c  VelocityY    0.15815E+08    9545   0.10066E+01   0.00000E+00 
c  VelocityZ    0.15815E+08    9545   0.10066E+01   0.00000E+00 
c  Pressure     0.82274E+03     689   0.10301E-01   0.16707E+00 
c  k            0.11462E+11     231   0.12796E-03   0.10984E+12 
c  epsilon      0.12563E+18     172   0.18944E-04   0.35559E+25 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -63990           24865         -64.384         -20.329
v  Velocity[Y]             -1.1889e+05      2.5884e+05          41.981         -15.374
v  Velocity[Z]                  -36201           85600           54.19          -1.028
v  ǁVelocityǁ                   7.8313      2.6408e+05          856.38          671.77
v  Pressure                -1.1474e+07      2.4724e+07      3.6096e+06      2.5195e+06
v  k                            2.1446      3.5159e+07      1.2428e+05           73103
v  epsilon                        2899      3.0336e+14      2.6242e+11       1.152e+11
v  turbulent_viscosity      1.6577e-05          1316.4          21.459          13.425
v  CourantNb                    74.664      5.0377e+08      1.8537e+05           83312
v  FourierNb                    19.559        2.15e+06           34538           14878
v  total_pressure          -1.0974e+07      2.5224e+07      4.1096e+06      3.0195e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          299.91      5.0584e+08      2.1991e+05           98191


 TIME FOR THE TIME STEP              169:        0.14105E+02

===============================================================


 INSTANT    0.170000000E+02   TIME STEP NUMBER             170
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.919189228E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274676723E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85804E+03 0.22858E+06
   Friction velocity        uet   :  0.17974E+00 0.12062E+05
   Friction velocity        uk    :  0.12526E+01 0.25936E+04
   Dimensionless distance   yplus :  0.10625E+02 0.18180E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        481
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.77808E+07   10000   0.99611E+00   0.35399E+07 
c  VelocityY    0.77808E+07   10000   0.99611E+00   0.00000E+00 
c  VelocityZ    0.77808E+07   10000   0.99611E+00   0.00000E+00 
c  Pressure     0.90685E+03     528   0.75709E-02   0.16941E+00 
c  k            0.14605E+11     258   0.13426E-03   0.20186E+12 
c  epsilon      0.17845E+18     172   0.26207E-04   0.99282E+25 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -65812           31131         -29.233         -29.664
v  Velocity[Y]             -1.3462e+05      2.6905e+05          71.298          12.235
v  Velocity[Z]                  -38986           91799          71.505         -3.1226
v  ǁVelocityǁ                    5.538       2.753e+05          785.36          558.73
v  Pressure                -1.3292e+07      2.6438e+07      3.5857e+06      2.5086e+06
v  k                            5.7376      5.9968e+07      1.6176e+05           91317
v  epsilon                  1.1653e+05       5.331e+14        3.48e+11      1.4829e+11
v  turbulent_viscosity      5.4542e-06          9188.4          18.748          13.605
v  CourantNb                    495.03      5.3906e+08      2.5961e+05      1.3522e+05
v  FourierNb                    9.8114      7.7344e+06           28164           13628
v  total_pressure          -1.2792e+07      2.6938e+07      4.0857e+06      3.0086e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          979.32       5.412e+08      2.8777e+05      1.4885e+05


 TIME FOR THE TIME STEP              170:        0.14774E+02

===============================================================


 INSTANT    0.171000000E+02   TIME STEP NUMBER             171
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.239056516E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.271748640E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76172E+03 0.24134E+06
   Friction velocity        uet   :  0.30762E+00 0.12390E+05
   Friction velocity        uk    :  0.17828E+01 0.29182E+04
   Dimensionless distance   yplus :  0.11817E+02 0.21276E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        203
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.22541E+08    9928   0.10080E+01   0.26611E+07 
c  VelocityY    0.22541E+08    9928   0.10080E+01   0.00000E+00 
c  VelocityZ    0.22541E+08    9928   0.10080E+01   0.00000E+00 
c  Pressure     0.96941E+03     663   0.94200E-02   0.16699E+00 
c  k            0.19637E+11     232   0.11155E-03   0.18534E+12 
c  epsilon      0.26578E+18     169   0.16334E-04   0.95301E+25 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -75951           32327          -88.65         -28.241
v  Velocity[Y]             -1.4086e+05      3.0995e+05         -28.633         -11.219
v  Velocity[Z]                  -40805      1.0281e+05          23.526         0.70136
v  ǁVelocityǁ                   6.1944      3.1694e+05          803.31          578.25
v  Pressure                -1.4121e+07      2.9177e+07      4.1833e+06      2.9384e+06
v  k                             1.453      6.5061e+07      1.6909e+05           92899
v  epsilon                       20832      6.3132e+14      4.3654e+11      1.8313e+11
v  turbulent_viscosity       0.0012003          566.48          31.618          21.042
v  CourantNb                    278.03      5.9776e+08      2.5687e+05      1.2341e+05
v  FourierNb                    34.928      2.4628e+06           49673           22309
v  total_pressure          -1.3621e+07      2.9677e+07      4.6833e+06      3.4384e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          720.16       6.002e+08      3.0654e+05      1.4572e+05


 TIME FOR THE TIME STEP              171:        0.14691E+02

===============================================================


 INSTANT    0.172000000E+02   TIME STEP NUMBER             172
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.240625877E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275119447E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74888E+03 0.27479E+06
   Friction velocity        uet   :  0.23865E+00 0.14234E+05
   Friction velocity        uk    :  0.74566E+00 0.31624E+04
   Dimensionless distance   yplus :  0.77129E+01 0.22163E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        132
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10990E+08   10000   0.99655E+00   0.28896E+07 
c  VelocityY    0.10990E+08   10000   0.99655E+00   0.00000E+00 
c  VelocityZ    0.10990E+08   10000   0.99655E+00   0.00000E+00 
c  Pressure     0.10675E+04     492   0.72507E-02   0.16911E+00 
c  k            0.24850E+11     233   0.11739E-03   0.22451E+12 
c  epsilon      0.37065E+18     171   0.21855E-04   0.20557E+26 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -79340           37453         -23.299         -32.272
v  Velocity[Y]             -1.6009e+05      3.2128e+05          46.839          15.392
v  Velocity[Z]                  -43715      1.1005e+05         -18.527         -9.1674
v  ǁVelocityǁ                   1.9851      3.2818e+05          723.49          462.74
v  Pressure                -1.6254e+07      3.1254e+07      4.1982e+06      2.9441e+06
v  k                           0.43863      7.2875e+07      1.9802e+05      1.0922e+05
v  epsilon                      1318.1      8.3348e+14      5.5862e+11      2.3454e+11
v  turbulent_viscosity      0.00096358          614.75           25.61           15.48
v  CourantNb                    248.79      6.5007e+08      2.6548e+05       1.267e+05
v  FourierNb                    14.237      2.5791e+06           41078           17671
v  total_pressure          -1.5754e+07      3.1754e+07      4.6982e+06      3.4441e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          702.38      6.5265e+08      3.0656e+05      1.4437e+05


 TIME FOR THE TIME STEP              172:        0.14643E+02

===============================================================


 INSTANT    0.173000000E+02   TIME STEP NUMBER             173
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.326206513E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.271307355E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35127E+03 0.29032E+06
   Friction velocity        uet   :  0.61687E-01 0.14579E+05
   Friction velocity        uk    :  0.57129E+00 0.34087E+04
   Dimensionless distance   yplus :  0.32689E+01 0.25083E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        265
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.32141E+08   10000   0.99942E+00   0.47568E+07 
c  VelocityY    0.32141E+08   10000   0.99942E+00   0.00000E+00 
c  VelocityZ    0.32141E+08   10000   0.99942E+00   0.00000E+00 
c  Pressure     0.11768E+04     709   0.12789E-01   0.17152E+00 
c  k            0.33336E+11     240   0.12102E-03   0.44621E+12 
c  epsilon      0.54497E+18     168   0.14125E-04   0.29429E+26 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -87020           42015         -62.618          -29.03
v  Velocity[Y]             -1.6874e+05      3.6997e+05         -12.176         -28.049
v  Velocity[Z]                  -50242      1.2394e+05          29.273         -3.2529
v  ǁVelocityǁ                   9.0143      3.7777e+05            1235           906.3
v  Pressure                -1.6159e+07      3.5652e+07      5.4717e+06      3.8564e+06
v  k                           0.10082      7.4909e+07      2.2908e+05      1.3391e+05
v  epsilon                      3263.4      9.3493e+14      7.3843e+11      3.1415e+11
v  turbulent_viscosity      0.00087893          660.77          30.646          17.989
v  CourantNb                    5.5374      7.1648e+08      2.6187e+05      1.1497e+05
v  FourierNb                    13.608      2.8469e+06           50041           20945
v  total_pressure          -1.5659e+07      3.6152e+07      5.9717e+06      4.3564e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          24.298      7.1932e+08      3.1191e+05      1.3592e+05


 TIME FOR THE TIME STEP              173:        0.14803E+02

===============================================================


 INSTANT    0.174000000E+02   TIME STEP NUMBER             174
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.516706986E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275902917E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25589E+04 0.32905E+06
   Friction velocity        uet   :  0.15539E+00 0.16765E+05
   Friction velocity        uk    :  0.15034E+01 0.37313E+04
   Dimensionless distance   yplus :  0.11065E+02 0.26150E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         70
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         26 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.16521E+08   10000   0.99612E+00   0.43673E+07 
c  VelocityY    0.16521E+08   10000   0.99612E+00   0.00000E+00 
c  VelocityZ    0.16521E+08   10000   0.99612E+00   0.00000E+00 
c  Pressure     0.12756E+04     515   0.74932E-02   0.17101E+00 
c  k            0.41981E+11     235   0.12903E-03   0.74335E+12 
c  epsilon      0.75926E+18     171   0.22540E-04   0.70488E+26 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -92983           45878         -92.622         -26.782
v  Velocity[Y]             -1.9076e+05      3.8506e+05          86.043          10.586
v  Velocity[Z]                  -62629       1.293e+05         -50.807         -10.946
v  ǁVelocityǁ                   6.8521      3.9365e+05          769.01          510.98
v  Pressure                -1.8754e+07      3.8096e+07      5.4445e+06      3.8364e+06
v  k                           0.21914      1.1343e+08      2.7747e+05      1.5284e+05
v  epsilon                       14508       1.452e+15      9.4997e+11      3.8842e+11
v  turbulent_viscosity      4.6919e-07          738.51           26.94           18.37
v  CourantNb                    174.72      7.7808e+08      3.7579e+05      1.8521e+05
v  FourierNb                    17.271      3.0259e+06           40839           19286
v  total_pressure          -1.8254e+07      3.8596e+07      5.9445e+06      4.3364e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          764.18       7.811e+08      4.1662e+05       2.045e+05


 TIME FOR THE TIME STEP              174:        0.14651E+02

===============================================================


 INSTANT    0.175000000E+02   TIME STEP NUMBER             175
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.529014563E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.270429512E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57670E+03 0.35109E+06
   Friction velocity        uet   :  0.10787E+00 0.17238E+05
   Friction velocity        uk    :  0.92328E+00 0.38321E+04
   Dimensionless distance   yplus :  0.12552E+02 0.32549E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         51
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.46337E+08   10000   0.10077E+01   0.10050E+08 
c  VelocityY    0.46337E+08   10000   0.10077E+01   0.00000E+00 
c  VelocityZ    0.46337E+08   10000   0.10077E+01   0.00000E+00 
c  Pressure     0.14214E+04     698   0.14412E-01   0.17471E+00 
c  k            0.57275E+11     439   0.98224E-04   0.12877E+13 
c  epsilon      0.11161E+19     211   0.19103E-04   0.99989E+26 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0904e+05           46134         -30.348         -26.793
v  Velocity[Y]             -2.0364e+05      4.4083e+05         -216.25         -35.601
v  Velocity[Z]                  -50546      1.4831e+05          20.899         0.36701
v  ǁVelocityǁ                    4.774      4.5094e+05          2186.9          1521.2
v  Pressure                -1.8402e+07      4.3584e+07      6.7977e+06      4.8209e+06
v  k                          0.059795      1.2398e+08      3.9111e+05      2.1472e+05
v  epsilon                      4508.5      1.8431e+15        1.27e+12      5.4236e+11
v  turbulent_viscosity      1.1331e-05          835.65          37.038          22.588
v  CourantNb                    78.549      8.6425e+08      2.8991e+05       1.267e+05
v  FourierNb                    15.872      3.6153e+06           59057           25662
v  total_pressure          -1.7902e+07      4.4084e+07      7.2977e+06      5.3209e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          777.33      8.6786e+08      3.4897e+05      1.5236e+05


 TIME FOR THE TIME STEP              175:        0.14840E+02

===============================================================


 INSTANT    0.176000000E+02   TIME STEP NUMBER             176
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.146459078E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275977327E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16785E+04 0.39533E+06
   Friction velocity        uet   :  0.44800E+00 0.19671E+05
   Friction velocity        uk    :  0.13783E+01 0.47326E+04
   Dimensionless distance   yplus :  0.13017E+02 0.35188E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        167
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.25680E+08   10000   0.10003E+01   0.10935E+08 
c  VelocityY    0.25680E+08   10000   0.10003E+01   0.00000E+00 
c  VelocityZ    0.25680E+08   10000   0.10003E+01   0.00000E+00 
c  Pressure     0.15204E+04     500   0.68248E-02   0.17187E+00 
c  k            0.70831E+11     236   0.11978E-03   0.12546E+13 
c  epsilon      0.15365E+19     172   0.22819E-04   0.21680E+27 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k               -19.933                             2
a  epsilon      -1.851e+07                             3


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1202e+05           52943         -72.787         -27.883
v  Velocity[Y]             -2.2956e+05      4.5998e+05           106.9          6.1733
v  Velocity[Z]                  -62321      1.5679e+05          30.584         -8.4358
v  ǁVelocityǁ                   2.9195      4.6977e+05          939.35          596.47
v  Pressure                -2.1551e+07      4.6478e+07      6.7771e+06      4.7967e+06
v  k                         0.0042117      1.7979e+08      4.0153e+05      2.1898e+05
v  epsilon                      112.83      2.6824e+15       1.598e+12      6.6275e+11
v  turbulent_viscosity      1.1746e-07             855          45.171          27.598
v  CourantNb                    539.25      9.2574e+08      6.0761e+05      3.0091e+05
v  FourierNb                    15.959      3.5103e+06           73307           31047
v  total_pressure          -2.1051e+07      4.6978e+07      7.2771e+06      5.2967e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          710.39      9.2925e+08      6.8092e+05      3.3195e+05


 TIME FOR THE TIME STEP              176:        0.14645E+02

===============================================================


 INSTANT    0.177000000E+02   TIME STEP NUMBER             177
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.103022146E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.270363847E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30597E+04 0.42125E+06
   Friction velocity        uet   :  0.19505E+00 0.20283E+05
   Friction velocity        uk    :  0.91672E+00 0.53563E+04
   Dimensionless distance   yplus :  0.57239E+01 0.37539E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        273
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.65107E+08    9730   0.10061E+01   0.90484E+07 
c  VelocityY    0.65107E+08    9730   0.10061E+01   0.00000E+00 
c  VelocityZ    0.65107E+08    9730   0.10061E+01   0.00000E+00 
c  Pressure     0.16320E+04     697   0.11119E-01   0.16975E+00 
c  k            0.96807E+11     239   0.99711E-04   0.13758E+13 
c  epsilon      0.22655E+19     171   0.16322E-04   0.25727E+27 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.3124e+05           55522         -91.563         -25.699
v  Velocity[Y]             -2.4113e+05      5.2832e+05          19.164         -46.283
v  Velocity[Z]                  -70468      1.7415e+05          74.124         -9.8626
v  ǁVelocityǁ                   14.309      5.3905e+05            1476          1116.5
v  Pressure                -2.2111e+07      5.2021e+07      8.3761e+06      5.9398e+06
v  k                           0.66292      2.1032e+08      3.9181e+05      2.2283e+05
v  epsilon                      7087.6      3.4376e+15      1.9953e+12       8.192e+11
v  turbulent_viscosity      1.0218e-05          954.42          50.966            30.3
v  CourantNb                    39.988      1.0297e+09      3.5147e+05      1.5084e+05
v  FourierNb                    14.816      4.1386e+06           83371           34868
v  total_pressure          -2.1611e+07      5.2521e+07      8.8761e+06      6.4398e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          422.73      1.0338e+09      4.3484e+05      1.8571e+05


 TIME FOR THE TIME STEP              177:        0.14435E+02

===============================================================


 INSTANT    0.178000000E+02   TIME STEP NUMBER             178
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.243240145E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.276608520E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58493E+04 0.47897E+06
   Friction velocity        uet   :  0.16916E+00 0.23243E+05
   Friction velocity        uk    :  0.12949E+01 0.52985E+04
   Dimensionless distance   yplus :  0.98840E+01 0.38308E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        386
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30053E+08   10000   0.99097E+00   0.10411E+08 
c  VelocityY    0.30053E+08   10000   0.99097E+00   0.00000E+00 
c  VelocityZ    0.30053E+08   10000   0.99097E+00   0.00000E+00 
c  Pressure     0.17973E+04     462   0.70859E-02   0.17181E+00 
c  k            0.12295E+12     237   0.11293E-03   0.19538E+13 
c  epsilon      0.31630E+19     173   0.26753E-04   0.62516E+27 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.3549e+05           63658         -108.44         -29.091
v  Velocity[Y]             -2.7299e+05      5.4711e+05          166.81         -2.3542
v  Velocity[Z]                  -83374      1.8776e+05         -63.905         -15.672
v  ǁVelocityǁ                   3.2524      5.5998e+05          1248.2          784.25
v  Pressure                -2.5798e+07       5.552e+07       8.396e+06      5.9557e+06
v  k                           0.88843      2.7523e+08      4.6757e+05      2.6129e+05
v  epsilon                       21444      4.9504e+15       2.639e+12      1.0552e+12
v  turbulent_viscosity       0.0010175          1019.1          31.343          21.679
v  CourantNb                    395.38      1.1119e+09      4.6837e+05      2.2904e+05
v  FourierNb                    10.579      4.5742e+06           47646           22498
v  total_pressure          -2.5298e+07       5.602e+07       8.896e+06      6.4557e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          793.17      1.1164e+09      5.1602e+05      2.5154e+05


 TIME FOR THE TIME STEP              178:        0.14635E+02

===============================================================


 INSTANT    0.179000000E+02   TIME STEP NUMBER             179
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.206259526E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.269108755E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50984E+04 0.50622E+06
   Friction velocity        uet   :  0.64347E-01 0.23779E+05
   Friction velocity        uk    :  0.12485E+01 0.58539E+04
   Dimensionless distance   yplus :  0.84450E+01 0.43186E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        332
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.92825E+08   10000   0.10067E+01   0.91991E+07 
c  VelocityY    0.92825E+08   10000   0.10067E+01   0.00000E+00 
c  VelocityZ    0.92825E+08   10000   0.10067E+01   0.00000E+00 
c  Pressure     0.19584E+04     696   0.11893E-01   0.17182E+00 
c  k            0.16965E+12     252   0.72087E-04   0.24977E+13 
c  epsilon      0.47178E+19     171   0.19804E-04   0.77135E+27 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.5795e+05           63304         -26.567         -31.011
v  Velocity[Y]             -2.8979e+05      6.2929e+05         -415.64         -55.381
v  Velocity[Z]                  -94271       2.062e+05          152.58        -0.57333
v  ǁVelocityǁ                   11.532      6.4269e+05          1846.9          1339.7
v  Pressure                -2.6286e+07      6.2342e+07      1.0118e+07      7.1941e+06
v  k                            90.023      3.0311e+08      6.3833e+05      3.3724e+05
v  epsilon                  1.3095e+05      6.2103e+15      3.5648e+12        1.44e+12
v  turbulent_viscosity      0.00090459          1211.9          38.516          26.341
v  CourantNb                    416.19      1.2312e+09      4.4817e+05       1.924e+05
v  FourierNb                    10.083      5.2271e+06           58908           27543
v  total_pressure          -2.5786e+07      6.2842e+07      1.0618e+07      7.6941e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            1231      1.2363e+09      5.0708e+05      2.1994e+05


 TIME FOR THE TIME STEP              179:        0.14808E+02

===============================================================


 INSTANT    0.180000000E+02   TIME STEP NUMBER             180
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.154507050E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.276858980E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36927E+03 0.57609E+06
   Friction velocity        uet   :  0.26147E+00 0.27273E+05
   Friction velocity        uk    :  0.51968E+01 0.63350E+04
   Dimensionless distance   yplus :  0.11962E+02 0.45064E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          7
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         41 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.42674E+08   10000   0.99979E+00   0.69324E+07 
c  VelocityY    0.42674E+08   10000   0.99979E+00   0.00000E+00 
c  VelocityZ    0.42674E+08   10000   0.99979E+00   0.00000E+00 
c  Pressure     0.21492E+04     606   0.73697E-02   0.17328E+00 
c  k            0.21494E+12     237   0.98873E-04   0.32988E+13 
c  epsilon      0.65871E+19     173   0.24128E-04   0.16978E+28 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k                -159.1                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6371e+05           75307         -230.15         -33.848
v  Velocity[Y]             -3.2748e+05       6.554e+05          102.45          11.331
v  Velocity[Z]                  -88372       2.244e+05         -84.115         -4.3553
v  ǁVelocityǁ                    2.204      6.6944e+05          1394.5          917.31
v  Pressure                -3.1251e+07       6.597e+07      9.7561e+06      6.9217e+06
v  k                            2.7423      3.8931e+08      7.0849e+05      3.7266e+05
v  epsilon                       36453      8.7003e+15      4.4624e+12      1.7721e+12
v  turbulent_viscosity        0.051599          1171.7          57.918           33.52
v  CourantNb                    534.26      1.3382e+09      5.7861e+05      2.7721e+05
v  FourierNb                    73.523      5.4901e+06           96444           39144
v  total_pressure          -3.0751e+07       6.647e+07      1.0256e+07      7.4217e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1256.2      1.3436e+09      6.7505e+05      3.1635e+05


 TIME FOR THE TIME STEP              180:        0.14706E+02

===============================================================


 INSTANT    0.181000000E+02   TIME STEP NUMBER             181
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.961198957E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.269429054E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56316E+04 0.60991E+06
   Friction velocity        uet   :  0.45280E+00 0.28084E+05
   Friction velocity        uk    :  0.19785E+01 0.71060E+04
   Dimensionless distance   yplus :  0.11547E+02 0.51776E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        135
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.13496E+09   10000   0.10073E+01   0.16236E+08 
c  VelocityY    0.13496E+09   10000   0.10073E+01   0.00000E+00 
c  VelocityZ    0.13496E+09   10000   0.10073E+01   0.00000E+00 
c  Pressure     0.23799E+04     660   0.11698E-01   0.17558E+00 
c  k            0.28742E+12     238   0.75563E-04   0.52778E+13 
c  epsilon      0.96455E+19     172   0.15851E-04   0.25023E+28 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.896e+05           70759         -73.487         -40.356
v  Velocity[Y]             -3.4735e+05      7.5352e+05          271.77         -60.692
v  Velocity[Z]                  -94432      2.5593e+05           47.36         -1.3031
v  ǁVelocityǁ                   13.019      7.7032e+05          2002.4          1411.6
v  Pressure                -3.2873e+07      7.3127e+07       1.102e+07      7.8251e+06
v  k                            1.8886      4.3511e+08      7.2718e+05      4.1255e+05
v  epsilon                       31740      1.0642e+16      5.8064e+12      2.3787e+12
v  turbulent_viscosity      1.8391e-05          1379.7          73.281          41.144
v  CourantNb                    258.35       1.476e+09      5.0526e+05      2.1961e+05
v  FourierNb                    17.703      6.2225e+06      1.2351e+05           49130
v  total_pressure          -3.2373e+07      7.3627e+07       1.152e+07      8.3251e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1450.6      1.4822e+09      6.2877e+05      2.6874e+05


 TIME FOR THE TIME STEP              181:        0.14787E+02

===============================================================


 INSTANT    0.182000000E+02   TIME STEP NUMBER             182
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.192955462E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.277373825E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64879E+04 0.69409E+06
   Friction velocity        uet   :  0.14622E+00 0.32183E+05
   Friction velocity        uk    :  0.82541E+00 0.80427E+04
   Dimensionless distance   yplus :  0.10845E+02 0.56366E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        158
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         35 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.59809E+08   10000   0.99164E+00   0.21295E+08 
c  VelocityY    0.59809E+08   10000   0.99164E+00   0.00000E+00 
c  VelocityZ    0.59809E+08   10000   0.99164E+00   0.00000E+00 
c  Pressure     0.25684E+04     566   0.73640E-02   0.17407E+00 
c  k            0.36741E+12     236   0.11561E-03   0.99966E+13 
c  epsilon      0.13646E+20     173   0.27932E-04   0.65995E+28 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9198e+05           94758         -114.03           -41.5
v  Velocity[Y]             -3.9257e+05      7.8239e+05          196.44          3.0687
v  Velocity[Z]             -1.2697e+05      2.6677e+05         -112.43         -3.2106
v  ǁVelocityǁ                   6.3891      8.0035e+05          1611.5          1012.8
v  Pressure                -3.8696e+07      7.7579e+07      1.0796e+07      7.6493e+06
v  k                            1.5101      5.5839e+08      8.5107e+05      4.6011e+05
v  epsilon                  3.2978e+05      1.4917e+16      7.7458e+12      2.9938e+12
v  turbulent_viscosity       0.0002982            1409          41.778          29.153
v  CourantNb                    153.02      1.5853e+09      6.4236e+05      3.0013e+05
v  FourierNb                    10.619      6.3251e+06           63401           30048
v  total_pressure          -3.8196e+07      7.8079e+07      1.1296e+07      8.1493e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1461.5      1.5916e+09      7.0576e+05      3.3018e+05


 TIME FOR THE TIME STEP              182:        0.14674E+02

===============================================================


 INSTANT    0.183000000E+02   TIME STEP NUMBER             183
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.230478952E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.269097899E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22751E+04 0.73203E+06
   Friction velocity        uet   :  0.24382E+00 0.33071E+05
   Friction velocity        uk    :  0.15507E+01 0.85015E+04
   Dimensionless distance   yplus :  0.91789E+01 0.62828E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        143
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.19333E+09   10000   0.10097E+01   0.26576E+08 
c  VelocityY    0.19333E+09   10000   0.10097E+01   0.00000E+00 
c  VelocityZ    0.19333E+09   10000   0.10097E+01   0.00000E+00 
c  Pressure     0.28198E+04     683   0.12263E-01   0.17516E+00 
c  k            0.50039E+12     305   0.68713E-04   0.10676E+14 
c  epsilon      0.20386E+20     169   0.11127E-04   0.65326E+28 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.2523e+05           87843         -141.94         -40.913
v  Velocity[Y]             -4.1779e+05      9.0156e+05         -443.73         -86.005
v  Velocity[Z]             -1.0942e+05      3.0124e+05          213.01          2.8386
v  ǁVelocityǁ                   29.711      9.2217e+05          2938.1          2105.6
v  Pressure                -3.9631e+07      8.7084e+07      1.2932e+07      9.1786e+06
v  k                            77.436      4.9285e+08      9.7996e+05      5.4692e+05
v  epsilon                  1.9546e+05      1.5151e+16      9.5837e+12      3.7891e+12
v  turbulent_viscosity      6.6566e-05          1655.5          57.197          35.534
v  CourantNb                    134.78      1.7753e+09      5.9578e+05      2.5138e+05
v  FourierNb                    10.714      7.8539e+06           91695           39638
v  total_pressure          -3.9131e+07      8.7584e+07      1.3432e+07      9.6786e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          699.35      1.7827e+09      6.8747e+05      2.9101e+05


 TIME FOR THE TIME STEP              183:        0.14801E+02

===============================================================


 INSTANT    0.184000000E+02   TIME STEP NUMBER             184
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.369831955E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.280364671E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59534E+04 0.83112E+06
   Friction velocity        uet   :  0.67397E+00 0.38021E+05
   Friction velocity        uk    :  0.48203E+01 0.95289E+04
   Dimensionless distance   yplus :  0.17320E+02 0.66782E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         15
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.93354E+08   10000   0.99523E+00   0.27567E+08 
c  VelocityY    0.93354E+08   10000   0.99523E+00   0.00000E+00 
c  VelocityZ    0.93354E+08   10000   0.99523E+00   0.00000E+00 
c  Pressure     0.30639E+04     587   0.75716E-02   0.17464E+00 
c  k            0.62144E+12     231   0.92229E-04   0.17818E+14 
c  epsilon      0.28380E+20     169   0.21705E-04   0.17065E+29 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.2885e+05      1.1178e+05         -115.56         -56.168
v  Velocity[Y]             -4.6909e+05      9.3844e+05          188.02         -10.998
v  Velocity[Z]             -1.2421e+05      3.2399e+05          3.3807         -8.7239
v  ǁVelocityǁ                   7.9612      9.5926e+05            2280          1562.1
v  Pressure                -4.6218e+07      9.2857e+07      1.2568e+07       8.915e+06
v  k                            16.502       7.003e+08      1.1992e+06      6.5836e+05
v  epsilon                  4.3614e+05      2.3211e+16      1.2547e+13      4.9067e+12
v  turbulent_viscosity       0.0066115          2289.7          59.782          41.852
v  CourantNb                     418.2      1.9076e+09      8.8459e+05      4.2613e+05
v  FourierNb                    149.22      7.5833e+06           92241           42760
v  total_pressure          -4.5718e+07      9.3357e+07      1.3068e+07       9.415e+06


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          770.79      1.9152e+09      9.7683e+05      4.6889e+05


 TIME FOR THE TIME STEP              184:        0.14761E+02

===============================================================


 INSTANT    0.185000000E+02   TIME STEP NUMBER             185
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.196580694E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.265284991E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20664E+04 0.87699E+06
   Friction velocity        uet   :  0.44708E+00 0.39167E+05
   Friction velocity        uk    :  0.42573E+01 0.10502E+05
   Dimensionless distance   yplus :  0.85874E+01 0.73605E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         19
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         39 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.27175E+09   10000   0.10065E+01   0.34392E+08 
c  VelocityY    0.27175E+09   10000   0.10065E+01   0.00000E+00 
c  VelocityZ    0.27175E+09   10000   0.10065E+01   0.00000E+00 
c  Pressure     0.32877E+04     662   0.10937E-01   0.17204E+00 
c  k            0.83636E+12     232   0.63933E-04   0.16066E+14 
c  epsilon      0.41759E+20     168   0.12570E-04   0.18604E+29 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6486e+05       1.126e+05         -215.73         -66.717
v  Velocity[Y]             -4.9552e+05      1.0764e+06         -313.96         -82.621
v  Velocity[Z]             -1.5421e+05      3.4926e+05           105.9          4.2243
v  ǁVelocityǁ                   6.8754      1.0973e+06          3186.2          2108.8
v  Pressure                -4.8678e+07      1.0282e+08      1.4441e+07      1.0232e+07
v  k                            5.5257        7.35e+08      1.2913e+06       6.869e+05
v  epsilon                  1.5376e+06      2.6521e+16       1.614e+13      6.1602e+12
v  turbulent_viscosity      0.00015881          1673.4          91.089          59.457
v  CourantNb                    906.66      2.1136e+09      7.7411e+05      3.4718e+05
v  FourierNb                    122.31      8.5066e+06      1.4497e+05           63787
v  total_pressure          -4.8178e+07      1.0332e+08      1.4941e+07      1.0732e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2427.7      2.1221e+09      9.1908e+05      4.1097e+05


 TIME FOR THE TIME STEP              185:        0.14707E+02

===============================================================


 INSTANT    0.186000000E+02   TIME STEP NUMBER             186
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.183271777E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.279599802E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.90406E+03 0.10011E+07
   Friction velocity        uet   :  0.19851E+00 0.44805E+05
   Friction velocity        uk    :  0.20306E+01 0.10978E+05
   Dimensionless distance   yplus :  0.10042E+02 0.76936E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         38
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         40 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.13413E+09   10000   0.99787E+00   0.36544E+08 
c  VelocityY    0.13413E+09   10000   0.99787E+00   0.00000E+00 
c  VelocityZ    0.13413E+09   10000   0.99787E+00   0.00000E+00 
c  Pressure     0.36260E+04     593   0.75317E-02   0.17425E+00 
c  k            0.10785E+13     230   0.80898E-04   0.20358E+14 
c  epsilon      0.58374E+20     170   0.19894E-04   0.38564E+29 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7629e+05      1.3291e+05         -290.89         -77.878
v  Velocity[Y]             -5.5862e+05      1.1166e+06          60.571          5.4373
v  Velocity[Z]             -1.7043e+05      3.7967e+05         -22.674         -13.348
v  ǁVelocityǁ                   14.455      1.1452e+06          2281.8          1580.1
v  Pressure                -5.7012e+07      1.0918e+08      1.3894e+07      9.8402e+06
v  k                            6.0424      9.6058e+08      1.5236e+06      7.8379e+05
v  epsilon                  2.4142e+05      3.8274e+16      2.0898e+13        7.95e+12
v  turbulent_viscosity      0.00077639          1613.3          72.718          46.173
v  CourantNb                    233.96      2.3063e+09      1.0023e+06       4.537e+05
v  FourierNb                    28.463      9.4591e+06      1.1676e+05           50468
v  total_pressure          -5.6512e+07      1.0968e+08      1.4394e+07       1.034e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          364.82      2.3156e+09       1.119e+06      5.0417e+05


 TIME FOR THE TIME STEP              186:        0.14757E+02

===============================================================


 INSTANT    0.187000000E+02   TIME STEP NUMBER             187
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.780507776E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.264090949E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14977E+04 0.10517E+07
   Friction velocity        uet   :  0.35255E+00 0.46001E+05
   Friction velocity        uk    :  0.15566E+01 0.11597E+05
   Dimensionless distance   yplus :  0.19374E+02 0.88134E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        176
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.39305E+09   10000   0.10074E+01   0.72135E+08 
c  VelocityY    0.39305E+09   10000   0.10074E+01   0.00000E+00 
c  VelocityZ    0.39305E+09   10000   0.10074E+01   0.00000E+00 
c  Pressure     0.40806E+04     678   0.13994E-01   0.17892E+00 
c  k            0.14234E+13     249   0.57725E-04   0.36456E+14 
c  epsilon      0.84537E+20     167   0.13910E-04   0.58479E+29 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.2358e+05      1.2348e+05         -133.13         -68.166
v  Velocity[Y]             -5.9734e+05      1.2831e+06         -116.88         -121.28
v  Velocity[Z]             -1.9069e+05      4.3005e+05          137.75          7.6045
v  ǁVelocityǁ                   14.946      1.3128e+06          4180.4          2910.5
v  Pressure                -5.8185e+07       1.229e+08      1.6425e+07      1.1644e+07
v  k                            13.443       1.187e+09      1.6934e+06      9.4273e+05
v  epsilon                   1.076e+05      5.0434e+16      2.7262e+13      1.0623e+13
v  turbulent_viscosity       0.0028303          1909.3          91.617          50.722
v  CourantNb                    42.583      2.5374e+09      8.2828e+05      3.6247e+05
v  FourierNb                    12.318      1.0295e+07      1.5417e+05           61303
v  total_pressure          -5.7685e+07       1.234e+08      1.6925e+07      1.2144e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          513.51      2.5476e+09      9.8245e+05      4.2377e+05


 TIME FOR THE TIME STEP              187:        0.14719E+02

===============================================================


 INSTANT    0.188000000E+02   TIME STEP NUMBER             188
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.383799766E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.282393865E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64789E+04 0.11963E+07
   Friction velocity        uet   :  0.23844E+00 0.52745E+05
   Friction velocity        uk    :  0.20082E+01 0.12568E+05
   Dimensionless distance   yplus :  0.15223E+02 0.92400E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         34
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         30 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.17474E+09   10000   0.99424E+00   0.82165E+08 
c  VelocityY    0.17474E+09   10000   0.99424E+00   0.00000E+00 
c  VelocityZ    0.17474E+09   10000   0.99424E+00   0.00000E+00 
c  Pressure     0.43848E+04     622   0.77693E-02   0.17672E+00 
c  k            0.17839E+13     238   0.11056E-03   0.84976E+14 
c  epsilon      0.11615E+21     172   0.27195E-04   0.17843E+30 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.3252e+05      1.5498e+05         -265.46         -82.186
v  Velocity[Y]             -6.6914e+05      1.3427e+06          86.725          1.5592
v  Velocity[Z]             -1.8819e+05      4.5953e+05         -95.536         -4.5905
v  ǁVelocityǁ                   19.401      1.3715e+06          2973.9          2014.9
v  Pressure                -6.8763e+07      1.2995e+08      1.5477e+07      1.0954e+07
v  k                           0.70031      1.8638e+09      2.0187e+06       1.056e+06
v  epsilon                  1.0194e+05      8.2495e+16      3.5383e+13      1.3364e+13
v  turbulent_viscosity        0.012817          2212.8          66.861          45.554
v  CourantNb                    568.87      2.7436e+09      1.2636e+06      5.9579e+05
v  FourierNb                    25.735      1.0536e+07      1.0266e+05           47732
v  total_pressure          -6.8263e+07      1.3045e+08      1.5977e+07      1.1454e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          754.06      2.7541e+09      1.3663e+06      6.4352e+05


 TIME FOR THE TIME STEP              188:        0.14771E+02

===============================================================


 INSTANT    0.189000000E+02   TIME STEP NUMBER             189
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.708294998E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.265612115E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36003E+04 0.12739E+07
   Friction velocity        uet   :  0.32234E+00 0.54555E+05
   Friction velocity        uk    :  0.17665E+01 0.14274E+05
   Dimensionless distance   yplus :  0.95311E+01 0.10763E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         28
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.56386E+09   10000   0.10062E+01   0.77690E+08 
c  VelocityY    0.56386E+09   10000   0.10062E+01   0.00000E+00 
c  VelocityZ    0.56386E+09   10000   0.10062E+01   0.00000E+00 
c  Pressure     0.48482E+04     679   0.12248E-01   0.17842E+00 
c  k            0.24678E+13     225   0.58465E-04   0.65264E+14 
c  epsilon      0.17307E+21     166   0.11455E-04   0.13681E+30 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.8455e+05      1.5571e+05         -32.603         -83.259
v  Velocity[Y]             -7.0853e+05      1.5398e+06         -578.27         -163.28
v  Velocity[Z]             -2.4759e+05       5.026e+05          64.414         -1.4894
v  ǁVelocityǁ                   23.576      1.5703e+06          4099.8          2949.1
v  Pressure                -7.0885e+07      1.4569e+08      1.8784e+07      1.3306e+07
v  k                            3.2996      1.4709e+09       2.425e+06      1.2404e+06
v  epsilon                  2.6956e+05      7.5449e+16      4.4639e+13      1.6778e+13
v  turbulent_viscosity      1.7971e-05          4301.7          90.798          56.254
v  CourantNb                    1445.4      3.0303e+09      1.0414e+06      4.5672e+05
v  FourierNb                    35.937      1.2386e+07      1.4646e+05           62727
v  total_pressure          -7.0385e+07      1.4619e+08      1.9284e+07      1.3806e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2389.9      3.0426e+09      1.1878e+06      5.1945e+05


 TIME FOR THE TIME STEP              189:        0.14708E+02

===============================================================


 INSTANT    0.190000000E+02   TIME STEP NUMBER             190
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.424287843E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.283593298E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13803E+05 0.14423E+07
   Friction velocity        uet   :  0.40301E+00 0.62507E+05
   Friction velocity        uk    :  0.23090E+01 0.14956E+05
   Dimensionless distance   yplus :  0.16808E+02 0.10490E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         82
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.24143E+09   10000   0.99782E+00   0.53936E+08 
c  VelocityY    0.24143E+09   10000   0.99782E+00   0.00000E+00 
c  VelocityZ    0.24143E+09   10000   0.99782E+00   0.00000E+00 
c  Pressure     0.51907E+04     574   0.68655E-02   0.17553E+00 
c  k            0.30354E+13     240   0.90635E-04   0.11838E+15 
c  epsilon      0.23674E+21     173   0.26169E-04   0.42991E+30 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.9342e+05       1.901e+05         -293.23         -78.937
v  Velocity[Y]             -8.0123e+05      1.5894e+06          -221.3         -102.64
v  Velocity[Z]             -2.4533e+05      5.5137e+05         -66.043          5.5129
v  ǁVelocityǁ                   5.1775      1.6273e+06          2888.1            1930
v  Pressure                -8.0412e+07      1.5717e+08       1.969e+07      1.3947e+07
v  k                            129.03      2.2157e+09      2.6534e+06      1.3422e+06
v  epsilon                  3.4737e+06      1.2358e+17       5.935e+13      2.1962e+13
v  turbulent_viscosity      0.00038334            2271          108.79          61.311
v  CourantNb                    373.66      3.2913e+09      1.2966e+06      6.0275e+05
v  FourierNb                     47.46      1.2978e+07      1.8324e+05           72971
v  total_pressure          -7.9912e+07      1.5767e+08       2.019e+07      1.4447e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            3342      3.3039e+09      1.4799e+06      6.7573e+05


 TIME FOR THE TIME STEP              190:        0.14759E+02

===============================================================


 INSTANT    0.191000000E+02   TIME STEP NUMBER             191
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.594433970E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.285665977E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97381E+03 0.15158E+07
   Friction velocity        uet   :  0.18874E+00 0.63798E+05
   Friction velocity        uk    :  0.62217E+01 0.15802E+05
   Dimensionless distance   yplus :  0.16190E+02 0.12551E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         30
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         51 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.79245E+09   10000   0.10080E+01   0.76101E+08 
c  VelocityY    0.79245E+09   10000   0.10080E+01   0.00000E+00 
c  VelocityZ    0.79245E+09   10000   0.10080E+01   0.00000E+00 
c  Pressure     0.56356E+04     709   0.14679E-01   0.17452E+00 
c  k            0.41876E+13     235   0.52430E-04   0.12861E+15 
c  epsilon      0.34918E+21     169   0.12756E-04   0.40349E+30 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.724e+05      1.8317e+05         -187.94         -78.655
v  Velocity[Y]             -8.4727e+05      1.8376e+06         -503.07         -267.91
v  Velocity[Z]             -2.5467e+05      5.9775e+05          99.334         -15.877
v  ǁVelocityǁ                   46.243      1.8764e+06          6413.5          4776.1
v  Pressure                 -7.927e+07       1.796e+08      2.5935e+07      1.8447e+07
v  k                            490.93      2.3924e+09      3.1281e+06      1.8924e+06
v  epsilon                  1.5947e+07      1.4421e+17      7.7526e+13      2.9345e+13
v  turbulent_viscosity        0.023145          3146.4          103.07          57.621
v  CourantNb                    583.86      3.6366e+09      1.1027e+06       4.696e+05
v  FourierNb                    62.313      1.5225e+07      1.7297e+05           69231
v  total_pressure           -7.877e+07       1.801e+08      2.6435e+07      1.8947e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1987.4      3.6515e+09      1.2757e+06      5.3883e+05


 TIME FOR THE TIME STEP              191:        0.14729E+02

===============================================================


 INSTANT    0.192000000E+02   TIME STEP NUMBER             192
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.366839241E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.285269962E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.17135E+02 0.17374E+07
   Friction velocity        uet   :  0.11991E+01 0.73656E+05
   Friction velocity        uk    :  0.17576E+02 0.16850E+05
   Dimensionless distance   yplus :  0.21406E+02 0.12777E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         66 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.35001E+09   10000   0.99735E+00   0.88451E+08 
c  VelocityY    0.35001E+09   10000   0.99735E+00   0.00000E+00 
c  VelocityZ    0.35001E+09   10000   0.99735E+00   0.00000E+00 
c  Pressure     0.62023E+04     551   0.71842E-02   0.17655E+00 
c  k            0.52530E+13     241   0.80056E-04   0.22860E+15 
c  epsilon      0.47748E+21     174   0.16903E-04   0.10540E+31 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.8256e+05      2.1408e+05         -506.65         -120.98
v  Velocity[Y]             -9.5678e+05      1.9147e+06          27.556         -76.837
v  Velocity[Z]             -2.6691e+05      6.6622e+05         -51.803         -41.344
v  ǁVelocityǁ                    5.353       1.958e+06          3216.3          2077.3
v  Pressure                 -9.291e+07       1.911e+08      2.5473e+07      1.8146e+07
v  k                            44.309      2.5698e+09      3.6552e+06      1.9699e+06
v  epsilon                  4.9187e+07      1.8129e+17      9.7804e+13      3.7257e+13
v  turbulent_viscosity       0.0010251          3143.5          88.485          78.595
v  CourantNb                    5389.1      3.9512e+09      1.8813e+06      9.2901e+05
v  FourierNb                    691.75      1.5999e+07      1.2305e+05           68143
v  total_pressure           -9.241e+07       1.916e+08      2.5973e+07      1.8646e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7744.3      3.9671e+09      2.0043e+06      9.9715e+05


 TIME FOR THE TIME STEP              192:        0.14748E+02

===============================================================


 INSTANT    0.193000000E+02   TIME STEP NUMBER             193
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.665513380E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.261843599E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29830E+04 0.18460E+07
   Friction velocity        uet   :  0.91244E-01 0.75801E+05
   Friction velocity        uk    :  0.60091E+01 0.20411E+05
   Dimensionless distance   yplus :  0.43190E+02 0.15177E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         63
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         29 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.11439E+10   10000   0.10072E+01   0.12220E+09 
c  VelocityY    0.11439E+10   10000   0.10072E+01   0.00000E+00 
c  VelocityZ    0.11439E+10   10000   0.10072E+01   0.00000E+00 
c  Pressure     0.68923E+04     673   0.13310E-01   0.17884E+00 
c  k            0.72453E+13     236   0.56770E-04   0.22712E+15 
c  epsilon      0.71052E+21     172   0.13119E-04   0.14085E+31 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6202e+05      2.1223e+05         -75.896         -92.444
v  Velocity[Y]             -1.0105e+06      2.1971e+06          110.72         -260.92
v  Velocity[Z]             -2.7111e+05      7.2411e+05          11.716         -26.507
v  ǁVelocityǁ                   19.738      2.2423e+06            6914          4646.1
v  Pressure                -9.6749e+07       2.128e+08      2.9533e+07      2.1002e+07
v  k                           0.67964       2.812e+09      4.1374e+06      2.2609e+06
v  epsilon                  1.5235e+05      2.2048e+17      1.3102e+14      5.0391e+13
v  turbulent_viscosity      0.00056406            2885          113.52          68.449
v  CourantNb                    237.45      4.3331e+09      1.2515e+06       5.101e+05
v  FourierNb                     36.32      1.8005e+07       1.852e+05           77820
v  total_pressure          -9.6249e+07       2.133e+08      3.0033e+07      2.1502e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2623.1      4.3511e+09      1.4367e+06      5.8792e+05


 TIME FOR THE TIME STEP              193:        0.14714E+02

===============================================================


 INSTANT    0.194000000E+02   TIME STEP NUMBER             194
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.207837992E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.286896999E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71692E+04 0.20997E+07
   Friction velocity        uet   :  0.84450E+00 0.86817E+05
   Friction velocity        uk    :  0.15536E+01 0.21396E+05
   Dimensionless distance   yplus :  0.15555E+02 0.15292E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        295
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         37 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.49752E+09   10000   0.99248E+00   0.11595E+09 
c  VelocityY    0.49752E+09   10000   0.99248E+00   0.00000E+00 
c  VelocityZ    0.49752E+09   10000   0.99248E+00   0.00000E+00 
c  Pressure     0.74179E+04     587   0.71925E-02   0.17732E+00 
c  k            0.92454E+13     237   0.77959E-04   0.42519E+15 
c  epsilon      0.10154E+22     174   0.15323E-04   0.31117E+31 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6527e+05      2.7198e+05         -340.88         -108.16
v  Velocity[Y]             -1.1458e+06       2.265e+06          89.867          -63.31
v  Velocity[Z]             -3.0943e+05      8.0635e+05          3.5846         -25.984
v  ǁVelocityǁ                   22.083       2.324e+06          3502.7          2386.7
v  Pressure                -1.1422e+08      2.2519e+08      2.8589e+07      2.0288e+07
v  k                          0.012661      3.6321e+09       4.997e+06       2.599e+06
v  epsilon                       15253      3.0099e+17      1.6941e+14      6.3528e+13
v  turbulent_viscosity      1.3305e-06          2840.3          81.897          56.539
v  CourantNb                    495.88      4.6978e+09       2.113e+06      9.5968e+05
v  FourierNb                    13.293       1.882e+07      1.2269e+05           59169
v  total_pressure          -1.1372e+08      2.2569e+08      2.9089e+07      2.0788e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1353.9      4.7166e+09      2.2357e+06      1.0189e+06


 TIME FOR THE TIME STEP              194:        0.14761E+02

===============================================================


 INSTANT    0.195000000E+02   TIME STEP NUMBER             195
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.244233487E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.259787252E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65745E+04 0.21873E+07
   Friction velocity        uet   :  0.51419E+00 0.88513E+05
   Friction velocity        uk    :  0.10448E+01 0.24699E+05
   Dimensionless distance   yplus :  0.13740E+02 0.17886E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        838
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.16220E+10   10000   0.99909E+00   0.26909E+09 
c  VelocityY    0.16220E+10   10000   0.99909E+00   0.00000E+00 
c  VelocityZ    0.16220E+10   10000   0.99909E+00   0.00000E+00 
c  Pressure     0.82762E+04     683   0.14097E-01   0.18037E+00 
c  k            0.12413E+14     269   0.40792E-04   0.42440E+15 
c  epsilon      0.15122E+22     168   0.78212E-05   0.35045E+31 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6107e+05      2.6498e+05         -288.52         -102.35
v  Velocity[Y]             -1.2202e+06      2.6201e+06          712.05         -344.76
v  Velocity[Z]              -3.646e+05      8.7979e+05          199.33         -25.782
v  ǁVelocityǁ                   25.658      2.6802e+06           11030          7278.1
v  Pressure                -1.1488e+08      2.5528e+08      3.4472e+07        2.44e+07
v  k                           0.04783      3.4545e+09      5.5495e+06        3.07e+06
v  epsilon                      758.53      3.0451e+17      2.1616e+14       8.061e+13
v  turbulent_viscosity      6.5627e-07          3471.3          125.22          77.171
v  CourantNb                    413.56      5.1824e+09      1.4154e+06      5.8632e+05
v  FourierNb                    9.2265      2.0896e+07      1.9888e+05           86867
v  total_pressure          -1.1438e+08      2.5578e+08      3.4972e+07        2.49e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          480.25      5.2033e+09      1.6143e+06      6.7319e+05


 TIME FOR THE TIME STEP              195:        0.14721E+02

===============================================================


 INSTANT    0.196000000E+02   TIME STEP NUMBER             196
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.502846684E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.293040016E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26973E+05 0.24869E+07
   Friction velocity        uet   :  0.54892E+00 0.10235E+06
   Friction velocity        uk    :  0.12265E+01 0.25176E+05
   Dimensionless distance   yplus :  0.12471E+02 0.18099E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        304
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.57602E+09   10000   0.99423E+00   0.29084E+09 
c  VelocityY    0.57602E+09   10000   0.99423E+00   0.00000E+00 
c  VelocityZ    0.57602E+09   10000   0.99423E+00   0.00000E+00 
c  Pressure     0.88040E+04     519   0.68123E-02   0.17631E+00 
c  k            0.15324E+14     235   0.85193E-04   0.10088E+16 
c  epsilon      0.20850E+22     170   0.17818E-04   0.10338E+32 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6373e+05      3.3159e+05         -303.22         -112.94
v  Velocity[Y]             -1.3881e+06      2.7247e+06          128.11         -139.69
v  Velocity[Z]             -4.2517e+05      9.3193e+05           211.7         -14.505
v  ǁVelocityǁ                   29.867      2.7826e+06          3969.1          2647.4
v  Pressure                -1.3426e+08      2.7193e+08      3.4147e+07      2.4191e+07
v  k                            0.8354      5.1998e+09      6.6204e+06      3.4727e+06
v  epsilon                       13827       4.911e+17      2.8849e+14      1.0555e+14
v  turbulent_viscosity      4.8262e-08          3103.7          97.578          78.974
v  CourantNb                    135.23       5.616e+09      3.1494e+06      1.4535e+06
v  FourierNb                    11.237      2.1562e+07      1.3832e+05           73574
v  total_pressure          -1.3376e+08      2.7243e+08      3.4647e+07      2.4691e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3562.9      5.6376e+09      3.2877e+06      1.5271e+06


 TIME FOR THE TIME STEP              196:        0.14739E+02

===============================================================


 INSTANT    0.197000000E+02   TIME STEP NUMBER             197
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.162480944E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.251199570E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34206E+04 0.26283E+07
   Friction velocity        uet   :  0.14800E+00 0.10522E+06
   Friction velocity        uk    :  0.13676E+01 0.27765E+05
   Dimensionless distance   yplus :  0.13939E+02 0.22173E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         73
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         38 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.24006E+10   10000   0.10072E+01   0.44868E+09 
c  VelocityY    0.24006E+10   10000   0.10072E+01   0.00000E+00 
c  VelocityZ    0.24006E+10   10000   0.10072E+01   0.00000E+00 
c  Pressure     0.95309E+04     682   0.12280E-01   0.17496E+00 
c  k            0.20689E+14     263   0.43350E-04   0.15132E+16 
c  epsilon      0.30313E+22     164   0.11588E-04   0.11838E+32 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.064e+05      2.9933e+05         -557.37         -102.18
v  Velocity[Y]             -1.4537e+06      3.1345e+06         -1005.6         -382.12
v  Velocity[Z]              -3.693e+05      1.0627e+06          498.22         -18.393
v  ǁVelocityǁ                   22.779      3.2033e+06           10763          7343.1
v  Pressure                 -1.373e+08      3.0528e+08      4.1658e+07      2.9438e+07
v  k                            18.673      5.5155e+09      9.2624e+06      4.9035e+06
v  epsilon                       46061      6.0369e+17      3.7384e+14       1.462e+14
v  turbulent_viscosity      0.00057151          4360.5          123.78          88.138
v  CourantNb                    753.03      6.2375e+09      1.6569e+06      6.7207e+05
v  FourierNb                    18.573      2.5194e+07      1.8676e+05           89623
v  total_pressure           -1.368e+08      3.0578e+08      4.2158e+07      2.9938e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2786.2      6.2624e+09      1.8437e+06       7.617e+05


 TIME FOR THE TIME STEP              197:        0.14716E+02

===============================================================


 INSTANT    0.198000000E+02   TIME STEP NUMBER             198
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.132723805E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.297260526E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19237E+04 0.29649E+07
   Friction velocity        uet   :  0.96785E+00 0.12102E+06
   Friction velocity        uk    :  0.24786E+01 0.33932E+05
   Dimensionless distance   yplus :  0.29568E+02 0.23781E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          5
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         33 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.96954E+09   10000   0.99056E+00   0.63665E+09 
c  VelocityY    0.96954E+09   10000   0.99056E+00   0.00000E+00 
c  VelocityZ    0.96954E+09   10000   0.99056E+00   0.00000E+00 
c  Pressure     0.10596E+05     539   0.80323E-02   0.17856E+00 
c  k            0.24394E+14     228   0.63371E-04   0.18619E+16 
c  epsilon      0.40356E+22     166   0.12793E-04   0.19302E+32 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.2134e+05      3.7941e+05          -253.4         -129.64
v  Velocity[Y]             -1.6404e+06      3.2751e+06         -141.63         -138.31
v  Velocity[Z]               -4.59e+05      1.1219e+06         -191.99         -77.541
v  ǁVelocityǁ                   13.935      3.3518e+06          8041.4          5508.3
v  Pressure                 -1.618e+08       3.239e+08      4.1071e+07      2.9259e+07
v  k                              57.7      6.8084e+09      9.3254e+06      4.7542e+06
v  epsilon                  6.9503e+06       7.729e+17      4.5469e+14      1.6881e+14
v  turbulent_viscosity        0.017457            3991          132.24          91.664
v  CourantNb                    2796.2       6.671e+09      3.1787e+06      1.4767e+06
v  FourierNb                    61.101      2.3666e+07      2.0297e+05           94369
v  total_pressure           -1.613e+08       3.244e+08      4.1571e+07      2.9759e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          5513.2      6.6947e+09      3.3817e+06       1.571e+06


 TIME FOR THE TIME STEP              198:        0.14740E+02

===============================================================


 INSTANT    0.199000000E+02   TIME STEP NUMBER             199
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.472237650E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.247552986E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32405E+05 0.31398E+07
   Friction velocity        uet   :  0.35735E+00 0.12527E+06
   Friction velocity        uk    :  0.41632E+01 0.35624E+05
   Dimensionless distance   yplus :  0.17592E+02 0.24967E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        118
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ 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        161
@                                                            
@    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.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for         34 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.33290E+10   10000   0.10081E+01   0.38964E+09 
c  VelocityY    0.33290E+10   10000   0.10081E+01   0.00000E+00 
c  VelocityZ    0.33290E+10   10000   0.10081E+01   0.00000E+00 
c  Pressure     0.11494E+05     683   0.13584E-01   0.17715E+00 
c  k            0.32496E+14     230   0.41020E-04   0.15707E+16 
c  epsilon      0.57378E+22     166   0.86307E-05   0.22749E+32 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -9.3865e+05      3.8699e+05         -289.01         -127.73
v  Velocity[Y]             -1.7304e+06      3.7559e+06          524.01         -517.16
v  Velocity[Z]             -5.1154e+05      1.2343e+06          408.42          -41.66
v  ǁVelocityǁ                   56.116      3.8372e+06          7703.7          5467.1
v  Pressure                -1.6436e+08       3.647e+08      5.0764e+07      3.5991e+07
v  k                            5.6007      6.9297e+09      1.0069e+07      5.3222e+06
v  epsilon                  4.8807e+05      8.8074e+17       5.651e+14      2.0906e+14
v  turbulent_viscosity      5.7632e-05           24623          181.41          111.91
v  CourantNb                    1032.4      7.4533e+09      2.6723e+06      1.1881e+06
v  FourierNb                    58.585      2.7138e+07      2.9204e+05      1.2529e+05
v  total_pressure          -1.6386e+08       3.652e+08      5.1264e+07      3.6491e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4275.2      7.4804e+09      2.9643e+06      1.3134e+06


 TIME FOR THE TIME STEP              199:        0.14793E+02

===============================================================


 INSTANT    0.200000000E+02   TIME STEP NUMBER             200
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.123957661E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.301597995E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17852E+05 0.35815E+07
   Friction velocity        uet   :  0.14585E+01 0.14347E+06
   Friction velocity        uk    :  0.36308E+01 0.37829E+05
   Dimensionless distance   yplus :  0.27683E+02 0.26512E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        135
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :       6590
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ 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        161
@                                                            
@    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.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for         31 outlet faces on         82


 Write final restart files
   checkpoint at iteration        200, Physical time    0.20000E+02


   ** Writing the main restart file
      -----------------------------

 Start writing
   End writing the dimensions                           
   End writing the options                              
   End writing the main variables                       
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
   End writing the mass fluxes                          
   End writing the boundary conditions                  
 End writing


 Time for restart files:    0.11777E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.13603E+10   10000   0.99148E+00   0.36240E+09 
c  VelocityY    0.13603E+10   10000   0.99148E+00   0.00000E+00 
c  VelocityZ    0.13603E+10   10000   0.99148E+00   0.00000E+00 
c  Pressure     0.12589E+05     605   0.79613E-02   0.17818E+00 
c  k            0.40457E+14     231   0.75722E-04   0.32581E+16 
c  epsilon      0.76988E+22     169   0.16976E-04   0.55860E+32 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -9.7265e+05      4.6045e+05         -612.96         -164.12
v  Velocity[Y]             -1.9689e+06      3.9022e+06         -266.91          -173.9
v  Velocity[Z]             -5.8161e+05      1.3465e+06          246.53         -41.861
v  ǁVelocityǁ                   50.289      3.9871e+06          9823.4          6514.9
v  Pressure                -1.9452e+08        3.86e+08      4.8663e+07      3.4571e+07
v  k                             31.19      1.0997e+10       1.429e+07       7.017e+06
v  epsilon                  4.2177e+06      1.4244e+18      7.3639e+14      2.7207e+14
v  turbulent_viscosity      0.00011264          7387.1          174.72          117.68
v  CourantNb                    1425.6       8.062e+09       2.655e+06       1.171e+06
v  FourierNb                    14.764      2.8747e+07      2.7015e+05      1.2404e+05
v  total_pressure          -1.9402e+08       3.865e+08      4.9163e+07      3.5071e+07


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3799.6      8.0904e+09      2.9252e+06       1.295e+06


 TIME FOR THE TIME STEP              200:        0.14727E+02

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.17098E-03
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:           1539.992 s
  System CPU time:            4.092 s
  Total CPU time:          6176.252 s

  Elapsed time:            1548.298 s
  CPU / elapsed time          0.997

Memory use summary:

  Total memory used:                             618.707 MiB
                             local minimum:      154.117 MiB  (rank 0)
                             local maximum:      155.535 MiB  (rank 1)
  Theoretical instrumented dynamic memory:       104.896 MiB
                             local minimum:       25.755 MiB  (rank 0)
                             local maximum:       26.679 MiB  (rank 1)
