command: 
 /usr/local/libexec/code_saturne/cs_solver --param CilCurs_1ms_test02.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 09 Jul 2014 10:19:43 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/20140709-1019
  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   =              4 (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  =             10 (Turbulence model            )
       IDEUCH =              0 (0: one-scale model          )
                               (1: two-scale model          )
                               (2: invariant wall function  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.23810E+01 (Limit Y+                    )
       ILOGPO =              1 (0: power law (forbidden for
                                              k-epsilon)    )
                               (1: one-scale log law        )
       IGRHOK =              0 (1: computed Grad(rho k)     )

   - Mixing length       (ITURB = 10)
       XLOMLG =    0.85000E-03 (Characteristic length       )

 --- 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))


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


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

 --- Continuous phase:
       IVISSE =              1 (1: accounted for            )


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

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

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

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

------------------------------------
 Variable          ISTAT      CDTVAR
------------------------------------
 Velocity              1  0.1000E+01
 Pressure              0  0.1000E+01
----------------------------

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

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

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


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

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

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


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


 ** STOKES
    ------
       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 =              0 (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
-----------------------------------------------------------

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

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

       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
turbulent_viscosity
CourantNb
FourierNb
total_pressure
Local Time Step
         --           --

 --- 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 Density                       -1
         7 LamVisc                       -1
         8 turbulent_viscos              -1
         9 CourantNb                     -1
        10 FourierNb                     -1
        11 total_pressure                -1
        12 Local Time Step               -1
         --           --                --

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

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

         2 Velocity                       0
         5 Pressure                       0
         8 turbulent_viscos            -999
         9 CourantNb                   -999
        10 FourierNb                   -999
        11 total_pressure              -999
        12 Local Time Step             -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 (0.295 s)


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

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

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

 Histogram of the number of cells per rank:

    minimum value =              16761
    maximum value =              16762

      1 : [      16761 ;      16762 ] =          4

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

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

    minimum value =              18112
    maximum value =              18491

      1 : [      18112 ;      18187 [ =          2
      2 : [      18187 ;      18263 [ =          0
      3 : [      18263 ;      18339 [ =          0
      4 : [      18339 ;      18415 [ =          1
      5 : [      18415 ;      18491 ] =          1

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

 Histogram of the number of ghost cells per rank:

    minimum value =               1351
    maximum value =               1730

      1 : [       1351 ;       1426 [ =          2
      2 : [       1426 ;       1502 [ =          0
      3 : [       1502 ;       1578 [ =          0
      4 : [       1578 ;       1654 [ =          1
      5 : [       1654 ;       1730 ] =          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 =              17867
    maximum value =              18367

      1 : [      17867 ;      17967 [ =          2
      2 : [      17967 ;      18067 [ =          0
      3 : [      18067 ;      18167 [ =          0
      4 : [      18167 ;      18267 [ =          0
      5 : [      18267 ;      18367 ] =          2

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =               9205
    maximum value =               9293

      1 : [       9205 ;       9222 [ =          2
      2 : [       9222 ;       9240 [ =          1
      3 : [       9240 ;       9257 [ =          0
      4 : [       9257 ;       9275 [ =          0
      5 : [       9275 ;       9293 ] =          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 (0.02 s)
                                                             
       ALMAX  =    0.45893E-01 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.


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


 ** 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
 ---------------------------------

                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  0.0000E+00  0.0000E+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    :  0.00000E+00 0.00000E+00
   Dimensionless distance   yplus :  0.00000E+00 0.00000E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       6590
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.24149E-02     133   0.17421E+00   0.28956E+01 
c  VelocityY    0.24149E-02     133   0.17421E+00   0.00000E+00 
c  VelocityZ    0.24149E-02     133   0.17421E+00   0.00000E+00 
c  Pressure     0.15979E-01     917   0.76797E+00   0.96676E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step       0.0052553                           961


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6046          2.2638       -0.045812       -0.064045
v  Velocity[Y]                -0.60865           2.997         0.17582         0.22541
v  Velocity[Z]                 -2.3862          3.0539        0.040694     -0.00054089
v  ǁVelocityǁ                0.0025078          3.4291         0.30862         0.40402
v  Pressure                     4.0263          2003.7          1284.5            1014
v  turbulent_viscosity               0               0               0               0
v  CourantNb                         0               0               0               0
v  FourierNb                    6.4223          124.82          10.076          9.9961
v  total_pressure                5e+05        5.02e+05      5.0128e+05      5.0101e+05
v  Local Time Step                0.01            0.11        0.026637        0.048937


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.4223          124.82          10.076          9.9961


 TIME FOR THE TIME STEP                1:        0.74699E+00

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


 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         0.273282689E+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 0.18697E+01
   Friction velocity        uet   :  0.11668E-01 0.53813E+00
   Friction velocity        uk    :  0.11668E-01 0.53813E+00
   Dimensionless distance   yplus :  0.12548E+00 0.54309E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4157
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.79864E-01     210   0.66614E+00   0.97397E+00 
c  VelocityY    0.79864E-01     210   0.66614E+00   0.00000E+00 
c  VelocityZ    0.79864E-01     210   0.66614E+00   0.00000E+00 
c  Pressure     0.33265E-01     895   0.19191E+00   0.10577E+01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00012045                         16439


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8244          1.8112        -0.05909       -0.067738
v  Velocity[Y]                -0.50673          2.9743         0.20258          0.2292
v  Velocity[Z]                 -1.7923          2.2396        0.039212       0.0019521
v  ǁVelocityǁ                0.0080978           3.285         0.34744         0.40616
v  Pressure                    -39.847          2075.8          1687.5            1356
v  turbulent_viscosity      0.00034577         0.58087        0.019879        0.023299
v  CourantNb                   0.24126          107.74          5.8177          5.8377
v  FourierNb                   0.85994          847.41          7.6489          4.6432
v  total_pressure           4.9996e+05      5.0208e+05      5.0169e+05      5.0136e+05
v  Local Time Step                0.01           0.121        0.010093        0.010201


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8777          848.62          13.467          10.481


 TIME FOR THE TIME STEP                2:        0.10251E+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         0.361270140E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282694E+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 0.14613E+01
   Friction velocity        uet   :  0.16282E-01 0.66856E+00
   Friction velocity        uk    :  0.16282E-01 0.66856E+00
   Dimensionless distance   yplus :  0.12367E+00 0.46260E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4568
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.67613E-01     216   0.54070E+00   0.37222E+00 
c  VelocityY    0.67613E-01     216   0.54070E+00   0.00000E+00 
c  VelocityZ    0.67613E-01     216   0.54070E+00   0.00000E+00 
c  Pressure     0.33966E-01     824   0.80564E-01   0.62017E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00013608                         16284


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8085            1.74       -0.070188       -0.070025
v  Velocity[Y]                -0.54198          3.0847         0.22625          0.2318
v  Velocity[Z]                 -1.6432          1.6499        0.042204       0.0015045
v  ǁVelocityǁ                0.0019992          3.2244         0.38715         0.41651
v  Pressure                    -140.97          3017.6          2474.6          1954.3
v  turbulent_viscosity      0.00026036         0.64342        0.014727        0.016069
v  CourantNb                   0.08196          116.91          6.8172          6.0618
v  FourierNb                   0.86136          1211.9          7.3099          4.2819
v  total_pressure           4.9986e+05      5.0302e+05      5.0247e+05      5.0195e+05
v  Local Time Step                0.01         0.10872        0.010082        0.010193


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5851          1213.7          14.127          10.344


 TIME FOR THE TIME STEP                3:        0.11130E+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         0.249806229E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282706E+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 0.14865E+01
   Friction velocity        uet   :  0.14757E-01 0.62568E+00
   Friction velocity        uk    :  0.14757E-01 0.62568E+00
   Dimensionless distance   yplus :  0.14255E+00 0.45924E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4706
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.70584E-01     226   0.55441E+00   0.23783E+00 
c  VelocityY    0.70584E-01     226   0.55441E+00   0.00000E+00 
c  VelocityZ    0.70584E-01     226   0.55441E+00   0.00000E+00 
c  Pressure     0.32577E-01     833   0.41542E-01   0.44186E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00015997                         16004


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6571           1.601          -0.077        -0.07063
v  Velocity[Y]                -0.50872          3.1743         0.24645         0.23215
v  Velocity[Z]                 -1.5608          1.4244        0.049133      0.00066186
v  ǁVelocityǁ                0.0020106          3.3317         0.42663         0.43645
v  Pressure                    -246.62          3476.7            2831          2203.6
v  turbulent_viscosity       0.0003684         0.63094        0.015511        0.016457
v  CourantNb                  0.004027          118.08          7.7756          6.3423
v  FourierNb                   0.86322          769.43          7.4398          4.3356
v  total_pressure           4.9975e+05      5.0348e+05      5.0283e+05       5.022e+05
v  Local Time Step                0.01         0.11959        0.010086        0.010217


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4887          769.43          15.215          10.678


 TIME FOR THE TIME STEP                4:        0.12407E+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         0.525975200E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282704E+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 0.15672E+01
   Friction velocity        uet   :  0.63054E-02 0.61101E+00
   Friction velocity        uk    :  0.63054E-02 0.61101E+00
   Dimensionless distance   yplus :  0.71688E-01 0.46916E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4763
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.70693E-01     231   0.51115E+00   0.18778E+00 
c  VelocityY    0.70693E-01     231   0.51115E+00   0.00000E+00 
c  VelocityZ    0.70693E-01     231   0.51115E+00   0.00000E+00 
c  Pressure     0.29974E-01     715   0.31093E-01   0.33749E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00016055                         15782


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5802          1.4294       -0.080844       -0.070682
v  Velocity[Y]                -0.56995          3.2053         0.26297           0.232
v  Velocity[Z]                 -1.5467          1.3029        0.057184     -0.00013022
v  ǁVelocityǁ                0.0019423          3.3964         0.46252          0.4567
v  Pressure                    -388.65          3731.3          3010.9          2312.2
v  turbulent_viscosity      0.00048278          0.5725        0.016592        0.017525
v  CourantNb                0.00062181          118.34          8.6957          6.7268
v  FourierNb                   0.86996          600.39          7.5962          4.4226
v  total_pressure           4.9961e+05      5.0373e+05      5.0301e+05      5.0231e+05
v  Local Time Step                0.01         0.13155        0.010098        0.010248


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4878           600.7          16.292          11.149


 TIME FOR THE TIME STEP                5:        0.10348E+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        -0.969892429E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282711E+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 0.16953E+01
   Friction velocity        uet   :  0.86759E-02 0.56901E+00
   Friction velocity        uk    :  0.86759E-02 0.56901E+00
   Dimensionless distance   yplus :  0.13330E+00 0.48251E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4747
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.72718E-01     234   0.48943E+00   0.15614E+00 
c  VelocityY    0.72718E-01     234   0.48943E+00   0.00000E+00 
c  VelocityZ    0.72718E-01     234   0.48943E+00   0.00000E+00 
c  Pressure     0.26907E-01     721   0.26168E-01   0.26288E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step        0.000164                         15770


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5787          1.4412       -0.083102       -0.070689
v  Velocity[Y]                -0.55489          3.2474         0.27438         0.23191
v  Velocity[Z]                 -1.4953          1.2944        0.065241      -0.0007135
v  ǁVelocityǁ                0.0013011          3.3823         0.49324         0.47491
v  Pressure                    -480.54            3908          3114.7          2365.7
v  turbulent_viscosity      0.00060809         0.50815        0.017631        0.018609
v  CourantNb                  0.006177          114.52          9.5412          7.1033
v  FourierNb                     0.873          562.49          7.7406          4.5088
v  total_pressure           4.9952e+05      5.0391e+05      5.0311e+05      5.0237e+05
v  Local Time Step                0.01         0.14047        0.010115        0.010291


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4794          562.78          17.282          11.612


 TIME FOR THE TIME STEP                6:        0.98391E+00

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


 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         0.467548952E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282726E+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 0.17041E+01
   Friction velocity        uet   :  0.76072E-02 0.54531E+00
   Friction velocity        uk    :  0.76072E-02 0.54531E+00
   Dimensionless distance   yplus :  0.71382E-01 0.52406E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4702
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.73655E-01     237   0.46166E+00   0.12475E+00 
c  VelocityY    0.73655E-01     237   0.46166E+00   0.00000E+00 
c  VelocityZ    0.73655E-01     237   0.46166E+00   0.00000E+00 
c  Pressure     0.25419E-01     690   0.20246E-01   0.21891E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00017066                         15817


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6297          1.4974       -0.084937       -0.070806
v  Velocity[Y]                -0.61617          3.3103         0.28128         0.23203
v  Velocity[Z]                 -1.4925          1.2767        0.072534      -0.0010723
v  ǁVelocityǁ               0.00070297          3.3973         0.52093         0.49323
v  Pressure                    -533.85            4073          3203.3          2414.4
v  turbulent_viscosity      0.00051917         0.44804        0.018563        0.019591
v  CourantNb                 0.0092889          111.48           10.27          7.4346
v  FourierNb                    0.8799          542.29          7.8696          4.5864
v  total_pressure           4.9947e+05      5.0407e+05       5.032e+05      5.0241e+05
v  Local Time Step                0.01         0.14106        0.010128        0.010325


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4646          542.65           18.14          12.021


 TIME FOR THE TIME STEP                7:        0.93252E+00

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


 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        -0.632720377E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282716E+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 0.17791E+01
   Friction velocity        uet   :  0.57085E-02 0.51275E+00
   Friction velocity        uk    :  0.57085E-02 0.51275E+00
   Dimensionless distance   yplus :  0.64510E-01 0.56130E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4654
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.75751E-01     242   0.44355E+00   0.10249E+00 
c  VelocityY    0.75751E-01     242   0.44355E+00   0.00000E+00 
c  VelocityZ    0.75751E-01     242   0.44355E+00   0.00000E+00 
c  Pressure     0.24415E-01     695   0.15902E-01   0.18757E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00017465                         15897


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6194          1.5375       -0.086499       -0.071074
v  Velocity[Y]                -0.68364          3.2539         0.28394          0.2324
v  Velocity[Z]                 -1.5163          1.3163         0.07857      -0.0011963
v  ǁVelocityǁ               0.00063248          3.3764         0.54558         0.51101
v  Pressure                    -565.77          4223.4          3285.4          2465.3
v  turbulent_viscosity      0.00034363         0.40648        0.019425          0.0205
v  CourantNb                  0.012882          106.63          10.913          7.7536
v  FourierNb                   0.89091          531.57           7.993          4.6605
v  total_pressure           4.9943e+05      5.0422e+05      5.0329e+05      5.0247e+05
v  Local Time Step                0.01         0.14097         0.01014        0.010358


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2589           531.9          18.906          12.414


 TIME FOR THE TIME STEP                8:        0.95150E+00

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


 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        -0.643076678E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282718E+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 0.18110E+01
   Friction velocity        uet   :  0.42057E-02 0.50145E+00
   Friction velocity        uk    :  0.42057E-02 0.50145E+00
   Dimensionless distance   yplus :  0.33697E-01 0.58233E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4594
   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    0.77325E-01     248   0.42268E+00   0.87779E-01 
c  VelocityY    0.77325E-01     248   0.42268E+00   0.00000E+00 
c  VelocityZ    0.77325E-01     248   0.42268E+00   0.00000E+00 
c  Pressure     0.23738E-01     662   0.13111E-01   0.16445E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00018017                         15943


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6177          1.5702       -0.087197       -0.071465
v  Velocity[Y]                -0.73615          3.2684         0.28317         0.23278
v  Velocity[Z]                 -1.5699          1.4043        0.083278      -0.0012432
v  ǁVelocityǁ                0.0028246          3.3864         0.56649         0.52739
v  Pressure                    -591.07          4375.7          3375.6            2528
v  turbulent_viscosity      0.00033084         0.41086        0.020245        0.021379
v  CourantNb                  0.020685          105.92          11.472          8.0521
v  FourierNb                   0.90386          538.36          8.1051          4.7288
v  total_pressure           4.9941e+05      5.0438e+05      5.0338e+05      5.0253e+05
v  Local Time Step                0.01         0.14059        0.010152        0.010392


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5057          538.85          19.577          12.781


 TIME FOR THE TIME STEP                9:        0.97866E+00

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


 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        -0.265345644E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282730E+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 0.18536E+01
   Friction velocity        uet   :  0.13045E-01 0.49817E+00
   Friction velocity        uk    :  0.13045E-01 0.49817E+00
   Dimensionless distance   yplus :  0.11891E+00 0.59014E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4540
   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    0.79511E-01     251   0.42255E+00   0.74825E-01 
c  VelocityY    0.79511E-01     251   0.42255E+00   0.00000E+00 
c  VelocityZ    0.79511E-01     251   0.42255E+00   0.00000E+00 
c  Pressure     0.23040E-01     698   0.11081E-01   0.14534E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00018766                         16023


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6547          1.5987        -0.08689       -0.071832
v  Velocity[Y]                -0.77439          3.2778          0.2805           0.233
v  Velocity[Z]                 -1.6211          1.5063        0.086783       -0.001263
v  ǁVelocityǁ                 0.001507          3.4543         0.58374         0.54196
v  Pressure                    -597.66            4529          3472.6          2599.2
v  turbulent_viscosity      0.00029543         0.44627        0.021022        0.022186
v  CourantNb                  0.023436          105.56          11.934          8.3204
v  FourierNb                   0.91667          548.54          8.2165          4.7967
v  total_pressure            4.994e+05      5.0453e+05      5.0347e+05       5.026e+05
v  Local Time Step                0.01          0.1397        0.010161         0.01042


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7001          548.78          20.151          13.117


 TIME FOR THE TIME STEP               10:        0.99865E+00

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


 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        -0.469446173E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282730E+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 0.18554E+01
   Friction velocity        uet   :  0.10060E-01 0.50025E+00
   Friction velocity        uk    :  0.10060E-01 0.50025E+00
   Dimensionless distance   yplus :  0.11782E+00 0.58988E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4472
   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    0.81132E-01     251   0.42180E+00   0.62382E-01 
c  VelocityY    0.81132E-01     251   0.42180E+00   0.00000E+00 
c  VelocityZ    0.81132E-01     251   0.42180E+00   0.00000E+00 
c  Pressure     0.22639E-01     719   0.96993E-02   0.13124E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00018572                         16097


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7224          1.6264       -0.085649       -0.072111
v  Velocity[Y]                -0.78568           3.293         0.27757         0.23303
v  Velocity[Z]                 -1.7068          1.5588        0.089483      -0.0011625
v  ǁVelocityǁ                0.0022655          3.4363         0.59788         0.55494
v  Pressure                     -586.9          4674.4          3564.8            2668
v  turbulent_viscosity      0.00022185         0.47664        0.021747        0.022942
v  CourantNb                 0.0074832           103.6          12.307          8.5524
v  FourierNb                   0.93189          555.54          8.3187          4.8593
v  total_pressure           4.9941e+05      5.0467e+05      5.0356e+05      5.0267e+05
v  Local Time Step                0.01         0.13244        0.010171         0.01045


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.762          555.73          20.625          13.412


 TIME FOR THE TIME STEP               11:        0.96567E+00

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


 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        -0.479733653E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282760E+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 0.18584E+01
   Friction velocity        uet   :  0.46633E-02 0.50965E+00
   Friction velocity        uk    :  0.46633E-02 0.50965E+00
   Dimensionless distance   yplus :  0.51635E-01 0.59236E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4410
   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    0.82681E-01     249   0.40855E+00   0.52390E-01 
c  VelocityY    0.82681E-01     249   0.40855E+00   0.00000E+00 
c  VelocityZ    0.82681E-01     249   0.40855E+00   0.00000E+00 
c  Pressure     0.22020E-01     661   0.85370E-02   0.11829E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00017976                         16158


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7754          1.6492       -0.083622       -0.072295
v  Velocity[Y]                -0.79252          3.3098         0.27528         0.23306
v  Velocity[Z]                 -1.7773          1.5859        0.091553      -0.0010276
v  ǁVelocityǁ                0.0020069          3.4809         0.60964         0.56651
v  Pressure                    -567.81          4807.4          3652.2            2733
v  turbulent_viscosity      0.00020143         0.50667         0.02238        0.023614
v  CourantNb                  0.005452          102.67          12.606          8.7551
v  FourierNb                    0.9402          573.25          8.4033           4.912
v  total_pressure           4.9943e+05      5.0481e+05      5.0365e+05      5.0273e+05
v  Local Time Step                0.01         0.14569        0.010178        0.010476


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7048          573.37          21.009          13.667


 TIME FOR THE TIME STEP               12:        0.98578E+00

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


 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        -0.677933407E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282740E+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 0.18581E+01
   Friction velocity        uet   :  0.72554E-02 0.51880E+00
   Friction velocity        uk    :  0.72554E-02 0.51880E+00
   Dimensionless distance   yplus :  0.95286E-01 0.59411E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4345
   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    0.83751E-01     249   0.40708E+00   0.44883E-01 
c  VelocityY    0.83751E-01     249   0.40708E+00   0.00000E+00 
c  VelocityZ    0.83751E-01     249   0.40708E+00   0.00000E+00 
c  Pressure     0.21876E-01     683   0.77261E-02   0.10935E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00017468                         16202


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8325          1.6984       -0.081085       -0.072359
v  Velocity[Y]                -0.82856          3.3686          0.2739         0.23297
v  Velocity[Z]                 -1.8641          1.5965        0.093318     -0.00091785
v  ǁVelocityǁ                0.0017399          3.5106         0.61954         0.57674
v  Pressure                    -551.85          4922.5          3729.4          2789.2
v  turbulent_viscosity       0.0001781         0.53506        0.022943        0.024209
v  CourantNb                  0.022585          100.72          12.847          8.9293
v  FourierNb                   0.93844          577.13          8.4806           4.959
v  total_pressure           4.9945e+05      5.0492e+05      5.0373e+05      5.0279e+05
v  Local Time Step                0.01         0.15708        0.010181        0.010497


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7749           577.2          21.328          13.888


 TIME FOR THE TIME STEP               13:        0.10021E+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        -0.447098400E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282775E+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 0.18470E+01
   Friction velocity        uet   :  0.83853E-02 0.52788E+00
   Friction velocity        uk    :  0.83853E-02 0.52788E+00
   Dimensionless distance   yplus :  0.10437E+00 0.58483E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4296
   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    0.84999E-01     251   0.39425E+00   0.39658E-01 
c  VelocityY    0.84999E-01     251   0.39425E+00   0.00000E+00 
c  VelocityZ    0.84999E-01     251   0.39425E+00   0.00000E+00 
c  Pressure     0.21525E-01     679   0.68081E-02   0.10074E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00017099                         16253


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9082           1.679       -0.078254       -0.072336
v  Velocity[Y]                -0.84131          3.3694         0.27355         0.23299
v  Velocity[Z]                 -1.9197          1.5888        0.094979     -0.00074432
v  ǁVelocityǁ                  0.00171           3.568         0.62833         0.58608
v  Pressure                    -543.85          5031.4          3802.4          2841.8
v  turbulent_viscosity      0.00020762         0.56669        0.023429        0.024723
v  CourantNb                 0.0082293          98.978          13.046          9.0818
v  FourierNb                   0.93359          594.92          8.5474          5.0003
v  total_pressure           4.9946e+05      5.0503e+05       5.038e+05      5.0284e+05
v  Local Time Step                0.01          0.1233        0.010187        0.010521


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9342          594.93          21.593          14.082


 TIME FOR THE TIME STEP               14:        0.97757E+00

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


 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        -0.396227454E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282770E+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 0.19243E+01
   Friction velocity        uet   :  0.56314E-02 0.53915E+00
   Friction velocity        uk    :  0.56314E-02 0.53915E+00
   Dimensionless distance   yplus :  0.91538E-01 0.57305E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4255
   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    0.85934E-01     253   0.37484E+00   0.36701E-01 
c  VelocityY    0.85934E-01     253   0.37484E+00   0.00000E+00 
c  VelocityZ    0.85934E-01     253   0.37484E+00   0.00000E+00 
c  Pressure     0.21188E-01     662   0.61947E-02   0.93238E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00016812                         16317


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9288          1.7231       -0.075421       -0.072363
v  Velocity[Y]                 -0.8648          3.4266         0.27391         0.23296
v  Velocity[Z]                 -2.0022          1.5783        0.096799     -0.00046221
v  ǁVelocityǁ                0.0024135          3.5873         0.63634         0.59479
v  Pressure                    -542.66          5131.8          3869.6          2888.7
v  turbulent_viscosity      0.00020561          0.6054        0.023862        0.025186
v  CourantNb                 0.0090321          97.572           13.22          9.2199
v  FourierNb                   0.94403          586.42          8.6076           5.036
v  total_pressure           4.9946e+05      5.0513e+05      5.0387e+05      5.0289e+05
v  Local Time Step                0.01        0.091771        0.010186        0.010515


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.0116          586.74          21.828          14.256


 TIME FOR THE TIME STEP               15:        0.96570E+00

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


 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        -0.403283140E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282764E+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 0.19029E+01
   Friction velocity        uet   :  0.76755E-02 0.54850E+00
   Friction velocity        uk    :  0.76755E-02 0.54850E+00
   Dimensionless distance   yplus :  0.90809E-01 0.56680E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4223
   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    0.87875E-01     255   0.37431E+00   0.33723E-01 
c  VelocityY    0.87875E-01     255   0.37431E+00   0.00000E+00 
c  VelocityZ    0.87875E-01     255   0.37431E+00   0.00000E+00 
c  Pressure     0.20774E-01     684   0.55243E-02   0.86311E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00016591                         16364


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9628          1.7206       -0.072722       -0.072344
v  Velocity[Y]                -0.88736          3.4097         0.27484         0.23295
v  Velocity[Z]                   -2.05          1.5736        0.098765     -0.00014862
v  ǁVelocityǁ                0.0032939          3.5978          0.6438         0.60292
v  Pressure                    -549.58          5230.2          3937.4          2935.7
v  turbulent_viscosity       0.0002071         0.64073        0.024248        0.025598
v  CourantNb                  0.017947          104.05           13.38          9.3475
v  FourierNb                   0.95369           581.8          8.6569          5.0624
v  total_pressure           4.9945e+05      5.0523e+05      5.0394e+05      5.0294e+05
v  Local Time Step                0.01        0.081586        0.010177        0.010478


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9568           582.2          22.036           14.41


 TIME FOR THE TIME STEP               16:        0.97880E+00

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


 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         0.208317165E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282799E+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 0.19567E+01
   Friction velocity        uet   :  0.12979E-01 0.56459E+00
   Friction velocity        uk    :  0.12979E-01 0.56459E+00
   Dimensionless distance   yplus :  0.12798E+00 0.57008E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4188
   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    0.87991E-01     256   0.34927E+00   0.33103E-01 
c  VelocityY    0.87991E-01     256   0.34927E+00   0.00000E+00 
c  VelocityZ    0.87991E-01     256   0.34927E+00   0.00000E+00 
c  Pressure     0.20555E-01     618   0.50716E-02   0.80953E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00016254                         16413


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9693          1.7184       -0.070389       -0.072397
v  Velocity[Y]                -0.93428          3.4311         0.27608         0.23283
v  Velocity[Z]                 -2.0922          1.5542         0.10105      0.00012682
v  ǁVelocityǁ                 0.003539          3.6144         0.65103         0.61093
v  Pressure                    -560.71            5321          4000.8          2979.9
v  turbulent_viscosity      0.00026066         0.68575        0.024609        0.025992
v  CourantNb                 0.0075103          109.86          13.529          9.4664
v  FourierNb                   0.93657          599.55          8.7023          5.0826
v  total_pressure           4.9944e+05      5.0532e+05        5.04e+05      5.0298e+05
v  Local Time Step                0.01        0.063812        0.010161        0.010421


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9366          599.81          22.232          14.549


 TIME FOR THE TIME STEP               17:        0.95434E+00

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


 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        -0.868532695E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282761E+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 0.19439E+01
   Friction velocity        uet   :  0.14927E-01 0.57774E+00
   Friction velocity        uk    :  0.14927E-01 0.57774E+00
   Dimensionless distance   yplus :  0.13002E+00 0.56475E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4155
   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    0.89839E-01     257   0.35772E+00   0.32006E-01 
c  VelocityY    0.89839E-01     257   0.35772E+00   0.00000E+00 
c  VelocityZ    0.89839E-01     257   0.35772E+00   0.00000E+00 
c  Pressure     0.20292E-01     646   0.46693E-02   0.75974E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00016126                         16453


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9993          1.7144       -0.068487       -0.072441
v  Velocity[Y]                -0.95482          3.4776          0.2775          0.2328
v  Velocity[Z]                 -2.1297          1.5452         0.10349      0.00037487
v  ǁVelocityǁ                0.0028482          3.6796         0.65781         0.61849
v  Pressure                    -572.31          5408.4            4063          3022.8
v  turbulent_viscosity      0.00027015         0.73793        0.024948        0.026363
v  CourantNb                 0.0063704          114.85          13.675          9.5828
v  FourierNb                    0.9431          587.35          8.7449          5.1045
v  total_pressure           4.9943e+05      5.0541e+05      5.0406e+05      5.0302e+05
v  Local Time Step                0.01        0.069301        0.010147        0.010375


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6632          588.02           22.42          14.687


 TIME FOR THE TIME STEP               18:        0.96134E+00

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


 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        -0.214588518E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282799E+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 0.20047E+01
   Friction velocity        uet   :  0.51406E-02 0.59713E+00
   Friction velocity        uk    :  0.51406E-02 0.59713E+00
   Dimensionless distance   yplus :  0.70594E-01 0.56331E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4115
   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    0.90832E-01     257   0.34964E+00   0.30906E-01 
c  VelocityY    0.90832E-01     257   0.34964E+00   0.00000E+00 
c  VelocityZ    0.90832E-01     257   0.34964E+00   0.00000E+00 
c  Pressure     0.20046E-01     587   0.43115E-02   0.71614E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00015892                         16469


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0254          1.7562       -0.067059       -0.072543
v  Velocity[Y]                -0.96939          3.4701         0.27896         0.23275
v  Velocity[Z]                 -2.1799           1.531         0.10631      0.00064027
v  ǁVelocityǁ                0.0040815          3.6662         0.66435         0.62572
v  Pressure                    -584.27          5496.2          4127.8          3068.4
v  turbulent_viscosity      0.00028571         0.79448        0.025269        0.026721
v  CourantNb                  0.032903          118.88          13.812          9.6929
v  FourierNb                   0.95464          589.23          8.7837          5.1261
v  total_pressure           4.9942e+05       5.055e+05      5.0413e+05      5.0307e+05
v  Local Time Step                0.01        0.071204        0.010136        0.010338


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6754          590.02          22.596          14.819


 TIME FOR THE TIME STEP               19:        0.98122E+00

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


 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        -0.143876983E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282768E+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 0.19833E+01
   Friction velocity        uet   :  0.14499E-01 0.61416E+00
   Friction velocity        uk    :  0.14499E-01 0.61416E+00
   Dimensionless distance   yplus :  0.12973E+00 0.55281E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4071
   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    0.92165E-01     257   0.34395E+00   0.29743E-01 
c  VelocityY    0.92165E-01     257   0.34395E+00   0.00000E+00 
c  VelocityZ    0.92165E-01     257   0.34395E+00   0.00000E+00 
c  Pressure     0.19718E-01     586   0.39507E-02   0.67397E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00015886                         16496


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0646          1.7281       -0.065993       -0.072608
v  Velocity[Y]                -0.98142          3.4403          0.2803         0.23268
v  Velocity[Z]                 -2.1988          1.5196         0.10921      0.00082923
v  ǁVelocityǁ                0.0036366          3.6432         0.67056         0.63275
v  Pressure                    -593.36          5574.1          4185.8          3109.1
v  turbulent_viscosity      0.00035251         0.85511        0.025582        0.027046
v  CourantNb                 0.0062538           124.5          13.946          9.7981
v  FourierNb                   0.96323          597.55            8.82          5.1426
v  total_pressure           4.9941e+05      5.0557e+05      5.0419e+05      5.0311e+05
v  Local Time Step                0.01        0.075167        0.010128         0.01031


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3194          598.33          22.766          14.941


 TIME FOR THE TIME STEP               20:        0.10089E+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        -0.138043871E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282769E+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 0.20593E+01
   Friction velocity        uet   :  0.14618E-01 0.63855E+00
   Friction velocity        uk    :  0.14618E-01 0.63855E+00
   Dimensionless distance   yplus :  0.12454E+00 0.56385E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4019
   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    0.93411E-01     256   0.34320E+00   0.29533E-01 
c  VelocityY    0.93411E-01     256   0.34320E+00   0.00000E+00 
c  VelocityZ    0.93411E-01     256   0.34320E+00   0.00000E+00 
c  Pressure     0.19543E-01     587   0.37440E-02   0.64092E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00015616                         16520


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0994          1.7438       -0.065368       -0.072656
v  Velocity[Y]                  -0.987          3.5208         0.28157         0.23252
v  Velocity[Z]                 -2.2202          1.5188         0.11224       0.0010017
v  ǁVelocityǁ                0.0038668          3.6963         0.67638         0.63942
v  Pressure                    -599.36          5644.6          4238.1          3145.1
v  turbulent_viscosity      0.00033531         0.92826        0.025881        0.027368
v  CourantNb                  0.022772          127.18          14.074          9.9011
v  FourierNb                   0.96639          601.24          8.8622          5.1673
v  total_pressure            4.994e+05      5.0564e+05      5.0424e+05      5.0315e+05
v  Local Time Step                0.01        0.074203        0.010122        0.010294


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4365          602.14          22.936          15.068


 TIME FOR THE TIME STEP               21:        0.95829E+00

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


 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         0.355778322E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282770E+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 0.20466E+01
   Friction velocity        uet   :  0.10108E-01 0.66444E+00
   Friction velocity        uk    :  0.10108E-01 0.66444E+00
   Dimensionless distance   yplus :  0.69521E-01 0.55794E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3969
   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    0.94272E-01     255   0.35326E+00   0.28634E-01 
c  VelocityY    0.94272E-01     255   0.35326E+00   0.00000E+00 
c  VelocityZ    0.94272E-01     255   0.35326E+00   0.00000E+00 
c  Pressure     0.19196E-01     565   0.34601E-02   0.60584E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00015543                         16539


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1253          1.8002       -0.065095       -0.072711
v  Velocity[Y]                -0.99068           3.507         0.28263         0.23241
v  Velocity[Z]                 -2.2465          1.5166         0.11522       0.0011257
v  ǁVelocityǁ                0.0037287          3.7456          0.6817         0.64582
v  Pressure                    -602.33          5711.7          4288.7            3180
v  turbulent_viscosity      0.00031902          1.0162        0.026169        0.027662
v  CourantNb                  0.021348          133.25          14.194          9.9984
v  FourierNb                   0.96684          611.34          8.8983          5.1875
v  total_pressure            4.994e+05      5.0571e+05      5.0429e+05      5.0318e+05
v  Local Time Step                0.01          0.0749        0.010118        0.010285


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4381          612.29          23.092          15.186


 TIME FOR THE TIME STEP               22:        0.94190E+00

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


 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        -0.687711344E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282799E+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 0.20458E+01
   Friction velocity        uet   :  0.11851E-01 0.69540E+00
   Friction velocity        uk    :  0.11851E-01 0.69540E+00
   Dimensionless distance   yplus :  0.89629E-01 0.56565E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3936
   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    0.95323E-01     252   0.34554E+00   0.27784E-01 
c  VelocityY    0.95323E-01     252   0.34554E+00   0.00000E+00 
c  VelocityZ    0.95323E-01     252   0.34554E+00   0.00000E+00 
c  Pressure     0.18756E-01     565   0.31652E-02   0.57109E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00015316                         16552


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1443          1.8366       -0.065261       -0.072859
v  Velocity[Y]                -0.99949          3.5322         0.28361         0.23224
v  Velocity[Z]                 -2.2681          1.5233         0.11804       0.0011937
v  ǁVelocityǁ                  0.00423          3.7548         0.68659         0.65168
v  Pressure                    -601.04          5776.6          4337.9          3214.2
v  turbulent_viscosity      0.00032149          1.1102        0.026449        0.027957
v  CourantNb                  0.002627          137.89          14.303          10.091
v  FourierNb                   0.97257          639.87          8.9331          5.2076
v  total_pressure            4.994e+05      5.0578e+05      5.0434e+05      5.0321e+05
v  Local Time Step                0.01        0.074002        0.010115        0.010278


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.331          640.87          23.236          15.298


 TIME FOR THE TIME STEP               23:        0.92933E+00

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


 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        -0.985954126E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282801E+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 0.20612E+01
   Friction velocity        uet   :  0.16149E-01 0.72715E+00
   Friction velocity        uk    :  0.16149E-01 0.72715E+00
   Dimensionless distance   yplus :  0.14449E+00 0.57426E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3900
   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    0.96672E-01     248   0.34155E+00   0.26851E-01 
c  VelocityY    0.96672E-01     248   0.34155E+00   0.00000E+00 
c  VelocityZ    0.96672E-01     248   0.34155E+00   0.00000E+00 
c  Pressure     0.18385E-01     537   0.29577E-02   0.54116E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00015355                         16566


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1462          1.8771       -0.065701       -0.072891
v  Velocity[Y]                 -1.0036          3.5411          0.2843         0.23211
v  Velocity[Z]                 -2.2725          1.5559         0.12079       0.0012881
v  ǁVelocityǁ                0.0053211          3.7907          0.6908         0.65707
v  Pressure                    -600.15          5832.9          4380.5            3243
v  turbulent_viscosity      0.00030394          1.2124        0.026722         0.02823
v  CourantNb                 0.0017074          141.62          14.402          10.176
v  FourierNb                   0.97392          662.38          8.9726          5.2304
v  total_pressure            4.994e+05      5.0583e+05      5.0438e+05      5.0324e+05
v  Local Time Step                0.01        0.076666        0.010112        0.010271


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6204             692          23.375          15.407


 TIME FOR THE TIME STEP               24:        0.93523E+00

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


 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        -0.135751456E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282819E+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 0.20825E+01
   Friction velocity        uet   :  0.83749E-02 0.76220E+00
   Friction velocity        uk    :  0.83749E-02 0.76220E+00
   Dimensionless distance   yplus :  0.10896E+00 0.56764E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3876
   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    0.97626E-01     248   0.33260E+00   0.26033E-01 
c  VelocityY    0.97626E-01     248   0.33260E+00   0.00000E+00 
c  VelocityZ    0.97626E-01     248   0.33260E+00   0.00000E+00 
c  Pressure     0.18308E-01     570   0.28037E-02   0.52180E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00015291                         16589


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1184          1.9182       -0.066527       -0.073003
v  Velocity[Y]                 -1.0042          3.6102         0.28492           0.232
v  Velocity[Z]                 -2.2737          1.5635         0.12337       0.0013214
v  ǁVelocityǁ                0.0058208          3.8251          0.6946         0.66191
v  Pressure                    -600.92          5882.7          4417.6            3268
v  turbulent_viscosity      0.00033571          1.3231         0.02698        0.028497
v  CourantNb                  0.022856          145.99          14.488          10.254
v  FourierNb                   0.97229          719.21          9.0069          5.2505
v  total_pressure            4.994e+05      5.0588e+05      5.0442e+05      5.0327e+05
v  Local Time Step                0.01        0.072651        0.010107        0.010258


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6442          752.44          23.495          15.505


 TIME FOR THE TIME STEP               25:        0.91579E+00

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


 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        -0.562666782E-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 : -0.00000E+00 0.20779E+01
   Friction velocity        uet   :  0.15286E-01 0.83026E+00
   Friction velocity        uk    :  0.15286E-01 0.83026E+00
   Dimensionless distance   yplus :  0.14773E+00 0.58438E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3862
   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    0.98692E-01     245   0.33712E+00   0.24924E-01 
c  VelocityY    0.98692E-01     245   0.33712E+00   0.00000E+00 
c  VelocityZ    0.98692E-01     245   0.33712E+00   0.00000E+00 
c  Pressure     0.17828E-01     551   0.25622E-02   0.49318E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00015095                         16599


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1658          1.9445       -0.067592       -0.073029
v  Velocity[Y]                 -1.0024          3.5965         0.28536         0.23188
v  Velocity[Z]                 -2.2814          1.6046         0.12568       0.0013867
v  ǁVelocityǁ                0.0074422          3.8378         0.69788         0.66629
v  Pressure                    -603.22          5926.1          4449.1            3288
v  turbulent_viscosity      0.00030492          1.5385        0.027241        0.028764
v  CourantNb                  0.010355          151.18          14.565          10.325
v  FourierNb                   0.95573          831.91          9.0414          5.2665
v  total_pressure            4.994e+05      5.0593e+05      5.0445e+05      5.0329e+05
v  Local Time Step                0.01        0.079916        0.010102        0.010244


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5453          855.89          23.606          15.591


 TIME FOR THE TIME STEP               26:        0.89807E+00

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


 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        -0.130962742E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282787E+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 0.21014E+01
   Friction velocity        uet   :  0.14218E-01 0.91308E+00
   Friction velocity        uk    :  0.14218E-01 0.91308E+00
   Dimensionless distance   yplus :  0.12025E+00 0.57871E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3844
   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    0.99940E-01     245   0.32692E+00   0.23516E-01 
c  VelocityY    0.99940E-01     245   0.32692E+00   0.00000E+00 
c  VelocityZ    0.99940E-01     245   0.32692E+00   0.00000E+00 
c  Pressure     0.17541E-01     553   0.23773E-02   0.47160E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00015053                         16620


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1345          1.9715       -0.068787        -0.07303
v  Velocity[Y]                -0.99749          3.5652         0.28565         0.23178
v  Velocity[Z]                 -2.2931          1.6176          0.1279       0.0014087
v  ǁVelocityǁ                0.0048711          3.8232         0.70083         0.67041
v  Pressure                    -609.73          5965.8          4477.3          3305.5
v  turbulent_viscosity      0.00026453          1.7835        0.027478           0.029
v  CourantNb                   0.07677           153.6           14.63          10.389
v  FourierNb                   0.94535          955.39          9.0709          5.2823
v  total_pressure           4.9939e+05      5.0597e+05      5.0448e+05      5.0331e+05
v  Local Time Step                0.01        0.087908        0.010096        0.010229


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4942          981.26          23.701          15.671


 TIME FOR THE TIME STEP               27:        0.93526E+00

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


 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        -0.843224608E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282837E+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 0.21081E+01
   Friction velocity        uet   :  0.11908E-01 0.97218E+00
   Friction velocity        uk    :  0.11908E-01 0.97218E+00
   Dimensionless distance   yplus :  0.15002E+00 0.59289E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3815
   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    0.10056E+00     247   0.32167E+00   0.22612E-01 
c  VelocityY    0.10056E+00     247   0.32167E+00   0.00000E+00 
c  VelocityZ    0.10056E+00     247   0.32167E+00   0.00000E+00 
c  Pressure     0.17694E-01     533   0.22533E-02   0.46289E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00014628                         16642


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1233          1.9825       -0.070191       -0.072972
v  Velocity[Y]                 -1.0126          3.6633         0.28578         0.23163
v  Velocity[Z]                 -2.2842          1.6605         0.12994       0.0015504
v  ǁVelocityǁ                 0.008882           3.937         0.70327         0.67402
v  Pressure                    -616.33          6000.2          4498.6          3317.5
v  turbulent_viscosity      0.00030218          1.9994        0.027719        0.029237
v  CourantNb                  0.083135          156.86          14.688          10.449
v  FourierNb                   0.92758            1064          9.1049          5.2977
v  total_pressure           4.9938e+05        5.06e+05       5.045e+05      5.0332e+05
v  Local Time Step                0.01        0.095611        0.010091        0.010217


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7105          1092.1          23.793          15.747


 TIME FOR THE TIME STEP               28:        0.90626E+00

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


 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        -0.446985407E-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 : -0.00000E+00 0.20980E+01
   Friction velocity        uet   :  0.13073E-01 0.10312E+01
   Friction velocity        uk    :  0.13073E-01 0.10312E+01
   Dimensionless distance   yplus :  0.15248E+00 0.60162E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3788
   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    0.10225E+00     250   0.33452E+00   0.22257E-01 
c  VelocityY    0.10225E+00     250   0.33452E+00   0.00000E+00 
c  VelocityZ    0.10225E+00     250   0.33452E+00   0.00000E+00 
c  Pressure     0.17423E-01     498   0.21418E-02   0.44405E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step       0.0001435                         16666


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1334          2.0214       -0.071663       -0.072887
v  Velocity[Y]                 -1.0151          3.6283         0.28566         0.23147
v  Velocity[Z]                 -2.3024          1.6697         0.13203       0.0016363
v  ǁVelocityǁ                0.0039573          3.9078         0.70539         0.67741
v  Pressure                    -623.89          6092.7          4513.3          3324.3
v  turbulent_viscosity      0.00034507          2.2324        0.027942        0.029449
v  CourantNb                  0.072533          159.51          14.736          10.504
v  FourierNb                   0.91659          1184.3          9.1393          5.3129
v  total_pressure           4.9938e+05      5.0609e+05      5.0451e+05      5.0332e+05
v  Local Time Step                0.01        0.092377        0.010086        0.010206


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7805          1215.2          23.876          15.816


 TIME FOR THE TIME STEP               29:        0.88534E+00

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


 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        -0.566389280E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282831E+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 0.21058E+01
   Friction velocity        uet   :  0.11859E-01 0.10942E+01
   Friction velocity        uk    :  0.11859E-01 0.10942E+01
   Dimensionless distance   yplus :  0.12308E+00 0.60945E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3763
   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    0.10332E+00     254   0.35360E+00   0.20811E-01 
c  VelocityY    0.10332E+00     254   0.35360E+00   0.00000E+00 
c  VelocityZ    0.10332E+00     254   0.35360E+00   0.00000E+00 
c  Pressure     0.17354E-01     480   0.20850E-02   0.43112E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00014167                         16684


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1264          2.0392        -0.07318       -0.072815
v  Velocity[Y]                 -1.0211          3.6801         0.28535         0.23136
v  Velocity[Z]                 -2.3041          1.7025         0.13396       0.0016287
v  ǁVelocityǁ                0.0015669          3.9709         0.70711         0.68053
v  Pressure                    -634.43          6190.4          4524.5          3328.9
v  turbulent_viscosity      0.00034948          2.4811        0.028154        0.029633
v  CourantNb                  0.028042          163.14          14.777          10.553
v  FourierNb                   0.94431          1310.4           9.171          5.3268
v  total_pressure           4.9937e+05      5.0619e+05      5.0452e+05      5.0333e+05
v  Local Time Step                0.01        0.091226        0.010083        0.010197


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6836          1344.4          23.948           15.88


 TIME FOR THE TIME STEP               30:        0.93970E+00

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


 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        -0.983419810E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282802E+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 0.21075E+01
   Friction velocity        uet   :  0.11227E-01 0.11673E+01
   Friction velocity        uk    :  0.11227E-01 0.11673E+01
   Dimensionless distance   yplus :  0.15344E+00 0.61177E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3728
   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    0.10357E+00     257   0.34169E+00   0.19720E-01 
c  VelocityY    0.10357E+00     257   0.34169E+00   0.00000E+00 
c  VelocityZ    0.10357E+00     257   0.34169E+00   0.00000E+00 
c  Pressure     0.17269E-01     503   0.19917E-02   0.41834E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00014097                         16691


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1285          2.0441        -0.07478       -0.072778
v  Velocity[Y]                 -1.0293          3.6908         0.28493         0.23134
v  Velocity[Z]                 -2.3408          1.7163         0.13587       0.0016222
v  ǁVelocityǁ                0.0034954          3.9855         0.70842         0.68297
v  Pressure                    -648.49            6296          4538.7          3336.5
v  turbulent_viscosity      0.00029085          2.7885        0.028368        0.029832
v  CourantNb                 0.0084105          165.18          14.808          10.595
v  FourierNb                   0.92597          1467.2           9.205           5.343
v  total_pressure           4.9935e+05       5.063e+05      5.0454e+05      5.0334e+05
v  Local Time Step                0.01        0.077151        0.010081        0.010193


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5153          1504.7          24.013          15.939


 TIME FOR THE TIME STEP               31:        0.89777E+00

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


 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        -0.768544757E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282870E+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 0.20848E+01
   Friction velocity        uet   :  0.14501E-01 0.12412E+01
   Friction velocity        uk    :  0.14501E-01 0.12412E+01
   Dimensionless distance   yplus :  0.15526E+00 0.61409E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3699
   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    0.10541E+00     259   0.35080E+00   0.19103E-01 
c  VelocityY    0.10541E+00     259   0.35080E+00   0.00000E+00 
c  VelocityZ    0.10541E+00     259   0.35080E+00   0.00000E+00 
c  Pressure     0.17388E-01     479   0.20236E-02   0.41090E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00013866                         16698


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1284           2.065       -0.076269       -0.072646
v  Velocity[Y]                 -1.0273          3.7292         0.28445         0.23132
v  Velocity[Z]                 -2.3638          1.7336         0.13759       0.0016124
v  ǁVelocityǁ                0.0058467          4.0293         0.70958         0.68524
v  Pressure                    -660.64          6405.4          4547.4            3340
v  turbulent_viscosity      0.00030914           3.111        0.028564        0.029988
v  CourantNb                  0.025222          166.04          14.832           10.63
v  FourierNb                   0.93598            1836          9.2414          5.3597
v  total_pressure           4.9934e+05      5.0641e+05      5.0455e+05      5.0334e+05
v  Local Time Step                0.01        0.072378        0.010083          0.0102


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7456          1877.1          24.074          15.989


 TIME FOR THE TIME STEP               32:        0.94863E+00

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


 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        -0.370883302E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282822E+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 0.21033E+01
   Friction velocity        uet   :  0.13659E-01 0.13206E+01
   Friction velocity        uk    :  0.13659E-01 0.13206E+01
   Dimensionless distance   yplus :  0.15704E+00 0.61789E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3668
   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    0.10689E+00     260   0.36880E+00   0.17826E-01 
c  VelocityY    0.10689E+00     260   0.36880E+00   0.00000E+00 
c  VelocityZ    0.10689E+00     260   0.36880E+00   0.00000E+00 
c  Pressure     0.17323E-01     482   0.19736E-02   0.39959E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00013329                         16707


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1567          2.0821       -0.077835       -0.072666
v  Velocity[Y]                 -1.0424          3.7472         0.28391          0.2313
v  Velocity[Z]                 -2.3782          1.7532         0.13927       0.0016039
v  ǁVelocityǁ                0.0047449          4.0443         0.71055         0.68723
v  Pressure                    -671.15          6512.4          4558.3            3346
v  turbulent_viscosity      0.00035105          3.5143        0.028751        0.030144
v  CourantNb                  0.025685          169.92          14.853          10.663
v  FourierNb                   0.94216          1834.5          9.2698          5.3734
v  total_pressure           4.9933e+05      5.0651e+05      5.0456e+05      5.0335e+05
v  Local Time Step                0.01        0.078825        0.010085        0.010206


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8948          1879.8          24.123          16.036


 TIME FOR THE TIME STEP               33:        0.88311E+00

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


 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        -0.264988964E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282858E+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 0.21272E+01
   Friction velocity        uet   :  0.93321E-02 0.14011E+01
   Friction velocity        uk    :  0.93321E-02 0.14011E+01
   Dimensionless distance   yplus :  0.12256E+00 0.61457E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3655
   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    0.10843E+00     260   0.38995E+00   0.18836E-01 
c  VelocityY    0.10843E+00     260   0.38995E+00   0.00000E+00 
c  VelocityZ    0.10843E+00     260   0.38995E+00   0.00000E+00 
c  Pressure     0.17489E-01     555   0.19090E-02   0.39375E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00013192                         16711


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1607          2.0983        -0.07932        -0.07259
v  Velocity[Y]                 -1.0539          3.6917         0.28348         0.23133
v  Velocity[Z]                 -2.4007          1.7851         0.14069        0.001566
v  ǁVelocityǁ                0.0044601          3.9859         0.71119          0.6886
v  Pressure                    -680.67          6626.3            4569          3352.2
v  turbulent_viscosity       0.0003728          3.9442        0.028922         0.03028
v  CourantNb                 0.0014246          172.03           14.87           10.69
v  FourierNb                   0.87818          2051.8          9.3014          5.3863
v  total_pressure           4.9932e+05      5.0663e+05      5.0457e+05      5.0335e+05
v  Local Time Step                0.01        0.078339        0.010085        0.010205


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8814          2101.5          24.172          16.076


 TIME FOR THE TIME STEP               34:        0.95588E+00

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


 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         0.750312373E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282872E+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 0.21373E+01
   Friction velocity        uet   :  0.90437E-02 0.14968E+01
   Friction velocity        uk    :  0.90437E-02 0.14968E+01
   Dimensionless distance   yplus :  0.90289E-01 0.61645E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3632
   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    0.11086E+00     260   0.42146E+00   0.18316E-01 
c  VelocityY    0.11086E+00     260   0.42146E+00   0.00000E+00 
c  VelocityZ    0.11086E+00     260   0.42146E+00   0.00000E+00 
c  Pressure     0.17633E-01     533   0.19022E-02   0.38764E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00012831                         16713


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2173          2.1033       -0.080838       -0.072524
v  Velocity[Y]                 -1.0507          3.7267         0.28302         0.23134
v  Velocity[Z]                 -2.4479          1.8045         0.14193       0.0015384
v  ǁVelocityǁ                0.0045086          4.0364         0.71171         0.68982
v  Pressure                    -688.89          6744.2          4577.3          3357.3
v  turbulent_viscosity      0.00036911          4.4643        0.029079        0.030406
v  CourantNb                  0.062399          174.16          14.884           10.71
v  FourierNb                   0.89313            2611          9.3313          5.3957
v  total_pressure           4.9931e+05      5.0674e+05      5.0458e+05      5.0336e+05
v  Local Time Step                0.01        0.079607        0.010084        0.010199


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9462          2665.9          24.215          16.106


 TIME FOR THE TIME STEP               35:        0.94034E+00

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


 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        -0.318448654E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282840E+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 0.21466E+01
   Friction velocity        uet   :  0.15263E-01 0.15900E+01
   Friction velocity        uk    :  0.15263E-01 0.15900E+01
   Dimensionless distance   yplus :  0.16097E+00 0.61969E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3618
   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    0.11399E+00     259   0.47469E+00   0.18021E-01 
c  VelocityY    0.11399E+00     259   0.47469E+00   0.00000E+00 
c  VelocityZ    0.11399E+00     259   0.47469E+00   0.00000E+00 
c  Pressure     0.17754E-01     480   0.18492E-02   0.38116E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00012512                         16718


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1972          2.1168       -0.082541       -0.072572
v  Velocity[Y]                 -1.0397          3.7803         0.28276         0.23145
v  Velocity[Z]                 -2.4625           1.859          0.1428        0.001479
v  ǁVelocityǁ                0.0042943          4.0911         0.71218          0.6909
v  Pressure                    -692.91          6858.6          4585.3          3362.7
v  turbulent_viscosity       0.0003165          5.0116        0.029221        0.030508
v  CourantNb                  0.078468          176.57          14.895          10.729
v  FourierNb                   0.90173          2592.9          9.3527          5.4054
v  total_pressure           4.9931e+05      5.0686e+05      5.0459e+05      5.0336e+05
v  Local Time Step                0.01        0.080248        0.010082        0.010195


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9761            2653          24.247          16.135


 TIME FOR THE TIME STEP               36:        0.91930E+00

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


 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        -0.760967782E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282850E+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 0.21935E+01
   Friction velocity        uet   :  0.17041E-01 0.16989E+01
   Friction velocity        uk    :  0.17041E-01 0.16989E+01
   Dimensionless distance   yplus :  0.16126E+00 0.61437E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3602
   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    0.11799E+00     257   0.51947E+00   0.17456E-01 
c  VelocityY    0.11799E+00     257   0.51947E+00   0.00000E+00 
c  VelocityZ    0.11799E+00     257   0.51947E+00   0.00000E+00 
c  Pressure     0.18053E-01     410   0.18606E-02   0.37862E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00011946                         16714


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3046          2.1393       -0.084185       -0.072521
v  Velocity[Y]                 -1.0216          3.7153         0.28236         0.23153
v  Velocity[Z]                  -2.501          2.0413         0.14352       0.0015237
v  ǁVelocityǁ                0.0026254          4.0277         0.71224         0.69144
v  Pressure                    -698.97            6980          4592.9          3367.8
v  turbulent_viscosity      0.00034869          5.6695        0.029355        0.030612
v  CourantNb                  0.012589          178.61          14.906          10.748
v  FourierNb                   0.90303          2927.9          9.3769          5.4171
v  total_pressure            4.993e+05      5.0698e+05      5.0459e+05      5.0337e+05
v  Local Time Step                0.01        0.085247        0.010082        0.010197


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9671          2994.3          24.283          16.165


 TIME FOR THE TIME STEP               37:        0.88607E+00

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


 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         0.914547429E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282825E+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 0.22680E+01
   Friction velocity        uet   :  0.95490E-02 0.18199E+01
   Friction velocity        uk    :  0.95490E-02 0.18199E+01
   Dimensionless distance   yplus :  0.12479E+00 0.61110E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3595
   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    0.12509E+00     255   0.58802E+00   0.17471E-01 
c  VelocityY    0.12509E+00     255   0.58802E+00   0.00000E+00 
c  VelocityZ    0.12509E+00     255   0.58802E+00   0.00000E+00 
c  Pressure     0.18260E-01     474   0.18282E-02   0.37413E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00011863                         16716


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2658          2.1404       -0.085876       -0.072526
v  Velocity[Y]                 -1.0759          3.7056         0.28202          0.2316
v  Velocity[Z]                 -2.5093          2.2258          0.1439       0.0014782
v  ǁVelocityǁ                 0.002831          4.0256         0.71221         0.69188
v  Pressure                    -704.04          7098.2          4603.2          3375.8
v  turbulent_viscosity        0.000341          6.4326        0.029492        0.030704
v  CourantNb                  0.090397          181.96           14.91          10.758
v  FourierNb                   0.90234          3734.1          9.4098          5.4265
v  total_pressure            4.993e+05       5.071e+05       5.046e+05      5.0338e+05
v  Local Time Step                0.01        0.081996        0.010084        0.010204


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8962          3807.3           24.32          16.184


 TIME FOR THE TIME STEP               38:        0.91771E+00

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


 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        -0.867015480E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282826E+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 0.26124E+01
   Friction velocity        uet   :  0.14783E-01 0.19393E+01
   Friction velocity        uk    :  0.14783E-01 0.19393E+01
   Dimensionless distance   yplus :  0.16554E+00 0.61028E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3570
   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    0.13456E+00     253   0.66801E+00   0.17725E-01 
c  VelocityY    0.13456E+00     253   0.66801E+00   0.00000E+00 
c  VelocityZ    0.13456E+00     253   0.66801E+00   0.00000E+00 
c  Pressure     0.18777E-01     422   0.18129E-02   0.37580E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00011521                         16715


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3007          2.1502       -0.087551       -0.072567
v  Velocity[Y]                 -1.0819          3.6863         0.28147         0.23169
v  Velocity[Z]                 -2.5353          2.4327         0.14413       0.0015085
v  ǁVelocityǁ                0.0019697          3.9975         0.71199         0.69208
v  Pressure                    -707.67            7218          4610.9          3381.8
v  turbulent_viscosity      0.00034507          7.2525        0.029627        0.030799
v  CourantNb                   0.11275           198.4          14.913          10.769
v  FourierNb                   0.89439          4204.8          9.4426          5.4419
v  total_pressure           4.9929e+05      5.0722e+05      5.0461e+05      5.0338e+05
v  Local Time Step                0.01        0.090195        0.010086         0.01021


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9041          4285.2          24.355          16.211


 TIME FOR THE TIME STEP               39:        0.89775E+00

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


 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        -0.124946889E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282858E+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 0.30442E+01
   Friction velocity        uet   :  0.97666E-02 0.20752E+01
   Friction velocity        uk    :  0.97666E-02 0.20752E+01
   Dimensionless distance   yplus :  0.12012E+00 0.60544E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3564
   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    0.14896E+00     253   0.75083E+00   0.17132E-01 
c  VelocityY    0.14896E+00     253   0.75083E+00   0.00000E+00 
c  VelocityZ    0.14896E+00     253   0.75083E+00   0.00000E+00 
c  Pressure     0.19093E-01     426   0.18026E-02   0.37326E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00011267                         16719


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3685          2.1626        -0.08916       -0.072634
v  Velocity[Y]                 -1.1581          3.6804         0.28087         0.23173
v  Velocity[Z]                 -2.5855          2.6388         0.14411       0.0015491
v  ǁVelocityǁ                0.0021788          3.9845         0.71162         0.69227
v  Pressure                    -712.18          7344.3          4616.1          3386.5
v  turbulent_viscosity      0.00033852          8.2526        0.029755        0.030875
v  CourantNb                 0.0048815          222.72          14.911          10.775
v  FourierNb                   0.91261          4774.2          9.4688           5.451
v  total_pressure           4.9929e+05      5.0734e+05      5.0462e+05      5.0339e+05
v  Local Time Step                0.01        0.099215        0.010089         0.01022


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9126          4863.2           24.38          16.226


 TIME FOR THE TIME STEP               40:        0.87276E+00

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


 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        -0.924013394E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282870E+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 0.35312E+01
   Friction velocity        uet   :  0.99414E-02 0.22203E+01
   Friction velocity        uk    :  0.99414E-02 0.22203E+01
   Dimensionless distance   yplus :  0.94911E-01 0.60748E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3545
   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    0.16922E+00     251   0.83136E+00   0.17770E-01 
c  VelocityY    0.16922E+00     251   0.83136E+00   0.00000E+00 
c  VelocityZ    0.16922E+00     251   0.83136E+00   0.00000E+00 
c  Pressure     0.19532E-01     444   0.17927E-02   0.37302E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00010816                         16717


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6738          2.1579       -0.090486       -0.072598
v  Velocity[Y]                 -1.1971          3.7161         0.28007         0.23175
v  Velocity[Z]                 -2.5735          2.9036         0.14399       0.0016108
v  ǁVelocityǁ                0.0022416          4.0813         0.71121         0.69242
v  Pressure                    -715.66          7463.3          4624.1          3393.4
v  turbulent_viscosity       0.0003277          9.3768        0.029889         0.03096
v  CourantNb                 0.0026683          249.55          14.909          10.783
v  FourierNb                   0.92382          5411.4          9.4981          5.4596
v  total_pressure           4.9928e+05      5.0746e+05      5.0462e+05      5.0339e+05
v  Local Time Step                0.01         0.10914        0.010092        0.010229


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9615          5509.5          24.407          16.242


 TIME FOR THE TIME STEP               41:        0.87520E+00

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


 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        -0.161148548E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282838E+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 0.40448E+01
   Friction velocity        uet   :  0.14272E-01 0.23646E+01
   Friction velocity        uk    :  0.14272E-01 0.23646E+01
   Dimensionless distance   yplus :  0.17571E+00 0.61458E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3532
   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    0.19554E+00     259   0.89490E+00   0.16910E-01 
c  VelocityY    0.19554E+00     259   0.89490E+00   0.00000E+00 
c  VelocityZ    0.19554E+00     259   0.89490E+00   0.00000E+00 
c  Pressure     0.20109E-01     388   0.17635E-02   0.37519E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00010728                         16716


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -3.037          2.1819       -0.091695       -0.072614
v  Velocity[Y]                 -1.2989          3.7061         0.27927         0.23187
v  Velocity[Z]                 -2.5757           3.186         0.14377       0.0016424
v  ǁVelocityǁ                0.0020506          4.6305          0.7107         0.69263
v  Pressure                    -718.39          7642.4          4632.7          3400.8
v  turbulent_viscosity      0.00031493          10.544        0.030026        0.031029
v  CourantNb                  0.012455          279.24          14.903          10.789
v  FourierNb                    0.9052          5391.4          9.5238          5.4709
v  total_pressure           4.9928e+05      5.0764e+05      5.0463e+05       5.034e+05
v  Local Time Step                0.01         0.12005        0.010095        0.010239


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9037          5499.3          24.427           16.26


 TIME FOR THE TIME STEP               42:        0.88406E+00

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


 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        -0.479672111E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282830E+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 0.46642E+01
   Friction velocity        uet   :  0.87293E-02 0.25256E+01
   Friction velocity        uk    :  0.87293E-02 0.25256E+01
   Dimensionless distance   yplus :  0.12174E+00 0.68083E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3528
   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    0.23347E+00     278   0.95006E+00   0.16625E-01 
c  VelocityY    0.23347E+00     278   0.95006E+00   0.00000E+00 
c  VelocityZ    0.23347E+00     278   0.95006E+00   0.00000E+00 
c  Pressure     0.20627E-01     425   0.17583E-02   0.37580E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00010283                         16717


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.4431          2.1614       -0.092626       -0.072684
v  Velocity[Y]                 -1.2963          3.7169         0.27832         0.23192
v  Velocity[Z]                 -2.6183          3.5198         0.14351       0.0016471
v  ǁVelocityǁ                0.0044761          5.2694         0.70989         0.69249
v  Pressure                    -732.51          7897.6          4640.7          3408.1
v  turbulent_viscosity      0.00031554          11.943        0.030177        0.031118
v  CourantNb                  0.075356          312.58          14.896          10.795
v  FourierNb                   0.89755          6094.9          9.5592          5.4812
v  total_pressure           4.9927e+05       5.079e+05      5.0464e+05      5.0341e+05
v  Local Time Step                0.01         0.07757        0.010099         0.01025


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6371          6214.1          24.455          16.276


 TIME FOR THE TIME STEP               43:        0.96632E+00

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


 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        -0.102406482E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282852E+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 0.53869E+01
   Friction velocity        uet   :  0.72455E-02 0.26982E+01
   Friction velocity        uk    :  0.72455E-02 0.26982E+01
   Dimensionless distance   yplus :  0.10297E+00 0.75592E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3517
   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    0.28535E+00     300   0.99286E+00   0.16926E-01 
c  VelocityY    0.28535E+00     300   0.99286E+00   0.00000E+00 
c  VelocityZ    0.28535E+00     300   0.99286E+00   0.00000E+00 
c  Pressure     0.21265E-01     412   0.17519E-02   0.37830E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      0.00010172                         16717


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.9363          2.1674        -0.09347       -0.072714
v  Velocity[Y]                 -1.6136          3.9322         0.27757         0.23199
v  Velocity[Z]                 -2.6459          3.9186         0.14316       0.0016927
v  ǁVelocityǁ                0.0049162          6.0133         0.70957         0.69267
v  Pressure                    -747.26            8189          4648.9            3415
v  turbulent_viscosity      0.00033667          13.531        0.030337        0.031195
v  CourantNb                  0.043153          350.05          14.882          10.795
v  FourierNb                   0.89057          7777.1          9.6139          5.4952
v  total_pressure           4.9925e+05      5.0819e+05      5.0465e+05      5.0342e+05
v  Local Time Step                0.01        0.075978        0.010105        0.010271


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5875          7908.9          24.496           16.29


 TIME FOR THE TIME STEP               44:        0.95565E+00

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


 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        -0.655033077E-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 : -0.00000E+00 0.62414E+01
   Friction velocity        uet   :  0.14301E-01 0.28982E+01
   Friction velocity        uk    :  0.14301E-01 0.28982E+01
   Dimensionless distance   yplus :  0.14194E+00 0.84219E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3509
   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    0.35247E+00     325   0.10215E+01   0.16882E-01 
c  VelocityY    0.35247E+00     325   0.10215E+01   0.00000E+00 
c  VelocityZ    0.35247E+00     325   0.10215E+01   0.00000E+00 
c  Pressure     0.22348E-01     393   0.17862E-02   0.38804E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      9.8076e-05                         16717


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -4.4952          2.1481       -0.094116       -0.072708
v  Velocity[Y]                 -1.8462          4.4359         0.27665         0.23197
v  Velocity[Z]                 -2.6335          4.3172         0.14279       0.0017731
v  ǁVelocityǁ                0.0032203          6.8425         0.70915         0.69295
v  Pressure                    -761.95          8517.4          4656.9          3422.1
v  turbulent_viscosity      0.00031642          15.403        0.030526        0.031281
v  CourantNb                  0.030274          391.87          14.881          10.802
v  FourierNb                   0.89768          8846.7          9.6631          5.5074
v  total_pressure           4.9924e+05      5.0852e+05      5.0466e+05      5.0342e+05
v  Local Time Step                0.01         0.08202        0.010108        0.010284


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5703          8992.7          24.544          16.309


 TIME FOR THE TIME STEP               45:        0.99961E+00

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


 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        -0.667831216E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282867E+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 0.72023E+01
   Friction velocity        uet   :  0.10020E-01 0.31006E+01
   Friction velocity        uk    :  0.10020E-01 0.31006E+01
   Dimensionless distance   yplus :  0.16983E+00 0.93654E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3503
   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    0.44477E+00     353   0.10428E+01   0.16764E-01 
c  VelocityY    0.44477E+00     353   0.10428E+01   0.00000E+00 
c  VelocityZ    0.44477E+00     353   0.10428E+01   0.00000E+00 
c  Pressure     0.22927E-01     420   0.17590E-02   0.38829E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      9.6576e-05                         16719


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -5.0909            2.14       -0.094641       -0.072772
v  Velocity[Y]                 -1.8504          5.0384         0.27599         0.23201
v  Velocity[Z]                 -3.0394          4.8057         0.14224       0.0018113
v  ǁVelocityǁ                0.0037711          7.7808         0.70876         0.69287
v  Pressure                    -776.84          8885.4          4666.6          3430.3
v  turbulent_viscosity      0.00026379          17.507        0.030733        0.031383
v  CourantNb                   0.02605          443.28          14.876          10.808
v  FourierNb                   0.90491          8896.2          9.7035          5.5193
v  total_pressure           4.9922e+05      5.0889e+05      5.0467e+05      5.0343e+05
v  Local Time Step                0.01        0.080877        0.010107         0.01028


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4918          9055.5          24.579          16.327


 TIME FOR THE TIME STEP               46:        0.10655E+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        -0.134037289E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282845E+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 0.82888E+01
   Friction velocity        uet   :  0.12848E-01 0.33068E+01
   Friction velocity        uk    :  0.12848E-01 0.33068E+01
   Dimensionless distance   yplus :  0.19209E+00 0.10404E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3499
   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    0.56674E+00     379   0.10542E+01   0.17088E-01 
c  VelocityY    0.56674E+00     379   0.10542E+01   0.00000E+00 
c  VelocityZ    0.56674E+00     379   0.10542E+01   0.00000E+00 
c  Pressure     0.23580E-01     421   0.17770E-02   0.38951E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      9.4233e-05                         16718


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -5.8136          2.1558        -0.09504       -0.072769
v  Velocity[Y]                 -2.3001          5.6744         0.27527           0.232
v  Velocity[Z]                 -3.5653          5.3779         0.14172       0.0019133
v  ǁVelocityǁ                0.0045228          8.8718         0.70851         0.69262
v  Pressure                    -785.14          9306.7          4676.1          3437.8
v  turbulent_viscosity       0.0002772          19.848        0.030945        0.031466
v  CourantNb                  0.036678          496.47          14.875          10.811
v  FourierNb                   0.89486           10069          9.7669          5.5353
v  total_pressure           4.9921e+05      5.0931e+05      5.0468e+05      5.0344e+05
v  Local Time Step                0.01        0.081018        0.010104        0.010272


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7433           10245          24.642          16.346


 TIME FOR THE TIME STEP               47:        0.11118E+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        -0.122027206E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282858E+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 0.95749E+01
   Friction velocity        uet   :  0.97833E-02 0.35455E+01
   Friction velocity        uk    :  0.97833E-02 0.35455E+01
   Dimensionless distance   yplus :  0.16929E+00 0.11600E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3487
   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    0.72152E+00     410   0.10656E+01   0.17282E-01 
c  VelocityY    0.72152E+00     410   0.10656E+01   0.00000E+00 
c  VelocityZ    0.72152E+00     410   0.10656E+01   0.00000E+00 
c  Pressure     0.24806E-01     356   0.17797E-02   0.39946E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      9.2281e-05                         16718


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -6.6242          2.2344       -0.095478       -0.072876
v  Velocity[Y]                 -2.3802          6.4404         0.27495         0.23197
v  Velocity[Z]                 -4.1193          5.9939         0.14133       0.0019659
v  ǁVelocityǁ                0.0042877          10.116         0.70876         0.69282
v  Pressure                    -803.93          9771.3          4684.7          3444.8
v  turbulent_viscosity      0.00029215          22.599        0.031205        0.031555
v  CourantNb                   0.02878          556.73          14.878          10.813
v  FourierNb                   0.88831           11462          9.8389          5.5496
v  total_pressure            4.992e+05      5.0977e+05      5.0468e+05      5.0344e+05
v  Local Time Step                0.01        0.082697        0.010103        0.010268


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8292           11657          24.717          16.362


 TIME FOR THE TIME STEP               48:        0.11382E+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        -0.331411567E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282481E+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 0.11031E+02
   Friction velocity        uet   :  0.57794E-02 0.37913E+01
   Friction velocity        uk    :  0.57794E-02 0.37913E+01
   Dimensionless distance   yplus :  0.99882E-01 0.12920E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3474
   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    0.92731E+00     449   0.10680E+01   0.17670E-01 
c  VelocityY    0.92731E+00     449   0.10680E+01   0.00000E+00 
c  VelocityZ    0.92731E+00     449   0.10680E+01   0.00000E+00 
c  Pressure     0.26205E-01     377   0.18244E-02   0.41094E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      8.9517e-05                         16720


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -7.5525          2.5612        -0.09582       -0.072879
v  Velocity[Y]                 -2.9463          7.2758         0.27435         0.23192
v  Velocity[Z]                 -4.7907           6.737         0.14083       0.0020241
v  ǁVelocityǁ                0.0052569          11.529         0.70885         0.69254
v  Pressure                    -818.52           10298          4687.8          3448.2
v  turbulent_viscosity      0.00023816           25.69        0.031497         0.03167
v  CourantNb                  0.037011          623.94          14.894          10.823
v  FourierNb                   0.87985           14687           9.945          5.5664
v  total_pressure           4.9918e+05       5.103e+05      5.0469e+05      5.0345e+05
v  Local Time Step                0.01        0.082404        0.010104        0.010273


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9274           14903          24.839          16.389


 TIME FOR THE TIME STEP               49:        0.12194E+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        -0.389758902E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282907E+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 0.12713E+02
   Friction velocity        uet   :  0.92842E-02 0.40589E+01
   Friction velocity        uk    :  0.92842E-02 0.40589E+01
   Dimensionless distance   yplus :  0.10634E+00 0.14407E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3471
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          5 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:    0.87895E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.11950E+01     477   0.10707E+01   0.19182E-01 
c  VelocityY    0.11950E+01     477   0.10707E+01   0.00000E+00 
c  VelocityZ    0.11950E+01     477   0.10707E+01   0.00000E+00 
c  Pressure     0.27246E-01     371   0.18174E-02   0.41592E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      8.8494e-05                         16721


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -8.562          2.8539        -0.09614       -0.072969
v  Velocity[Y]                 -3.0657          8.2717         0.27382         0.23189
v  Velocity[Z]                 -5.4439          7.5425         0.14031       0.0020659
v  ǁVelocityǁ                 0.003027          13.091         0.70873         0.69187
v  Pressure                    -833.82           10889          4695.7          3454.3
v  turbulent_viscosity      0.00022455          29.271        0.031805        0.031767
v  CourantNb                  0.006662          698.97          14.906          10.826
v  FourierNb                   0.87287           16734          10.037          5.5893
v  total_pressure           4.9917e+05      5.1089e+05       5.047e+05      5.0345e+05
v  Local Time Step                0.01        0.082868        0.010107        0.010287


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.935           16973          24.944          16.415


 TIME FOR THE TIME STEP               50:        0.12326E+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        -0.138703167E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282715E+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 0.14582E+02
   Friction velocity        uet   :  0.12674E-01 0.43218E+01
   Friction velocity        uk    :  0.12674E-01 0.43218E+01
   Dimensionless distance   yplus :  0.13985E+00 0.16018E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3466
   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    0.15461E+01     504   0.10707E+01   0.20067E-01 
c  VelocityY    0.15461E+01     504   0.10707E+01   0.00000E+00 
c  VelocityZ    0.15461E+01     504   0.10707E+01   0.00000E+00 
c  Pressure     0.28910E-01     363   0.18767E-02   0.42938E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      8.6626e-05                         16720


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -9.7618          3.2315       -0.096509       -0.073046
v  Velocity[Y]                 -3.8054           9.332         0.27353         0.23182
v  Velocity[Z]                 -6.3117          8.4955         0.13982       0.0021087
v  ǁVelocityǁ                0.0038238          14.907         0.70929         0.69162
v  Pressure                    -855.35           11574          4701.7          3458.9
v  turbulent_viscosity      0.00016862          33.185        0.032128        0.031859
v  CourantNb                 0.0065712           780.1          14.918          10.826
v  FourierNb                   0.86638           18951           10.14            5.61
v  total_pressure           4.9914e+05      5.1157e+05       5.047e+05      5.0346e+05
v  Local Time Step                0.01        0.082668         0.01011        0.010299


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8972           19215          25.059          16.436


 TIME FOR THE TIME STEP               51:        0.12285E+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        -0.609709287E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282655E+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 0.16800E+02
   Friction velocity        uet   :  0.95360E-02 0.33527E+01
   Friction velocity        uk    :  0.95360E-02 0.33527E+01
   Dimensionless distance   yplus :  0.98542E-01 0.17885E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3463
   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    0.21749E+01     615   0.10304E+01   0.19462E-01 
c  VelocityY    0.21749E+01     615   0.10304E+01   0.00000E+00 
c  VelocityZ    0.21749E+01     615   0.10304E+01   0.00000E+00 
c  Pressure     0.30621E-01     352   0.19385E-02   0.44197E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      8.5266e-05                         16722


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -8.5268          3.7153       -0.096681       -0.073095
v  Velocity[Y]                 -4.4372          9.7526         0.27295          0.2318
v  Velocity[Z]                 -5.9377          9.5151         0.13947       0.0021897
v  ǁVelocityǁ                0.0034896           14.25         0.70939         0.69108
v  Pressure                    -925.85           12341          4703.6          3461.1
v  turbulent_viscosity       0.0001877          37.775        0.032532        0.031995
v  CourantNb                 0.0028741          871.36          14.944          10.834
v  FourierNb                   0.86347           19104           10.22          5.6282
v  total_pressure           4.9907e+05      5.1234e+05       5.047e+05      5.0346e+05
v  Local Time Step                0.01        0.083263        0.010113        0.010314


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8635           19397          25.164          16.462


 TIME FOR THE TIME STEP               52:        0.14201E+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        -0.183239895E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282485E+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 0.14460E+02
   Friction velocity        uet   :  0.87552E-02 0.43957E+01
   Friction velocity        uk    :  0.87552E-02 0.43957E+01
   Dimensionless distance   yplus :  0.12863E+00 0.15914E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3459
   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    0.18592E+01     523   0.10646E+01   0.26316E-01 
c  VelocityY    0.18592E+01     523   0.10646E+01   0.00000E+00 
c  VelocityZ    0.18592E+01     523   0.10646E+01   0.00000E+00 
c  Pressure     0.32328E-01     403   0.18565E-02   0.45312E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      8.2669e-05                         16720


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -11.853          3.9735       -0.097046       -0.073119
v  Velocity[Y]                 -4.5649          11.578           0.273          0.2318
v  Velocity[Z]                  -7.456          10.572         0.13907       0.0021504
v  ǁVelocityǁ                0.0016841           18.17         0.70968          0.6902
v  Pressure                      -1132           13186          4712.2          3467.2
v  turbulent_viscosity      0.00019612          32.093        0.032733        0.032095
v  CourantNb                 0.0043974          1072.1          14.969          10.839
v  FourierNb                   0.88544           16803          10.241          5.6504
v  total_pressure           4.9887e+05      5.1319e+05      5.0471e+05      5.0347e+05
v  Local Time Step                0.01         0.09159        0.010121         0.01034


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8854           17250          25.209          16.489


 TIME FOR THE TIME STEP               53:        0.12171E+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         0.679677766E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282933E+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 0.20644E+02
   Friction velocity        uet   :  0.85821E-02 0.37105E+01
   Friction velocity        uk    :  0.85821E-02 0.37105E+01
   Dimensionless distance   yplus :  0.12982E+00 0.21024E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3443
   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    0.33759E+01     695   0.10271E+01   0.23436E-01 
c  VelocityY    0.33759E+01     695   0.10271E+01   0.00000E+00 
c  VelocityZ    0.33759E+01     695   0.10271E+01   0.00000E+00 
c  Pressure     0.35688E-01     333   0.20230E-02   0.48480E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      8.2086e-05                         16719


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -10.409          4.8157       -0.097182       -0.073115
v  Velocity[Y]                 -5.5954          12.202         0.27232         0.23169
v  Velocity[Z]                 -7.2019          12.012         0.13903       0.0021946
v  ǁVelocityǁ                0.0016207          17.442         0.71047         0.68984
v  Pressure                    -1359.4           14160          4713.1          3468.1
v  turbulent_viscosity      0.00023047          46.416        0.033284        0.032185
v  CourantNb                  0.031452          1113.3          14.993           10.84
v  FourierNb                   0.91115           26468          10.505          5.6809
v  total_pressure           4.9864e+05      5.1416e+05      5.0471e+05      5.0347e+05
v  Local Time Step                0.01         0.10075         0.01013        0.010372


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9434           26825          25.498          16.521


 TIME FOR THE TIME STEP               54:        0.14271E+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        -0.660366738E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282475E+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 0.17856E+02
   Friction velocity        uet   :  0.49787E-02 0.39364E+01
   Friction velocity        uk    :  0.49787E-02 0.39364E+01
   Dimensionless distance   yplus :  0.70251E-01 0.18758E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3439
   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    0.31175E+01     636   0.10233E+01   0.25275E-01 
c  VelocityY    0.31175E+01     636   0.10233E+01   0.00000E+00 
c  VelocityZ    0.31175E+01     636   0.10233E+01   0.00000E+00 
c  Pressure     0.37177E-01     317   0.20213E-02   0.48908E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      8.0398e-05                         16720


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -12.416          4.9282       -0.097577       -0.073208
v  Velocity[Y]                 -6.2634           13.59         0.27199         0.23167
v  Velocity[Z]                 -8.4438          13.014         0.13895       0.0021516
v  ǁVelocityǁ                0.0018752          20.252         0.71062         0.68899
v  Pressure                    -1573.1           15209            4710          3465.9
v  turbulent_viscosity      0.00026766          39.335        0.033559        0.032346
v  CourantNb                  0.050586          1372.9          15.039           10.85
v  FourierNb                   0.92454           20678          10.484          5.7065
v  total_pressure           4.9843e+05      5.1521e+05      5.0471e+05      5.0347e+05
v  Local Time Step                0.01         0.11082        0.010138        0.010403


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9245           21246          25.524          16.556


 TIME FOR THE TIME STEP               55:        0.14354E+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         0.577554709E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282641E+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 0.20618E+02
   Friction velocity        uet   :  0.10751E-01 0.40528E+01
   Friction velocity        uk    :  0.10751E-01 0.40528E+01
   Dimensionless distance   yplus :  0.10205E+00 0.21003E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3413
   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    0.40213E+01     707   0.10203E+01   0.26433E-01 
c  VelocityY    0.40213E+01     707   0.10203E+01   0.00000E+00 
c  VelocityZ    0.40213E+01     707   0.10203E+01   0.00000E+00 
c  Pressure     0.40228E-01     352   0.20415E-02   0.51152E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step       7.924e-05                         16719


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -13.199          5.5093       -0.097877       -0.073283
v  Velocity[Y]                 -7.2873          15.148         0.27161         0.23163
v  Velocity[Z]                 -9.3037          14.313           0.139       0.0021989
v  ǁVelocityǁ                0.0013326          22.141         0.71156         0.68855
v  Pressure                    -1804.9           16376          4714.7          3469.4
v  turbulent_viscosity      0.00013636           45.34        0.033983        0.032447
v  CourantNb                  0.031136          1550.4          15.066          10.849
v  FourierNb                   0.93954           26547          10.677          5.7326
v  total_pressure            4.982e+05      5.1638e+05      5.0471e+05      5.0347e+05
v  Local Time Step                0.01         0.11303        0.010146        0.010431


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.952           27178          25.743          16.582


 TIME FOR THE TIME STEP               56:        0.14742E+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        -0.565563072E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282784E+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 0.22583E+02
   Friction velocity        uet   :  0.13787E-01 0.43628E+01
   Friction velocity        uk    :  0.13787E-01 0.43628E+01
   Dimensionless distance   yplus :  0.12741E+00 0.22569E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3396
   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    0.49407E+01     745   0.10171E+01   0.25972E-01 
c  VelocityY    0.49407E+01     745   0.10171E+01   0.00000E+00 
c  VelocityZ    0.49407E+01     745   0.10171E+01   0.00000E+00 
c  Pressure     0.43745E-01     343   0.22538E-02   0.53661E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      7.6921e-05                         16720


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -14.498          6.2731       -0.098304       -0.073427
v  Velocity[Y]                 -8.0978          17.008         0.27143          0.2316
v  Velocity[Z]                 -10.057          15.893         0.13893       0.0020862
v  ǁVelocityǁ                0.0022083          24.507         0.71245         0.68837
v  Pressure                      -2026           17687          4717.9          3472.1
v  turbulent_viscosity      0.00014128          49.569        0.034494        0.032603
v  CourantNb                  0.011179          1746.9          15.116          10.861
v  FourierNb                    0.9504           25919          10.784           5.765
v  total_pressure           4.9797e+05      5.1769e+05      5.0472e+05      5.0347e+05
v  Local Time Step                0.01         0.11541        0.010151        0.010449


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8305           26638            25.9          16.626


 TIME FOR THE TIME STEP               57:        0.16165E+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        -0.698812108E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282712E+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 0.25168E+02
   Friction velocity        uet   :  0.63099E-02 0.28438E+01
   Friction velocity        uk    :  0.63099E-02 0.28438E+01
   Dimensionless distance   yplus :  0.11502E+00 0.24597E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3385
   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    0.61181E+01     867   0.10156E+01   0.65482E-01 
c  VelocityY    0.61181E+01     867   0.10156E+01   0.00000E+00 
c  VelocityZ    0.61181E+01     867   0.10156E+01   0.00000E+00 
c  Pressure     0.47724E-01     360   0.23510E-02   0.56384E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      7.6534e-05                         16721


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -15.789          6.8949       -0.099047       -0.073609
v  Velocity[Y]                 -9.1487          18.598         0.27164         0.23161
v  Velocity[Z]                 -11.442          17.899         0.13927       0.0020268
v  ǁVelocityǁ                0.0036185          26.055         0.71504         0.68894
v  Pressure                    -2258.7           19037          4725.6          3477.6
v  turbulent_viscosity       0.0001521          55.299        0.035013        0.032781
v  CourantNb                  0.013637          1957.4           15.17          10.876
v  FourierNb                   0.94564           28880          10.909          5.7956
v  total_pressure           4.9774e+05      5.1904e+05      5.0473e+05      5.0348e+05
v  Local Time Step                0.01         0.11098         0.01015        0.010445


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.852           29685          26.079          16.672


 TIME FOR THE TIME STEP               58:        0.18069E+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        -0.109481722E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282997E+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 0.27032E+02
   Friction velocity        uet   :  0.10560E-01 0.29133E+01
   Friction velocity        uk    :  0.10560E-01 0.29133E+01
   Dimensionless distance   yplus :  0.15623E+00 0.26036E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3350
   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    0.71543E+01     803   0.10191E+01   0.50360E-01 
c  VelocityY    0.71543E+01     803   0.10191E+01   0.00000E+00 
c  VelocityZ    0.71543E+01     803   0.10191E+01   0.00000E+00 
c  Pressure     0.50672E-01     339   0.23951E-02   0.57543E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      7.5176e-05                         16730


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -16.871          7.7393       -0.099662       -0.073761
v  Velocity[Y]                 -10.297          20.593         0.27126         0.23163
v  Velocity[Z]                 -12.594          19.486         0.13885       0.0018334
v  ǁVelocityǁ                 0.003894          28.458         0.71719         0.68968
v  Pressure                    -2497.4           20524          4728.1          3480.6
v  turbulent_viscosity      0.00027882           59.54        0.035648         0.03306
v  CourantNb                  0.004273          2378.1          15.261          10.907
v  FourierNb                     0.946           31165          11.069          5.8328
v  total_pressure            4.975e+05      5.2052e+05      5.0473e+05      5.0348e+05
v  Local Time Step                0.01        0.083749        0.010138        0.010407


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6854           32126           26.33           16.74


 TIME FOR THE TIME STEP               59:        0.15858E+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        -0.188980594E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282368E+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 0.29719E+02
   Friction velocity        uet   :  0.10839E-01 0.31055E+01
   Friction velocity        uk    :  0.10839E-01 0.31055E+01
   Dimensionless distance   yplus :  0.12393E+00 0.28085E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3318
   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    0.87775E+01     828   0.10198E+01   0.49789E-01 
c  VelocityY    0.87775E+01     828   0.10198E+01   0.00000E+00 
c  VelocityZ    0.87775E+01     828   0.10198E+01   0.00000E+00 
c  Pressure     0.57013E-01     428   0.25117E-02   0.62039E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step        7.41e-05                         16738


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -19.283          8.6889        -0.10105       -0.073905
v  Velocity[Y]                 -11.264          22.939          0.2704         0.23167
v  Velocity[Z]                 -14.026          21.973         0.13904       0.0018252
v  ǁVelocityǁ                0.0032438          31.586         0.71992         0.69046
v  Pressure                    -2750.2           22225          4738.8          3489.6
v  turbulent_viscosity      0.00034396          65.827        0.036366        0.033326
v  CourantNb                  0.026178            2643          15.347          10.938
v  FourierNb                   0.95364           38695          11.317          5.8712
v  total_pressure           4.9725e+05      5.2222e+05      5.0474e+05      5.0349e+05
v  Local Time Step                0.01        0.083978        0.010121        0.010351


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8716           39766          26.664           16.81


 TIME FOR THE TIME STEP               60:        0.16426E+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        -0.379464143E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282977E+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 0.33130E+02
   Friction velocity        uet   :  0.10940E-01 0.33885E+01
   Friction velocity        uk    :  0.10940E-01 0.33885E+01
   Dimensionless distance   yplus :  0.16983E+00 0.30644E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3310
   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    0.10885E+02     858   0.10178E+01   0.52307E-01 
c  VelocityY    0.10885E+02     858   0.10178E+01   0.00000E+00 
c  VelocityZ    0.10885E+02     858   0.10178E+01   0.00000E+00 
c  Pressure     0.61491E-01     351   0.26029E-02   0.63956E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step       7.306e-05                         16735


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -21.294          9.8088        -0.10284       -0.074034
v  Velocity[Y]                 -12.543          25.682         0.26969         0.23168
v  Velocity[Z]                 -15.652          24.298         0.13933       0.0017631
v  ǁVelocityǁ                0.0064709          35.165         0.72385         0.69187
v  Pressure                    -2990.4           24103          4747.7          3496.7
v  turbulent_viscosity      0.00038001          73.026        0.037177        0.033605
v  CourantNb                   0.01966          2960.7          15.447          10.971
v  FourierNb                   0.95806           42973          11.551          5.9092
v  total_pressure           4.9701e+05       5.241e+05      5.0475e+05       5.035e+05
v  Local Time Step                0.01        0.083823        0.010104        0.010293


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7902           44175          26.998           16.88


 TIME FOR THE TIME STEP               61:        0.17063E+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        -0.132221446E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282725E+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 0.36990E+02
   Friction velocity        uet   :  0.12670E-01 0.37032E+01
   Friction velocity        uk    :  0.12670E-01 0.37032E+01
   Dimensionless distance   yplus :  0.20007E+00 0.33490E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3312
   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    0.13648E+02     883   0.10156E+01   0.66400E-01 
c  VelocityY    0.13648E+02     883   0.10156E+01   0.00000E+00 
c  VelocityZ    0.13648E+02     883   0.10156E+01   0.00000E+00 
c  Pressure     0.67459E-01     409   0.27342E-02   0.66898E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      7.1207e-05                         16728


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -23.962          10.895        -0.10499       -0.074219
v  Velocity[Y]                 -14.125          28.654          0.2691         0.23165
v  Velocity[Z]                 -17.462          27.149         0.13978       0.0017207
v  ǁVelocityǁ                 0.006864          39.075         0.72904          0.6939
v  Pressure                    -3241.2           26220          4763.9          3509.7
v  turbulent_viscosity      0.00022959          81.407        0.038066         0.03394
v  CourantNb                  0.099817          3322.5          15.583          11.016
v  FourierNb                   0.96656           42571           11.73           5.956
v  total_pressure           4.9676e+05      5.2622e+05      5.0476e+05      5.0351e+05
v  Local Time Step                0.01        0.084596        0.010093        0.010254


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7208           43920          27.313          16.972


 TIME FOR THE TIME STEP               62:        0.18521E+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        -0.719404273E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283048E+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 0.41266E+02
   Friction velocity        uet   :  0.12904E-01 0.40459E+01
   Friction velocity        uk    :  0.12904E-01 0.40459E+01
   Dimensionless distance   yplus :  0.16944E+00 0.36589E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3297
   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    0.16986E+02     891   0.10140E+01   0.75083E-01 
c  VelocityY    0.16986E+02     891   0.10140E+01   0.00000E+00 
c  VelocityZ    0.16986E+02     891   0.10140E+01   0.00000E+00 
c  Pressure     0.74270E-01     302   0.28662E-02   0.69990E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      7.0366e-05                         16731


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -26.662          12.265        -0.10762         -0.0744
v  Velocity[Y]                 -15.706          32.061          0.2679         0.23148
v  Velocity[Z]                 -19.522          30.274         0.14038       0.0017401
v  ǁVelocityǁ                0.0062593            43.5         0.73452         0.69604
v  Pressure                    -3517.5           28566          4764.1          3511.1
v  turbulent_viscosity      0.00022566           90.41        0.039208        0.034387
v  CourantNb                  0.014775            3725          15.752          11.077
v  FourierNb                   0.95041           47319          12.035          6.0218
v  total_pressure           4.9648e+05      5.2857e+05      5.0476e+05      5.0351e+05
v  Local Time Step                0.01        0.086051        0.010085        0.010228


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7913           48838          27.787          17.099


 TIME FOR THE TIME STEP               63:        0.16704E+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        -0.758498152E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282286E+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 0.46113E+02
   Friction velocity        uet   :  0.11230E-01 0.44279E+01
   Friction velocity        uk    :  0.11230E-01 0.44279E+01
   Dimensionless distance   yplus :  0.17734E+00 0.40044E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3291
   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    0.21277E+02     914   0.10140E+01   0.90155E-01 
c  VelocityY    0.21277E+02     914   0.10140E+01   0.00000E+00 
c  VelocityZ    0.21277E+02     914   0.10140E+01   0.00000E+00 
c  Pressure     0.81861E-01     337   0.30038E-02   0.73062E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      6.9744e-05                         16739


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -29.791          13.719        -0.11079        -0.07452
v  Velocity[Y]                 -17.703          35.754         0.26641         0.23139
v  Velocity[Z]                 -21.863          33.709         0.14062       0.0016326
v  ǁVelocityǁ                0.0082631          48.502         0.74169         0.69886
v  Pressure                    -3804.4           31190          4768.9          3515.8
v  turbulent_viscosity      0.00030473          100.77        0.040417        0.034861
v  CourantNb                  0.020025          4176.4          15.929          11.138
v  FourierNb                   0.84436           52738          12.359          6.0888
v  total_pressure            4.962e+05      5.3119e+05      5.0477e+05      5.0352e+05
v  Local Time Step                0.01        0.094656         0.01008         0.01021


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8777           54443          28.288          17.227


 TIME FOR THE TIME STEP               64:        0.16970E+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        -0.363178611E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283040E+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 0.51571E+02
   Friction velocity        uet   :  0.20070E-01 0.48508E+01
   Friction velocity        uk    :  0.20070E-01 0.48508E+01
   Dimensionless distance   yplus :  0.16360E+00 0.43868E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3284
   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    0.26486E+02     917   0.10126E+01   0.11931E+00 
c  VelocityY    0.26486E+02     917   0.10126E+01   0.00000E+00 
c  VelocityZ    0.26486E+02     917   0.10126E+01   0.00000E+00 
c  Pressure     0.89908E-01     367   0.31494E-02   0.75759E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      6.8256e-05                         16734


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -33.221          15.351         -0.1145       -0.074749
v  Velocity[Y]                 -19.742          39.968         0.26477         0.23132
v  Velocity[Z]                 -24.516          37.573         0.14016       0.0015534
v  ǁVelocityǁ                0.0045603          54.105         0.74971         0.70253
v  Pressure                    -4095.3           34141          4784.6          3527.9
v  turbulent_viscosity       0.0003951             112        0.041881        0.035427
v  CourantNb                  0.016618          4681.3          16.152          11.215
v  FourierNb                   0.85094           65985          12.849          6.1797
v  total_pressure            4.959e+05      5.3414e+05      5.0478e+05      5.0353e+05
v  Local Time Step                0.01         0.10412        0.010072        0.010188


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9517           67903          29.002          17.394


 TIME FOR THE TIME STEP               65:        0.18830E+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        -0.615298630E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282363E+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 0.57695E+02
   Friction velocity        uet   :  0.15982E-01 0.53175E+01
   Friction velocity        uk    :  0.15982E-01 0.53175E+01
   Dimensionless distance   yplus :  0.13777E+00 0.48089E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3260
   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    0.33142E+02     948   0.10121E+01   0.14772E+00 
c  VelocityY    0.33142E+02     948   0.10121E+01   0.00000E+00 
c  VelocityZ    0.33142E+02     948   0.10121E+01   0.00000E+00 
c  Pressure     0.99621E-01     329   0.33008E-02   0.78983E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      6.0438e-05                         16747


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -37.046          17.219        -0.11868       -0.074825
v  Velocity[Y]                 -22.158          44.597         0.26153          0.2311
v  Velocity[Z]                  -27.35           41.97         0.13908        0.001558
v  ǁVelocityǁ                0.0086921          60.106            0.76         0.70787
v  Pressure                    -4386.4           37423          4784.2            3530
v  turbulent_viscosity      0.00023433          124.82        0.043463        0.036065
v  CourantNb                  0.013396          5247.6            16.4          11.312
v  FourierNb                   0.86502           73542          13.277          6.2713
v  total_pressure           4.9561e+05      5.3742e+05      5.0478e+05      5.0353e+05
v  Local Time Step                0.01        0.083756        0.010064        0.010164


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7478           75698          29.677          17.583


 TIME FOR THE TIME STEP               66:        0.19365E+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        -0.974480304E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282308E+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 0.64324E+02
   Friction velocity        uet   :  0.16087E-01 0.58144E+01
   Friction velocity        uk    :  0.16087E-01 0.58144E+01
   Dimensionless distance   yplus :  0.14846E+00 0.52583E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3238
   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    0.41288E+02     951   0.10115E+01   0.18002E+00 
c  VelocityY    0.41288E+02     951   0.10115E+01   0.00000E+00 
c  VelocityZ    0.41288E+02     951   0.10115E+01   0.00000E+00 
c  Pressure     0.11048E+00     346   0.34160E-02   0.82083E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      5.3596e-05                         16749


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -41.414          19.228        -0.12318       -0.075012
v  Velocity[Y]                 -25.017          49.713         0.25813         0.23095
v  Velocity[Z]                  -30.57            46.7         0.13662       0.0015335
v  ǁVelocityǁ                 0.008913          66.867         0.77139         0.71354
v  Pressure                    -4710.2           41065            4793          3537.3
v  turbulent_viscosity      0.00025548           138.8        0.045336        0.036844
v  CourantNb                  0.003622          5875.1          16.699          11.436
v  FourierNb                   0.88741           72752          13.648          6.3819
v  total_pressure           4.9529e+05      5.4107e+05      5.0479e+05      5.0354e+05
v  Local Time Step                0.01        0.083519        0.010054        0.010139


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6845           75171          30.347          17.818


 TIME FOR THE TIME STEP               67:        0.19309E+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        -0.758686087E-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 : -0.00000E+00 0.71802E+02
   Friction velocity        uet   :  0.21235E-01 0.63661E+01
   Friction velocity        uk    :  0.21235E-01 0.63661E+01
   Dimensionless distance   yplus :  0.21163E+00 0.57572E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3207
   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    0.51370E+02     970   0.10106E+01   0.25057E+00 
c  VelocityY    0.51370E+02     970   0.10106E+01   0.00000E+00 
c  VelocityZ    0.51370E+02     970   0.10106E+01   0.00000E+00 
c  Pressure     0.12202E+00     278   0.36129E-02   0.84709E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.7176e-05                         16748


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -46.197          21.415         -0.1278       -0.075096
v  Velocity[Y]                  -27.71           55.48          0.2535         0.23075
v  Velocity[Z]                 -34.194          52.064         0.13253       0.0015399
v  ǁVelocityǁ                0.0072428          74.433         0.78493         0.72138
v  Pressure                    -5018.7           45155          4792.3          3538.3
v  turbulent_viscosity      0.00035452          154.34        0.047308        0.037676
v  CourantNb                  0.074437            6575          17.036          11.576
v  FourierNb                   0.90763           80921          14.153          6.4992
v  total_pressure           4.9498e+05      5.4515e+05      5.0479e+05      5.0354e+05
v  Local Time Step                0.01        0.083483        0.010049        0.010128


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9076           83632          31.189          18.075


 TIME FOR THE TIME STEP               68:        0.19446E+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        -0.286821155E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282255E+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 0.80171E+02
   Friction velocity        uet   :  0.14145E-01 0.69740E+01
   Friction velocity        uk    :  0.14145E-01 0.69740E+01
   Dimensionless distance   yplus :  0.20410E+00 0.63069E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3162
   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    0.64082E+02     988   0.10099E+01   0.30265E+00 
c  VelocityY    0.64082E+02     988   0.10099E+01   0.00000E+00 
c  VelocityZ    0.64082E+02     988   0.10099E+01   0.00000E+00 
c  Pressure     0.13572E+00     388   0.37629E-02   0.87689E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.1961e-05                         16744


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -51.334          24.209        -0.13266       -0.075299
v  Velocity[Y]                 -31.208          62.028         0.24854          0.2306
v  Velocity[Z]                  -38.34          58.151         0.12643       0.0017159
v  ǁVelocityǁ                0.0075555          83.148         0.80126         0.73117
v  Pressure                    -5348.1           49771          4802.7          3547.1
v  turbulent_viscosity      0.00030333          171.82         0.04954         0.03866
v  CourantNb                  0.034116          7359.5          17.416           11.75
v  FourierNb                   0.85858      1.0133e+05          14.904          6.6405
v  total_pressure           4.9465e+05      5.4977e+05       5.048e+05      5.0355e+05
v  Local Time Step                0.01         0.08303        0.010045        0.010118


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.8807      1.0437e+05           32.32           18.39


 TIME FOR THE TIME STEP               69:        0.18311E+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         0.223250092E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283195E+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 0.89765E+02
   Friction velocity        uet   :  0.17400E-01 0.76597E+01
   Friction velocity        uk    :  0.17400E-01 0.76597E+01
   Dimensionless distance   yplus :  0.23561E+00 0.69271E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3142
   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    0.80284E+02     989   0.10099E+01   0.41522E+00 
c  VelocityY    0.80284E+02     989   0.10099E+01   0.00000E+00 
c  VelocityZ    0.80284E+02     989   0.10099E+01   0.00000E+00 
c  Pressure     0.15112E+00     263   0.39700E-02   0.90561E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.7787e-05                         16739


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -57.488          26.498        -0.13748       -0.075612
v  Velocity[Y]                 -35.024          69.173          0.2422         0.23013
v  Velocity[Z]                 -42.862          65.022         0.11882       0.0020818
v  ǁVelocityǁ                0.0043217          92.566         0.82015         0.74417
v  Pressure                    -5686.8           54892          4802.6          3549.4
v  turbulent_viscosity      0.00044024          191.74        0.052032        0.039751
v  CourantNb                  0.016449            8240          17.875          11.959
v  FourierNb                   0.89323      1.1312e+05          15.572          6.7949
v  total_pressure           4.9431e+05      5.5489e+05       5.048e+05      5.0355e+05
v  Local Time Step                0.01        0.085187        0.010042        0.010114


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.0716      1.1652e+05          33.448          18.754


 TIME FOR THE TIME STEP               70:        0.18094E+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        -0.375317538E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282644E+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 0.10025E+03
   Friction velocity        uet   :  0.22759E-01 0.83974E+01
   Friction velocity        uk    :  0.22759E-01 0.83974E+01
   Dimensionless distance   yplus :  0.24297E+00 0.75942E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3078
   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    0.99920E+02     992   0.10084E+01   0.48789E+00 
c  VelocityY    0.99920E+02     992   0.10084E+01   0.00000E+00 
c  VelocityZ    0.99920E+02     992   0.10084E+01   0.00000E+00 
c  Pressure     0.16753E+00     323   0.40760E-02   0.92815E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.3542e-05                         16755


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -63.964          29.878        -0.14348       -0.076341
v  Velocity[Y]                 -39.289          77.378         0.23649         0.22998
v  Velocity[Z]                 -48.101          72.411         0.10985       0.0026084
v  ǁVelocityǁ                0.0043284          103.32         0.84068         0.75897
v  Pressure                    -6367.8           60624          4804.5          3553.7
v  turbulent_viscosity      0.00077845          213.31        0.054893        0.041078
v  CourantNb                   0.10088          9220.1          18.375          12.206
v  FourierNb                   0.93169      1.1196e+05          16.121          6.9624
v  total_pressure           4.9363e+05      5.6062e+05       5.048e+05      5.0355e+05
v  Local Time Step                0.01        0.085366        0.010039        0.010104


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.0185      1.1579e+05          34.496          19.168


 TIME FOR THE TIME STEP               71:        0.19666E+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        -0.151610427E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283386E+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 0.11224E+03
   Friction velocity        uet   :  0.18687E-01 0.92283E+01
   Friction velocity        uk    :  0.18687E-01 0.92283E+01
   Dimensionless distance   yplus :  0.16368E+00 0.83456E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3002
   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    0.12509E+03    1013   0.10077E+01   0.34245E+00 
c  VelocityY    0.12509E+03    1013   0.10077E+01   0.00000E+00 
c  VelocityZ    0.12509E+03    1013   0.10077E+01   0.00000E+00 
c  Pressure     0.18519E+00     408   0.41635E-02   0.94603E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.0485e-05                         16754


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -72.909          33.398        -0.14869       -0.076698
v  Velocity[Y]                 -43.566          86.584         0.22962          0.2295
v  Velocity[Z]                  -51.04          81.364        0.098256        0.003154
v  ǁVelocityǁ                0.0079714          113.49         0.85315         0.76887
v  Pressure                    -7538.2           67322          4831.8          3575.8
v  turbulent_viscosity      0.00099827          238.17        0.058003        0.042518
v  CourantNb                  0.083405           10311          18.926          12.479
v  FourierNb                   0.96937      1.2499e+05          16.975          7.1563
v  total_pressure           4.9246e+05      5.6732e+05      5.0483e+05      5.0358e+05
v  Local Time Step                0.01        0.077316        0.010035        0.010094


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9542      1.2927e+05          35.902          19.635


 TIME FOR THE TIME STEP               72:        0.20784E+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         0.832764413E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283437E+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 0.12456E+03
   Friction velocity        uet   :  0.11307E-01 0.10069E+02
   Friction velocity        uk    :  0.11307E-01 0.10069E+02
   Dimensionless distance   yplus :  0.15904E+00 0.91059E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2958
   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    0.15657E+03    1093   0.10142E+01   0.15514E+01 
c  VelocityY    0.15657E+03    1093   0.10142E+01   0.00000E+00 
c  VelocityZ    0.15657E+03    1093   0.10142E+01   0.00000E+00 
c  Pressure     0.20813E+00     386   0.44704E-02   0.97661E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.0358e-05                         16754


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -79.358          37.298        -0.15705       -0.077236
v  Velocity[Y]                 -49.509          95.136         0.21994         0.22836
v  Velocity[Z]                 -54.863          92.417        0.093735       0.0043437
v  ǁVelocityǁ                0.0069275          122.78         0.88712         0.79299
v  Pressure                    -9069.8           74450          4843.6          3585.1
v  turbulent_viscosity      0.00074777          265.51        0.060336        0.043563
v  CourantNb                  0.024184           11379          19.327          12.667
v  FourierNb                    1.0089       1.391e+05           17.64          7.3054
v  total_pressure           4.9093e+05      5.7445e+05      5.0484e+05      5.0359e+05
v  Local Time Step                0.01        0.071083        0.010031        0.010083


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9205      1.4379e+05          36.966          19.973


 TIME FOR THE TIME STEP               73:        0.20749E+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        -0.192503805E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283355E+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 0.13627E+03
   Friction velocity        uet   :  0.98773E-02 0.10858E+02
   Friction velocity        uk    :  0.98773E-02 0.10858E+02
   Dimensionless distance   yplus :  0.13080E+00 0.98195E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2889
   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    0.18820E+03     924   0.10060E+01   0.13065E+01 
c  VelocityY    0.18820E+03     924   0.10060E+01   0.00000E+00 
c  VelocityZ    0.18820E+03     924   0.10060E+01   0.00000E+00 
c  Pressure     0.23083E+00     338   0.44095E-02   0.99240E-01 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.4711e-05                         16750


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -87.824          40.998        -0.16418        -0.07803
v  Velocity[Y]                 -54.372          106.53         0.20491         0.22786
v  Velocity[Z]                 -63.028           101.2        0.075984        0.005369
v  ǁVelocityǁ                 0.012164          138.98         0.90431         0.81354
v  Pressure                     -10655           82526          4844.5          3591.7
v  turbulent_viscosity       0.0013225          290.72         0.06559        0.046066
v  CourantNb                  0.039368           12711          20.133          13.096
v  FourierNb                     1.034       1.528e+05          18.859          7.6312
v  total_pressure           4.8934e+05      5.8253e+05      5.0484e+05      5.0359e+05
v  Local Time Step                0.01        0.074939        0.010028        0.010076


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.2079      1.5806e+05          38.992          20.727


 TIME FOR THE TIME STEP               74:        0.18834E+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        -0.112866478E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283666E+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 0.15377E+03
   Friction velocity        uet   :  0.10611E-01 0.12021E+02
   Friction velocity        uk    :  0.10611E-01 0.12021E+02
   Dimensionless distance   yplus :  0.16135E+00 0.10871E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2808
   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    0.23797E+03    1105   0.10070E+01   0.15200E+01 
c  VelocityY    0.23797E+03    1105   0.10070E+01   0.00000E+00 
c  VelocityZ    0.23797E+03    1105   0.10070E+01   0.00000E+00 
c  Pressure     0.25529E+00     393   0.45211E-02   0.10033E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.3524e-05                         16750


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -101.46          46.192         -0.1727       -0.078799
v  Velocity[Y]                 -60.752          119.46         0.19409         0.22719
v  Velocity[Z]                 -69.332          113.81         0.06783       0.0069905
v  ǁVelocityǁ                 0.011208          155.16          0.9359         0.83646
v  Pressure                     -12312           91766          4860.2          3603.5
v  turbulent_viscosity       0.0012564          326.33         0.06884        0.047696
v  CourantNb                 0.0095151           14240          20.638          13.438
v  FourierNb                    1.0611       1.711e+05          19.767          7.8332
v  total_pressure           4.8769e+05      5.9177e+05      5.0486e+05       5.036e+05
v  Local Time Step                0.01        0.070383        0.010026         0.01007


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.2669      1.7696e+05          40.405          21.271


 TIME FOR THE TIME STEP               75:        0.22656E+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        -0.171726997E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283479E+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 0.17214E+03
   Friction velocity        uet   :  0.20384E-01 0.13222E+02
   Friction velocity        uk    :  0.20384E-01 0.13222E+02
   Dimensionless distance   yplus :  0.26409E+00 0.11958E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2766
   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    0.29949E+03    1047   0.10124E+01   0.20530E+01 
c  VelocityY    0.29949E+03    1047   0.10124E+01   0.00000E+00 
c  VelocityZ    0.29949E+03    1047   0.10124E+01   0.00000E+00 
c  Pressure     0.28677E+00     347   0.47685E-02   0.10273E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.1419e-05                         16753


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -109.06          51.898         -0.1859       -0.080036
v  Velocity[Y]                 -68.776          131.36          0.1726         0.22556
v  Velocity[Z]                 -75.385          128.35        0.073307       0.0093039
v  ǁVelocityǁ                 0.014965          168.13         0.99438         0.87583
v  Pressure                     -14474      1.0153e+05          4854.4          3607.3
v  turbulent_viscosity        0.001455          364.71        0.073756        0.049885
v  CourantNb                  0.040901           15773          21.458          13.849
v  FourierNb                    1.0505      1.9126e+05          21.047           8.147
v  total_pressure           4.8553e+05      6.0153e+05      5.0485e+05      5.0361e+05
v  Local Time Step                0.01         0.07104        0.010025        0.010067


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.914      1.9774e+05          42.505          21.996


 TIME FOR THE TIME STEP               76:        0.20023E+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        -0.733321090E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283474E+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 0.18857E+03
   Friction velocity        uet   :  0.44887E-02 0.14283E+02
   Friction velocity        uk    :  0.44887E-02 0.14283E+02
   Dimensionless distance   yplus :  0.35503E-01 0.12917E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2694
   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    0.36045E+03     961   0.10052E+01   0.34102E+01 
c  VelocityY    0.36045E+03     961   0.10052E+01   0.00000E+00 
c  VelocityZ    0.36045E+03     961   0.10052E+01   0.00000E+00 
c  Pressure     0.31901E+00     456   0.47629E-02   0.10396E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.7143e-05                         16750


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -122.3          56.823        -0.18628       -0.081423
v  Velocity[Y]                 -76.453          147.21         0.15514         0.22478
v  Velocity[Z]                  -87.27           140.4        0.053282        0.010872
v  ǁVelocityǁ                 0.012363           191.2          1.0308         0.91328
v  Pressure                     -16836       1.125e+05          4814.1          3584.7
v  turbulent_viscosity       0.0022006          399.75        0.081117        0.053306
v  CourantNb                 0.0081691           17604          22.896          14.569
v  FourierNb                    1.0799      2.1018e+05          22.788          8.6033
v  total_pressure           4.8316e+05       6.125e+05      5.0481e+05      5.0358e+05
v  Local Time Step                0.01         0.07063         0.01002        0.010055


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.1081      2.1748e+05          45.684          23.172


 TIME FOR THE TIME STEP               77:        0.20040E+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         0.654263469E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283633E+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 0.21355E+03
   Friction velocity        uet   :  0.15959E-01 0.15873E+02
   Friction velocity        uk    :  0.15959E-01 0.15873E+02
   Dimensionless distance   yplus :  0.14688E+00 0.14355E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2601
   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    0.45647E+03    1097   0.10052E+01   0.28547E+01 
c  VelocityY    0.45647E+03    1097   0.10052E+01   0.00000E+00 
c  VelocityZ    0.45647E+03    1097   0.10052E+01   0.00000E+00 
c  Pressure     0.35403E+00     390   0.48151E-02   0.10475E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.6591e-05                         16741


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -139.45          63.443        -0.19242       -0.082929
v  Velocity[Y]                 -83.469          165.39         0.15018         0.22372
v  Velocity[Z]                 -95.872          158.05        0.047284        0.013409
v  ǁVelocityǁ                0.0049207          212.86          1.0985         0.95603
v  Pressure                     -19131      1.2527e+05          4798.1          3579.4
v  turbulent_viscosity       0.0013079          449.17        0.085913        0.055943
v  CourantNb                  0.026976           19733          23.818          15.199
v  FourierNb                    1.0873      2.3568e+05          24.163          8.9144
v  total_pressure           4.8087e+05      6.2527e+05       5.048e+05      5.0358e+05
v  Local Time Step                0.01        0.070127        0.010019         0.01005


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           2.255      2.4383e+05          47.981          24.113


 TIME FOR THE TIME STEP               78:        0.21538E+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        -0.276503649E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283818E+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 0.23845E+03
   Friction velocity        uet   :  0.18649E-01 0.17434E+02
   Friction velocity        uk    :  0.18649E-01 0.17434E+02
   Dimensionless distance   yplus :  0.18218E+00 0.15767E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2463
   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    0.57633E+03    1082   0.10111E+01   0.55661E+01 
c  VelocityY    0.57633E+03    1082   0.10111E+01   0.00000E+00 
c  VelocityZ    0.57633E+03    1082   0.10111E+01   0.00000E+00 
c  Pressure     0.39590E+00     408   0.51108E-02   0.10616E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.4729e-05                         16748


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -152.91          72.551        -0.21597       -0.085234
v  Velocity[Y]                 -95.912          182.48         0.13475         0.22149
v  Velocity[Z]                 -104.97          178.03        0.079958        0.016652
v  ǁVelocityǁ                0.0074423          232.47          1.2184          1.0209
v  Pressure                     -22104      1.3883e+05          4757.9          3566.1
v  turbulent_viscosity      0.00096042          502.88         0.09305        0.059129
v  CourantNb                   0.10878           21874          25.553          16.012
v  FourierNb                    1.1118      2.6373e+05          25.926          9.3584
v  total_pressure            4.779e+05      6.3883e+05      5.0476e+05      5.0357e+05
v  Local Time Step                0.01        0.069184        0.010016        0.010044


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.1928      2.7272e+05          51.479           25.37


 TIME FOR THE TIME STEP               79:        0.21938E+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         0.909485084E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283930E+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 0.26328E+03
   Friction velocity        uet   :  0.82048E-02 0.18971E+02
   Friction velocity        uk    :  0.82048E-02 0.18971E+02
   Dimensionless distance   yplus :  0.14796E+00 0.17156E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2338
   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    0.69891E+03     971   0.10041E+01   0.85065E+01 
c  VelocityY    0.69891E+03     971   0.10041E+01   0.00000E+00 
c  VelocityZ    0.69891E+03     971   0.10041E+01   0.00000E+00 
c  Pressure     0.44288E+00     411   0.51218E-02   0.10744E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.2043e-05                         16758


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -168.94          79.228        -0.21221       -0.087222
v  Velocity[Y]                 -106.89          203.77         0.11334         0.22039
v  Velocity[Z]                 -120.92           195.3        0.050794        0.019732
v  ǁVelocityǁ                0.0087243          263.07          1.2841          1.0857
v  Pressure                     -25559      1.5379e+05          4681.8          3530.5
v  turbulent_viscosity       0.0017473          553.52         0.10386        0.063982
v  CourantNb                  0.025446           24404          28.523          17.273
v  FourierNb                     1.149      2.9108e+05           28.46          10.025
v  total_pressure           4.7444e+05      6.5379e+05      5.0468e+05      5.0353e+05
v  Local Time Step                0.01        0.068016        0.010016        0.010044


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.1516      3.0123e+05          56.983          27.298


 TIME FOR THE TIME STEP               80:        0.20101E+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        -0.435015806E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284429E+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 0.29648E+03
   Friction velocity        uet   :  0.15443E-01 0.20997E+02
   Friction velocity        uk    :  0.15443E-01 0.20997E+02
   Dimensionless distance   yplus :  0.21165E+00 0.18989E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2223
   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    0.87822E+03    1089   0.10037E+01   0.47989E+01 
c  VelocityY    0.87822E+03    1089   0.10037E+01   0.00000E+00 
c  VelocityZ    0.87822E+03    1089   0.10037E+01   0.00000E+00 
c  Pressure     0.49052E+00     401   0.51500E-02   0.10755E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.1264e-05                         16757


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -193.63          88.102        -0.21303       -0.088716
v  Velocity[Y]                 -116.92          229.18         0.12069         0.21933
v  Velocity[Z]                 -133.67          219.17         0.04183         0.02389
v  ǁVelocityǁ                 0.014047          294.16          1.3835          1.1586
v  Pressure                     -28890      1.7132e+05          4585.3          3474.9
v  turbulent_viscosity       0.0020901          619.47         0.11022         0.06785
v  CourantNb                  0.010793           27358           30.13          18.361
v  FourierNb                    1.1433      3.6573e+05          30.851           10.47
v  total_pressure           4.7111e+05      6.7132e+05      5.0459e+05      5.0347e+05
v  Local Time Step                0.01        0.065914        0.010015        0.010043


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.2031      3.7705e+05           60.98          28.831


 TIME FOR THE TIME STEP               81:        0.22663E+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        -0.385676948E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283920E+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 0.33235E+03
   Friction velocity        uet   :  0.10227E-01 0.23156E+02
   Friction velocity        uk    :  0.10227E-01 0.23156E+02
   Dimensionless distance   yplus :  0.20234E+00 0.20941E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2071
   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    0.11121E+04    1098   0.10067E+01   0.15105E+02 
c  VelocityY    0.11121E+04    1098   0.10067E+01   0.00000E+00 
c  VelocityZ    0.11121E+04    1098   0.10067E+01   0.00000E+00 
c  Pressure     0.54598E+00     404   0.52623E-02   0.10811E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.0585e-05                         16759


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -216.83          98.745        -0.25251       -0.090714
v  Velocity[Y]                 -132.49          254.05         0.10917          0.2158
v  Velocity[Z]                 -144.43          247.64         0.10996        0.027059
v  ǁVelocityǁ                 0.024186          321.46          1.5586          1.2436
v  Pressure                     -32760      1.9067e+05          4540.3          3471.6
v  turbulent_viscosity       0.0017529          694.91         0.11978          0.0725
v  CourantNb                   0.10814           30345           32.56          19.661
v  FourierNb                    1.1516      3.6457e+05           32.62          11.066
v  total_pressure           4.6724e+05      6.9067e+05      5.0454e+05      5.0347e+05
v  Local Time Step                0.01        0.064669        0.010014        0.010036


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.3424      3.7708e+05           65.18          30.727


 TIME FOR THE TIME STEP               82:        0.23218E+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        -0.232664449E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284224E+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 0.36673E+03
   Friction velocity        uet   :  0.26207E-01 0.25197E+02
   Friction velocity        uk    :  0.26207E-01 0.25197E+02
   Dimensionless distance   yplus :  0.29274E+00 0.22787E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1990
   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    0.13662E+04    1060   0.10091E+01   0.19676E+02 
c  VelocityY    0.13662E+04    1060   0.10091E+01   0.00000E+00 
c  VelocityZ    0.13662E+04    1060   0.10091E+01   0.00000E+00 
c  Pressure     0.61919E+00     404   0.58346E-02   0.11054E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      8.9819e-06                         16759


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -238.65          119.61        -0.24995       -0.095753
v  Velocity[Y]                 -150.14          280.14        0.052496         0.21216
v  Velocity[Z]                 -162.56          274.63         0.12365        0.034244
v  ǁVelocityǁ                 0.021339          353.66          1.6957          1.3611
v  Pressure                     -37491      2.1115e+05          4479.1          3472.4
v  turbulent_viscosity       0.0022888          768.34          0.1333        0.077899
v  CourantNb                    0.1759           33472          37.054          21.429
v  FourierNb                    1.1421      4.5375e+05          36.649          11.908
v  total_pressure           4.6251e+05      7.1115e+05      5.0448e+05      5.0347e+05
v  Local Time Step                0.01        0.050282        0.010011        0.010031


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.3145      4.6754e+05          73.703          33.337


 TIME FOR THE TIME STEP               83:        0.20835E+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        -0.238119325E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284366E+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 0.40442E+03
   Friction velocity        uet   :  0.15089E-01 0.27410E+02
   Friction velocity        uk    :  0.15089E-01 0.27410E+02
   Dimensionless distance   yplus :  0.24535E+00 0.24788E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1951
   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    0.16585E+04     966   0.10002E+01   0.28475E+02 
c  VelocityY    0.16585E+04     966   0.10002E+01   0.00000E+00 
c  VelocityZ    0.16585E+04     966   0.10002E+01   0.00000E+00 
c  Pressure     0.68994E+00     407   0.52776E-02   0.11095E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      7.5601e-06                         16759


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -256.18             136        -0.20059       -0.097699
v  Velocity[Y]                 -162.81          313.54        0.026535         0.21317
v  Velocity[Z]                 -188.04          300.86        0.024757        0.039121
v  ǁVelocityǁ                   0.0125          401.16          1.8352          1.4905
v  Pressure                     -43390      2.3353e+05          4152.9          3273.7
v  turbulent_viscosity       0.0021219          847.21         0.14787        0.086373
v  CourantNb                   0.16932           37525          40.086          23.405
v  FourierNb                    1.0945      4.4605e+05          39.485          12.857
v  total_pressure           4.5661e+05      7.3353e+05      5.0415e+05      5.0327e+05
v  Local Time Step                0.01         0.05531         0.01001        0.010028


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.0945       4.616e+05          79.571          36.261


 TIME FOR THE TIME STEP               84:        0.20685E+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        -0.832569570E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273280619E+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 0.45674E+03
   Friction velocity        uet   :  0.25758E-01 0.30440E+02
   Friction velocity        uk    :  0.25758E-01 0.30440E+02
   Dimensionless distance   yplus :  0.30867E+00 0.27529E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1860
   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    0.20963E+04    1113   0.10004E+01   0.33995E+02 
c  VelocityY    0.20963E+04    1113   0.10004E+01   0.00000E+00 
c  VelocityZ    0.20963E+04    1113   0.10004E+01   0.00000E+00 
c  Pressure     0.76761E+00     419   0.54275E-02   0.11110E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      7.7772e-06                         16757


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -295.45          150.06         -0.2231       -0.097614
v  Velocity[Y]                 -178.41          352.27        0.070811         0.20781
v  Velocity[Z]                 -205.57           340.8        0.053761        0.047231
v  ǁVelocityǁ                0.0096266           448.3          2.1156          1.6403
v  Pressure                     -49150      2.5993e+05          3941.6            3165
v  turbulent_viscosity       0.0027045          950.15         0.15909        0.092957
v  CourantNb                  0.040505           42095          43.364          25.561
v  FourierNb                    1.1132      4.9933e+05          42.394          13.597
v  total_pressure           4.5085e+05      7.5993e+05      5.0394e+05      5.0317e+05
v  Local Time Step                0.01        0.054283         0.01001        0.010027


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.0751       5.167e+05          85.758          39.158


 TIME FOR THE TIME STEP               85:        0.22983E+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        -0.190141360E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283431E+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 0.51150E+03
   Friction velocity        uet   :  0.65246E-02 0.33569E+02
   Friction velocity        uk    :  0.65246E-02 0.33569E+02
   Dimensionless distance   yplus :  0.87950E-01 0.30358E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1662
   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    0.26517E+04    1046   0.10081E+01   0.44855E+02 
c  VelocityY    0.26517E+04    1046   0.10081E+01   0.00000E+00 
c  VelocityZ    0.26517E+04    1046   0.10081E+01   0.00000E+00 
c  Pressure     0.85588E+00     450   0.61672E-02   0.11148E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step       6.188e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -326.05          172.69        -0.31578         -0.1108
v  Velocity[Y]                 -200.62          387.44        0.039526         0.20213
v  Velocity[Z]                 -222.48          382.95         0.13724        0.054979
v  ǁVelocityǁ                 0.018917          485.93          2.4079          1.7621
v  Pressure                     -55093      2.8878e+05          3985.9          3289.3
v  turbulent_viscosity        0.001827          1064.9          0.1809         0.10295
v  CourantNb                  0.001175           46970          50.348          28.458
v  FourierNb                    1.0949      5.5934e+05          47.644          14.972
v  total_pressure           4.4491e+05      7.8878e+05      5.0399e+05      5.0329e+05
v  Local Time Step                0.01        0.057433        0.010009        0.010023


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.7995      5.7852e+05          97.992          43.429


 TIME FOR THE TIME STEP               86:        0.22023E+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        -0.496766824E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273286037E+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 0.56097E+03
   Friction velocity        uet   :  0.19244E-01 0.36361E+02
   Friction velocity        uk    :  0.19244E-01 0.36361E+02
   Dimensionless distance   yplus :  0.24028E+00 0.32884E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1458
   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    0.31868E+04     999   0.10007E+01   0.18278E+03 
c  VelocityY    0.31868E+04     999   0.10007E+01   0.00000E+00 
c  VelocityZ    0.31868E+04     999   0.10007E+01   0.00000E+00 
c  Pressure     0.96505E+00     408   0.60586E-02   0.11293E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      5.2452e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -359.61          186.61        -0.16642        -0.10507
v  Velocity[Y]                 -226.09           434.4        0.032341         0.19941
v  Velocity[Z]                 -259.55          420.06        -0.01053        0.058126
v  ǁVelocityǁ                 0.023617           555.2          2.7145          2.0884
v  Pressure                     -65525      3.1749e+05          3295.2          2841.5
v  turbulent_viscosity        0.002754          1168.4         0.20222         0.11274
v  CourantNb                   0.07069           52254          58.026          31.143
v  FourierNb                     1.055      6.1519e+05          52.697          16.306
v  total_pressure           4.3448e+05      8.1749e+05       5.033e+05      5.0284e+05
v  Local Time Step                0.01         0.05564        0.010008        0.010019


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9318      6.3682e+05          110.72          47.449


 TIME FOR THE TIME STEP               87:        0.18909E+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        -0.659129143E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273280319E+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 0.63704E+03
   Friction velocity        uet   :  0.18964E-01 0.40601E+02
   Friction velocity        uk    :  0.18964E-01 0.40601E+02
   Dimensionless distance   yplus :  0.22981E+00 0.36718E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1380
   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    0.40428E+04    1096   0.10004E+01   0.97688E+02 
c  VelocityY    0.40428E+04    1096   0.10004E+01   0.00000E+00 
c  VelocityZ    0.40428E+04    1096   0.10004E+01   0.00000E+00 
c  Pressure     0.10538E+01     497   0.58766E-02   0.11092E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      5.9904e-06                         16757


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -407.63          207.45        -0.28024        -0.11205
v  Velocity[Y]                 -246.74          486.77        0.094686         0.19555
v  Velocity[Z]                 -287.52          466.74         0.01102        0.071407
v  ǁVelocityǁ                 0.016353          618.41          2.8233          2.1232
v  Pressure                     -73841      3.5304e+05          2340.7          2277.5
v  turbulent_viscosity        0.002061          1314.2         0.22392         0.12717
v  CourantNb                  0.093519           58503          64.204          36.394
v  FourierNb                    1.0397      6.9089e+05          57.746           17.78
v  total_pressure           4.2616e+05      8.5304e+05      5.0234e+05      5.0228e+05
v  Local Time Step                0.01        0.042636        0.010007        0.010018


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.2085      7.1515e+05          121.95          54.174


 TIME FOR THE TIME STEP               88:        0.22256E+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        -0.702868568E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273279475E+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 0.71110E+03
   Friction velocity        uet   :  0.18862E-01 0.44673E+02
   Friction velocity        uk    :  0.18862E-01 0.44673E+02
   Dimensionless distance   yplus :  0.27368E+00 0.40401E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1335
   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    0.50829E+04    1123   0.10043E+01   0.16849E+03 
c  VelocityY    0.50829E+04    1123   0.10043E+01   0.00000E+00 
c  VelocityZ    0.50829E+04    1123   0.10043E+01   0.00000E+00 
c  Pressure     0.11917E+01     511   0.62648E-02   0.11264E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.5683e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -456.27          236.95        -0.47438        -0.12961
v  Velocity[Y]                 -274.82          541.96         0.12183         0.18666
v  Velocity[Z]                 -311.28          532.22         0.21378        0.076461
v  ǁVelocityǁ                 0.012972          678.58          3.5258          2.4247
v  Pressure                     -82228      3.9397e+05            2636          2582.8
v  turbulent_viscosity       0.0019254          1469.5         0.24444         0.13542
v  CourantNb                 0.0099443           64967          67.719          37.205
v  FourierNb                    1.0434      7.7213e+05          63.114           19.04
v  total_pressure           4.1777e+05      8.9397e+05      5.0264e+05      5.0258e+05
v  Local Time Step                0.01        0.021799        0.010005        0.010013


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.2278      7.9895e+05          130.83          56.245


 TIME FOR THE TIME STEP               89:        0.20940E+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        -0.299462609E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273287072E+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 0.78851E+03
   Friction velocity        uet   :  0.57904E-02 0.48879E+02
   Friction velocity        uk    :  0.57904E-02 0.48879E+02
   Dimensionless distance   yplus :  0.74026E-01 0.44204E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1303
   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    0.62886E+04    1098   0.10063E+01   0.30948E+03 
c  VelocityY    0.62886E+04    1098   0.10063E+01   0.00000E+00 
c  VelocityZ    0.62886E+04    1098   0.10063E+01   0.00000E+00 
c  Pressure     0.13367E+01     459   0.70653E-02   0.11345E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.8721e-06                         16760


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -523.48          255.83        -0.28122        -0.12575
v  Velocity[Y]                 -315.92          597.85       -0.073583          0.1759
v  Velocity[Z]                 -353.03          587.18         0.34738        0.091993
v  ǁVelocityǁ                 0.014048           753.2          3.4393          2.6056
v  Pressure                     -94597      4.3502e+05            2664          2753.7
v  turbulent_viscosity       0.0012598          1632.5         0.28233         0.15287
v  CourantNb                  0.058086           71851           85.45          43.695
v  FourierNb                    1.0882      8.5838e+05          71.674          21.448
v  total_pressure            4.054e+05      9.3502e+05      5.0266e+05      5.0275e+05
v  Local Time Step                0.01        0.023979        0.010005        0.010015


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           2.017      8.8811e+05          157.12          65.142


 TIME FOR THE TIME STEP               90:        0.22546E+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        -0.574620865E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273286487E+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 0.87492E+03
   Friction velocity        uet   :  0.28395E-01 0.53519E+02
   Friction velocity        uk    :  0.28395E-01 0.53519E+02
   Dimensionless distance   yplus :  0.25947E+00 0.48400E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1406
   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    0.76453E+04    1078   0.99790E+00   0.37287E+03 
c  VelocityY    0.76453E+04    1078   0.99790E+00   0.00000E+00 
c  VelocityZ    0.76453E+04    1078   0.99790E+00   0.00000E+00 
c  Pressure     0.15011E+01     516   0.63030E-02   0.11424E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.5149e-06                         16757


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -550.21           294.6        -0.14061        -0.13355
v  Velocity[Y]                 -343.59          672.67        -0.19197          0.1818
v  Velocity[Z]                 -405.14          646.89        -0.23347         0.08787
v  ǁVelocityǁ                0.0090471          852.39           4.249          3.0832
v  Pressure                -1.1108e+05      4.7936e+05          1616.4          2051.9
v  turbulent_viscosity       0.0020623            1802         0.31032         0.16954
v  CourantNb                  0.042732           80759          81.716          45.608
v  FourierNb                   0.99587      9.4929e+05          78.416          23.256
v  total_pressure           3.8892e+05      9.7936e+05      5.0162e+05      5.0205e+05
v  Local Time Step                0.01        0.025937        0.010006        0.010016


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.0081        9.83e+05          160.13          68.864


 TIME FOR THE TIME STEP               91:        0.22617E+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         0.372964786E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273278000E+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 0.98690E+03
   Friction velocity        uet   :  0.22789E-01 0.59458E+02
   Friction velocity        uk    :  0.22789E-01 0.59458E+02
   Dimensionless distance   yplus :  0.24268E+00 0.53771E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1291
   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    0.97549E+04    1290   0.99751E+00   0.60265E+03 
c  VelocityY    0.97549E+04    1290   0.99751E+00   0.00000E+00 
c  VelocityZ    0.97549E+04    1290   0.99751E+00   0.00000E+00 
c  Pressure     0.16667E+01     516   0.66048E-02   0.11374E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.6383e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -631.23          324.09        -0.59795        -0.15375
v  Velocity[Y]                 -383.84          754.38         0.22124         0.17106
v  Velocity[Z]                 -442.95          730.09         0.11248         0.11149
v  ǁVelocityǁ                0.0079818          952.28          4.9177          3.3624
v  Pressure                -1.2557e+05       5.333e+05          487.35          1404.6
v  turbulent_viscosity       0.0025772          2030.4         0.34877         0.18864
v  CourantNb                  0.042077           90797          101.51          54.556
v  FourierNb                   0.99839      1.0672e+06          87.686          25.688
v  total_pressure           3.7443e+05      1.0333e+06      5.0049e+05       5.014e+05
v  Local Time Step                0.01        0.022705        0.010005        0.010015


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2193      1.1047e+06          189.19          80.244


 TIME FOR THE TIME STEP               92:        0.25947E+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        -0.182603156E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273277344E+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 0.11055E+04
   Friction velocity        uet   :  0.19475E-01 0.65666E+02
   Friction velocity        uk    :  0.19475E-01 0.65666E+02
   Dimensionless distance   yplus :  0.23083E+00 0.59385E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1166
   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    0.12299E+05    1264   0.10063E+01   0.59896E+03 
c  VelocityY    0.12299E+05    1264   0.10063E+01   0.00000E+00 
c  VelocityZ    0.12299E+05    1264   0.10063E+01   0.00000E+00 
c  Pressure     0.18720E+01     550   0.76515E-02   0.11460E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.6968e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -707.44          372.56        -0.69191         -0.1661
v  Velocity[Y]                 -430.39           830.5       -0.077964         0.14773
v  Velocity[Z]                 -475.62          824.27         0.87535         0.14458
v  ǁVelocityǁ                 0.016836          1029.5          4.6422          3.3167
v  Pressure                -1.3719e+05      5.9643e+05          2121.8          2864.3
v  turbulent_viscosity       0.0039311          2271.6         0.39825         0.21467
v  CourantNb                  0.060912      1.0133e+05          118.78          60.513
v  FourierNb                    1.0292      1.3424e+06          101.09          29.042
v  total_pressure           3.6281e+05      1.0964e+06      5.0212e+05      5.0286e+05
v  Local Time Step                0.01        0.023198        0.010004        0.010011


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2198      1.3839e+06          219.86          89.555


 TIME FOR THE TIME STEP               93:        0.25773E+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        -0.166298839E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273288310E+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 0.12111E+04
   Friction velocity        uet   :  0.15942E-01 0.71135E+02
   Friction velocity        uk    :  0.15942E-01 0.71135E+02
   Dimensionless distance   yplus :  0.15460E+00 0.64331E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1301
   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    0.14799E+05    1214   0.99863E+00   0.22969E+04 
c  VelocityY    0.14799E+05    1214   0.99863E+00   0.00000E+00 
c  VelocityZ    0.14799E+05    1214   0.99863E+00   0.00000E+00 
c  Pressure     0.21040E+01     468   0.81814E-02   0.11556E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step       2.413e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -776.21          407.04        -0.46098        -0.15688
v  Velocity[Y]                 -489.75          926.01        -0.56254          0.1495
v  Velocity[Z]                 -552.42          899.36        0.067612          0.1075
v  ǁVelocityǁ                 0.025045          1167.3          7.0888          5.0784
v  Pressure                -1.6851e+05      6.4866e+05          1358.2          2130.5
v  turbulent_viscosity       0.0032758          2496.1         0.43343         0.22938
v  CourantNb                  0.016136      1.1275e+05          112.32          59.008
v  FourierNb                   0.94538      1.4775e+06          110.41          31.225
v  total_pressure           3.3149e+05      1.1487e+06      5.0136e+05      5.0213e+05
v  Local Time Step                0.01         0.01762        0.010003         0.01001


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.531      1.5243e+06          222.73          90.234


 TIME FOR THE TIME STEP               94:        0.24237E+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        -0.143745458E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273274989E+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 0.13642E+04
   Friction velocity        uet   :  0.17996E-01 0.78975E+02
   Friction velocity        uk    :  0.17996E-01 0.78975E+02
   Dimensionless distance   yplus :  0.22540E+00 0.71422E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1136
   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    0.18557E+05    1557   0.99606E+00   0.22875E+04 
c  VelocityY    0.18557E+05    1557   0.99606E+00   0.00000E+00 
c  VelocityZ    0.18557E+05    1557   0.99606E+00   0.00000E+00 
c  Pressure     0.23310E+01     519   0.72293E-02   0.11487E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.7993e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -871.65           441.4       -0.013314        -0.16614
v  Velocity[Y]                 -523.49          1037.8        -0.48353         0.14569
v  Velocity[Z]                 -612.77          1004.9        -0.91677         0.18529
v  ǁVelocityǁ                 0.019053          1309.3           6.368          4.2328
v  Pressure                -1.9289e+05      7.1759e+05         -707.33           844.5
v  turbulent_viscosity       0.0031721            2791         0.49968         0.27589
v  CourantNb                   0.13273      1.2607e+05          166.99          90.344
v  FourierNb                   0.92312      1.4682e+06          121.24          35.737
v  total_pressure           3.0711e+05      1.2176e+06      4.9929e+05      5.0084e+05
v  Local Time Step                0.01        0.015033        0.010002        0.010009


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4314      1.5205e+06          288.23          126.08


 TIME FOR THE TIME STEP               95:        0.27066E+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        -0.609261535E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273275434E+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 0.15290E+04
   Friction velocity        uet   :  0.30656E-01 0.87307E+02
   Friction velocity        uk    :  0.30656E-01 0.87307E+02
   Dimensionless distance   yplus :  0.27979E+00 0.78956E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1179
   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    0.23399E+05    1494   0.10055E+01   0.29451E+04 
c  VelocityY    0.23399E+05    1494   0.10055E+01   0.00000E+00 
c  VelocityZ    0.23399E+05    1494   0.10055E+01   0.00000E+00 
c  Pressure     0.26695E+01     531   0.89667E-02   0.11773E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.2506e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -991.05           505.1         -1.2808         -0.2093
v  Velocity[Y]                  -600.5          1146.4         0.30864         0.11807
v  Velocity[Z]                 -663.07          1143.3         0.91033         0.21552
v  ǁVelocityǁ                 0.019968          1425.3          8.3214          5.5768
v  Pressure                -2.1478e+05      7.9885e+05          1256.6          2576.5
v  turbulent_viscosity       0.0041399          3123.5          0.5469         0.29478
v  CourantNb                  0.058858      1.4075e+05          155.16          76.938
v  FourierNb                   0.90693      1.6421e+06          134.04          38.618
v  total_pressure           2.8522e+05      1.2988e+06      5.0126e+05      5.0258e+05
v  Local Time Step                0.01         0.01331        0.010002        0.010008


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5112      1.6998e+06           289.2          115.56


 TIME FOR THE TIME STEP               96:        0.28134E+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        -0.358784138E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273289464E+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 0.16853E+04
   Friction velocity        uet   :  0.25965E-01 0.95123E+02
   Friction velocity        uk    :  0.25965E-01 0.95123E+02
   Dimensionless distance   yplus :  0.26312E+00 0.86025E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1100
   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    0.28343E+05    1556   0.99759E+00   0.59553E+04 
c  VelocityY    0.28343E+05    1556   0.99759E+00   0.00000E+00 
c  VelocityZ    0.28343E+05    1556   0.99759E+00   0.00000E+00 
c  Pressure     0.29199E+01     464   0.85051E-02   0.11562E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.8016e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1068.2          567.51        -0.84255        -0.17199
v  Velocity[Y]                 -667.45          1276.3        -0.26052          0.1118
v  Velocity[Z]                 -760.68          1242.2          1.1489         0.17091
v  ǁVelocityǁ                 0.012754          1601.7          9.2563           6.606
v  Pressure                -2.5889e+05      8.7044e+05         -581.35          1336.7
v  turbulent_viscosity       0.0033059          3442.6         0.63231         0.34434
v  CourantNb                   0.08602      1.5649e+05          199.93          100.64
v  FourierNb                   0.96748      1.8138e+06          152.14          44.366
v  total_pressure           2.4111e+05      1.3704e+06      4.9942e+05      5.0134e+05
v  Local Time Step                0.01        0.014641        0.010002        0.010007


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.499       1.879e+06          352.07             145


 TIME FOR THE TIME STEP               97:        0.28902E+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         0.234291981E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273274198E+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 0.18843E+04
   Friction velocity        uet   :  0.31640E-01 0.10496E+03
   Friction velocity        uk    :  0.31640E-01 0.10496E+03
   Dimensionless distance   yplus :  0.26854E+00 0.94924E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1170
   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    0.35414E+05    1683   0.99528E+00   0.55528E+04 
c  VelocityY    0.35414E+05    1683   0.99528E+00   0.00000E+00 
c  VelocityZ    0.35414E+05    1683   0.99528E+00   0.00000E+00 
c  Pressure     0.32776E+01     463   0.78190E-02   0.11627E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.7649e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1215.7          608.51         0.54518        -0.19644
v  Velocity[Y]                  -733.5          1434.4        -0.88303        0.091016
v  Velocity[Z]                 -846.01          1396.2         -1.2721         0.27354
v  ǁVelocityǁ                0.0052345          1802.9          9.0155          6.1221
v  Pressure                -2.9308e+05       9.654e+05          164.75          2087.1
v  turbulent_viscosity       0.0021337            3843         0.69381          0.3739
v  CourantNb                  0.091212       1.748e+05          218.38          117.64
v  FourierNb                   0.97463      2.0217e+06          166.58          48.204
v  total_pressure           2.0692e+05      1.4654e+06      5.0016e+05      5.0209e+05
v  Local Time Step                0.01        0.016071        0.010002        0.010006


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5619      2.0941e+06          384.96          165.84


 TIME FOR THE TIME STEP               98:        0.32366E+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        -0.255170790E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273293657E+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 0.21208E+04
   Friction velocity        uet   :  0.15043E-01 0.11652E+03
   Friction velocity        uk    :  0.15043E-01 0.11652E+03
   Dimensionless distance   yplus :  0.25839E+00 0.10538E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1261
   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    0.44870E+05    1763   0.10046E+01   0.10203E+05 
c  VelocityY    0.44870E+05    1763   0.10046E+01   0.00000E+00 
c  VelocityZ    0.44870E+05    1763   0.10046E+01   0.00000E+00 
c  Pressure     0.37227E+01     467   0.10017E-01   0.11830E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.6488e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1372.3          707.41         -1.4284        -0.27695
v  Velocity[Y]                 -818.16          1580.3         0.15518         0.06782
v  Velocity[Z]                 -915.09          1567.1          0.1896          0.3142
v  ǁVelocityǁ                0.0046413          1958.3          13.868          8.8924
v  Pressure                -3.3945e+05        1.06e+06         -1628.7          781.25
v  turbulent_viscosity       0.0022424          4312.3         0.77512         0.41499
v  CourantNb                 0.0045852      1.9509e+05          217.93          110.31
v  FourierNb                   0.96985      2.2675e+06          186.77          53.489
v  total_pressure           1.6055e+05        1.56e+06      4.9837e+05      5.0078e+05
v  Local Time Step                0.01         0.01349        0.010004        0.010012


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2481      2.3476e+06          404.69           163.8


 TIME FOR THE TIME STEP               99:        0.33458E+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        -0.404491770E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273294663E+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 0.23301E+04
   Friction velocity        uet   :  0.30532E-01 0.12664E+03
   Friction velocity        uk    :  0.30532E-01 0.12664E+03
   Dimensionless distance   yplus :  0.19257E+00 0.11453E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        971
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          1 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:    0.92862E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.54044E+05    1972   0.99767E+00   0.16117E+05 
c  VelocityY    0.54044E+05    1972   0.99767E+00   0.00000E+00 
c  VelocityZ    0.54044E+05    1972   0.99767E+00   0.00000E+00 
c  Pressure     0.41284E+01     476   0.92937E-02   0.11762E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.2917e-06                         16760


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                   -1499          779.94        -0.82193        -0.18679
v  Velocity[Y]                 -928.03          1764.2        -0.23892         0.06036
v  Velocity[Z]                 -1054.9          1724.6          1.6558          0.2433
v  ǁVelocityǁ                 0.018787          2216.6          12.931          9.3212
v  Pressure                -4.0594e+05      1.1538e+06         -4519.4         -1315.1
v  turbulent_viscosity       0.0028678          4741.9         0.91895           0.503
v  CourantNb                  0.051452      2.1653e+05          331.97          162.67
v  FourierNb                    1.0042      2.4984e+06          215.12          63.175
v  total_pressure                94064      1.6538e+06      4.9548e+05      4.9868e+05
v  Local Time Step                0.01        0.014641        0.010002        0.010006


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.3548      2.5886e+06          547.09          225.85


 TIME FOR THE TIME STEP              100:        0.36647E+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        -0.333117359E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273268125E+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 0.26216E+04
   Friction velocity        uet   :  0.23649E-01 0.14059E+03
   Friction velocity        uk    :  0.23649E-01 0.14059E+03
   Dimensionless distance   yplus :  0.23462E+00 0.12714E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1050
   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    0.67890E+05    1803   0.99362E+00   0.12177E+05 
c  VelocityY    0.67890E+05    1803   0.99362E+00   0.00000E+00 
c  VelocityZ    0.67890E+05    1803   0.99362E+00   0.00000E+00 
c  Pressure     0.45822E+01     443   0.82301E-02   0.11686E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.4012e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1656.6          861.97         0.50063        -0.27254
v  Velocity[Y]                 -1011.8          1983.3         -1.0766        0.029206
v  Velocity[Z]                 -1168.1          1935.7         -1.8567         0.43768
v  ǁVelocityǁ                 0.018783          2479.7          12.797          8.1935
v  Pressure                -4.5497e+05      1.2837e+06         -4021.6         -505.72
v  turbulent_viscosity       0.0036118          5307.1         0.96369         0.52699
v  CourantNb                  0.085149       2.422e+05          302.94          164.46
v  FourierNb                    1.0179      2.7931e+06           229.6          66.073
v  total_pressure                45030      1.7837e+06      4.9598e+05      4.9949e+05
v  Local Time Step                0.01        0.013489        0.010002        0.010007


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6305      2.8937e+06          532.54          230.53


 TIME FOR THE TIME STEP              101:        0.33501E+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        -0.312424920E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273295180E+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 0.29365E+04
   Friction velocity        uet   :  0.18421E-01 0.15547E+03
   Friction velocity        uk    :  0.18421E-01 0.15547E+03
   Dimensionless distance   yplus :  0.22486E+00 0.14060E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1408
   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    0.86155E+05    1833   0.10018E+01   0.12819E+05 
c  VelocityY    0.86155E+05    1833   0.10018E+01   0.00000E+00 
c  VelocityZ    0.86155E+05    1833   0.10018E+01   0.00000E+00 
c  Pressure     0.51139E+01     566   0.10146E-01   0.11682E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.0786e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                   -1959          961.25         -2.0869        -0.35159
v  Velocity[Y]                 -1137.4          2185.7        -0.41541      -0.0096364
v  Velocity[Z]                 -1265.4          2181.6          1.9589         0.50573
v  ǁVelocityǁ                 0.015685            2706          15.845          10.783
v  Pressure                -5.1243e+05      1.4231e+06         -2433.3          1317.1
v  turbulent_viscosity       0.0028699          5957.1          1.0713         0.57053
v  CourantNb                  0.041692      2.7004e+05          313.38          150.35
v  FourierNb                   0.97293      3.1327e+06          255.89          72.583
v  total_pressure               -12431      1.9231e+06      4.9757e+05      5.0132e+05
v  Local Time Step                0.01          0.0121        0.010003        0.010009


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.6284      3.2432e+06          569.27          222.93


 TIME FOR THE TIME STEP              102:        0.30314E+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         0.199882790E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273299624E+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 0.32334E+04
   Friction velocity        uet   :  0.31661E-01 0.16937E+03
   Friction velocity        uk    :  0.31661E-01 0.16937E+03
   Dimensionless distance   yplus :  0.22202E+00 0.15317E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        860
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10397E+06    1964   0.99777E+00   0.32700E+05 
c  VelocityY    0.10397E+06    1964   0.99777E+00   0.00000E+00 
c  VelocityZ    0.10397E+06    1964   0.99777E+00   0.00000E+00 
c  Pressure     0.57634E+01     519   0.98230E-02   0.11789E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.0176e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                   -2044          1117.3         -1.1748        -0.33285
v  Velocity[Y]                 -1277.9          2429.6         -1.2894      -0.0077422
v  Velocity[Z]                   -1434          2387.8         0.50858         0.40902
v  ǁVelocityǁ                0.0067566          3023.8          20.092          14.368
v  Pressure                -6.2464e+05      1.5306e+06          -11465         -5753.9
v  turbulent_viscosity       0.0030742          6551.4          1.2108         0.66467
v  CourantNb                   0.16795      3.0219e+05          377.69          192.93
v  FourierNb                   0.84604      3.8801e+06          292.35          82.475
v  total_pressure          -1.2464e+05      2.0306e+06      4.8853e+05      4.9425e+05
v  Local Time Step                0.01          0.0121        0.010001        0.010005


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2731      4.0046e+06          670.04          275.41


 TIME FOR THE TIME STEP              103:        0.36285E+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        -0.268364565E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273264816E+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 0.36052E+04
   Friction velocity        uet   :  0.27251E-01 0.18659E+03
   Friction velocity        uk    :  0.27251E-01 0.18659E+03
   Dimensionless distance   yplus :  0.23596E+00 0.16875E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        992
   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    0.12904E+06    1995   0.99501E+00   0.29752E+05 
c  VelocityY    0.12904E+06    1995   0.99501E+00   0.00000E+00 
c  VelocityZ    0.12904E+06    1995   0.99501E+00   0.00000E+00 
c  Pressure     0.64699E+01     536   0.97484E-02   0.11856E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      9.7828e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2296.4          1180.2          1.5362        -0.40806
v  Velocity[Y]                 -1410.5          2726.1          -1.496       -0.055622
v  Velocity[Z]                 -1614.8          2661.1         -2.6824         0.82112
v  ǁVelocityǁ                   0.0316          3408.5          17.553            11.9
v  Pressure                -7.0102e+05      1.6998e+06         -6862.6           -1993
v  turbulent_viscosity       0.0021004            7298          1.4079         0.78071
v  CourantNb                  0.046967      3.3544e+05          469.96          254.49
v  FourierNb                   0.93474      3.8419e+06          326.85          95.478
v  total_pressure          -2.0102e+05      2.1998e+06      4.9314e+05      4.9801e+05
v  Local Time Step                0.01         0.01331        0.010001        0.010004


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.4243      3.9808e+06          796.81          349.97


 TIME FOR THE TIME STEP              104:        0.32571E+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         0.436775822E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273304970E+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 0.40686E+04
   Friction velocity        uet   :  0.38159E-01 0.20781E+03
   Friction velocity        uk    :  0.38159E-01 0.20781E+03
   Dimensionless distance   yplus :  0.37380E+00 0.18794E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        441
   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    0.16321E+06    2051   0.10008E+01   0.56157E+05 
c  VelocityY    0.16321E+06    2051   0.10008E+01   0.00000E+00 
c  VelocityZ    0.16321E+06    2051   0.10008E+01   0.00000E+00 
c  Pressure     0.74728E+01     551   0.13345E-01   0.12261E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.0565e-06                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2727.1          1315.1         -3.0391        -0.51382
v  Velocity[Y]                 -1556.7          3007.4        -0.43834        -0.10387
v  Velocity[Z]                 -1767.5          2984.9          1.5894         0.95113
v  ǁVelocityǁ                   0.0622          3743.2          30.935          20.584
v  Pressure                 -8.059e+05      1.8651e+06         -3231.4          514.77
v  turbulent_viscosity       0.0034875          8183.1          1.5123         0.85808
v  CourantNb                   0.04439      3.7147e+05          423.45          212.08
v  FourierNb                   0.97728       4.838e+06          360.57          103.03
v  total_pressure           -3.059e+05      2.3651e+06      4.9677e+05      5.0051e+05
v  Local Time Step                0.01           0.011            0.01        0.010001


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.9747      4.9918e+06          784.01          315.12


 TIME FOR THE TIME STEP              105:        0.33754E+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         0.105633460E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273302697E+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 0.44758E+04
   Friction velocity        uet   :  0.42447E-01 0.22627E+03
   Friction velocity        uk    :  0.42447E-01 0.22627E+03
   Dimensionless distance   yplus :  0.37425E+00 0.20463E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        141
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.19743E+06    2623   0.99171E+00   0.90971E+05 
c  VelocityY    0.19743E+06    2623   0.99171E+00   0.00000E+00 
c  VelocityZ    0.19743E+06    2623   0.99171E+00   0.00000E+00 
c  Pressure     0.81175E+01     546   0.10359E-01   0.11952E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step       7.184e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2781.2            1518         -1.4522        -0.32478
v  Velocity[Y]                 -1736.1          3377.2          -1.295       -0.090895
v  Velocity[Z]                 -1974.5          3315.6           2.746         0.41274
v  ǁVelocityǁ                  0.05992          4197.1          27.459          19.523
v  Pressure                -9.4774e+05      2.0323e+06          -11981           -7724
v  turbulent_viscosity       0.0062179          9013.2          1.8962          1.0968
v  CourantNb                   0.50515       4.176e+05          726.47          367.88
v  FourierNb                    1.2074      5.3401e+06          433.86          129.48
v  total_pressure          -4.4774e+05      2.5323e+06      4.8802e+05      4.9228e+05
v  Local Time Step                0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.1967      5.5127e+06          1160.3          497.37


 TIME FOR THE TIME STEP              106:        0.41800E+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        -0.711221504E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273261551E+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 0.50205E+04
   Friction velocity        uet   :  0.15960E-01 0.25072E+03
   Friction velocity        uk    :  0.15960E-01 0.25072E+03
   Dimensionless distance   yplus :  0.21225E+00 0.22674E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        335
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.25155E+06    2087   0.10030E+01   0.56942E+05 
c  VelocityY    0.25155E+06    2087   0.10030E+01   0.00000E+00 
c  VelocityZ    0.25155E+06    2087   0.10030E+01   0.00000E+00 
c  Pressure     0.92222E+01     607   0.10390E-01   0.12133E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      5.9602e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3309.2            1663          1.2153        -0.56876
v  Velocity[Y]                 -1986.2          3721.7         -2.3677        -0.27037
v  Velocity[Z]                 -2164.1          3732.5          -1.868           1.228
v  ǁVelocityǁ                 0.063006          4599.3          23.394          15.925
v  Pressure                -1.0399e+06       2.275e+06          5819.2          6340.9
v  turbulent_viscosity       0.0068085           10140          1.9464          1.0953
v  CourantNb                   0.23959      4.6378e+05          641.26          343.13
v  FourierNb                    1.2155      5.3309e+06          448.42          131.41
v  total_pressure          -5.3988e+05       2.775e+06      5.0582e+05      5.0634e+05
v  Local Time Step                0.01           0.011            0.01        0.010001


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.4025        5.52e+06          1089.7          474.54


 TIME FOR THE TIME STEP              107:        0.33206E+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        -0.538955960E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273312747E+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 0.55510E+04
   Friction velocity        uet   :  0.32647E-01 0.27428E+03
   Friction velocity        uk    :  0.32647E-01 0.27428E+03
   Dimensionless distance   yplus :  0.38799E+00 0.24804E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        303
   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    0.30254E+06    2085   0.99429E+00   0.58540E+05 
c  VelocityY    0.30254E+06    2085   0.99429E+00   0.00000E+00 
c  VelocityZ    0.30254E+06    2085   0.99429E+00   0.00000E+00 
c  Pressure     0.10122E+02     516   0.13149E-01   0.11929E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      5.9282e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3577.4          1838.8         -2.7616         -0.6154
v  Velocity[Y]                 -2146.7          4170.7         -1.1385        -0.17072
v  Velocity[Z]                 -2529.2          4031.5         0.30458          1.4386
v  ǁVelocityǁ                  0.05117          5240.1          33.139          23.956
v  Pressure                -1.2205e+06      2.4652e+06         -497.97          2662.5
v  turbulent_viscosity        0.005699           11141          2.1125          1.2039
v  CourantNb                 0.0096664      5.1545e+05          560.53          282.02
v  FourierNb                    1.2734      5.8777e+06          488.93          142.58
v  total_pressure          -7.2052e+05      2.9652e+06       4.995e+05      5.0266e+05
v  Local Time Step                0.01           0.011            0.01        0.010001


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.5548      6.0923e+06          1049.5          424.61


 TIME FOR THE TIME STEP              108:        0.33569E+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         0.199339337E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273313475E+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 0.62694E+04
   Friction velocity        uet   :  0.48752E-01 0.30585E+03
   Friction velocity        uk    :  0.48752E-01 0.30585E+03
   Dimensionless distance   yplus :  0.36682E+00 0.27660E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         77
   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    0.38311E+06    2668   0.99386E+00   0.14332E+06 
c  VelocityY    0.38311E+06    2668   0.99386E+00   0.00000E+00 
c  VelocityZ    0.38311E+06    2668   0.99386E+00   0.00000E+00 
c  Pressure     0.11300E+02     550   0.11381E-01   0.11939E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      8.3765e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3887.1          2037.7          -4.848        -0.66109
v  Velocity[Y]                 -2417.6          4658.1         -2.3351        -0.17399
v  Velocity[Z]                 -2713.1          4648.3          6.6026         0.92903
v  ǁVelocityǁ                 0.038784          5782.4          43.635          28.944
v  Pressure                -1.4577e+06      2.6563e+06          -23483          -15603
v  turbulent_viscosity       0.0074939           12525          2.5428          1.4988
v  CourantNb                   0.61308      5.7548e+05          773.61          415.79
v  FourierNb                    1.5135      7.4079e+06          581.88          173.13
v  total_pressure          -9.5774e+05      3.1563e+06      4.7652e+05       4.844e+05
v  Local Time Step                0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4.8823      7.6472e+06          1355.5          588.93


 TIME FOR THE TIME STEP              109:        0.42006E+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         0.545604970E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273254010E+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 0.69661E+04
   Friction velocity        uet   :  0.41564E-01 0.33616E+03
   Friction velocity        uk    :  0.41564E-01 0.33616E+03
   Dimensionless distance   yplus :  0.62171E+00 0.30400E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        240
   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    0.47939E+06    2348   0.99967E+00   0.98418E+05 
c  VelocityY    0.47939E+06    2348   0.99967E+00   0.00000E+00 
c  VelocityZ    0.47939E+06    2348   0.99967E+00   0.00000E+00 
c  Pressure     0.12422E+02     594   0.10864E-01   0.11753E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.0077e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -4606.2          2329.4          1.5755        -0.82526
v  Velocity[Y]                 -2695.1          5108.5         -3.4339        -0.51458
v  Velocity[Z]                 -2947.8          5159.2         -1.5967          1.7362
v  ǁVelocityǁ                  0.04066          6279.2          30.204          19.911
v  Pressure                -1.5502e+06      3.0265e+06          4032.3          6055.3
v  turbulent_viscosity       0.0094452           13961          3.0937          1.7043
v  CourantNb                  0.027507      6.4163e+05          1027.4          519.15
v  FourierNb                    1.2623      7.3473e+06          689.58          206.34
v  total_pressure          -1.0502e+06      3.5265e+06      5.0403e+05      5.0606e+05
v  Local Time Step                0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.2885      7.6097e+06            1717          725.49


 TIME FOR THE TIME STEP              110:        0.37182E+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         0.366701249E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273326578E+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 0.76202E+04
   Friction velocity        uet   :  0.39715E-01 0.36435E+03
   Friction velocity        uk    :  0.39715E-01 0.36435E+03
   Dimensionless distance   yplus :  0.26029E+00 0.32950E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        332
   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    0.57355E+06    2443   0.99673E+00   0.21245E+06 
c  VelocityY    0.57355E+06    2443   0.99673E+00   0.00000E+00 
c  VelocityZ    0.57355E+06    2443   0.99673E+00   0.00000E+00 
c  Pressure     0.14350E+02     561   0.12179E-01   0.12135E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.6307e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -4973.1          2570.6         -1.8644         -1.2786
v  Velocity[Y]                 -3047.4          5732.2         -0.5914         -0.3755
v  Velocity[Z]                 -3403.4          5670.7          -1.797          1.7218
v  ǁVelocityǁ                  0.04674          7152.6          52.376          38.711
v  Pressure                -1.8698e+06       3.219e+06          -42838          -28424
v  turbulent_viscosity       0.0048891           15292          2.9662          1.6287
v  CourantNb                   0.22492      7.1477e+05          738.27          357.35
v  FourierNb                    1.2136      8.0634e+06          687.93          197.02
v  total_pressure          -1.3698e+06       3.719e+06      4.5716e+05      4.7158e+05
v  Local Time Step                0.01           0.011            0.01        0.010001


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2.1583      8.3567e+06          1426.2          554.37


 TIME FOR THE TIME STEP              111:        0.38456E+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        -0.284368581E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273249857E+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 0.86339E+04
   Friction velocity        uet   :  0.50478E-01 0.40761E+03
   Friction velocity        uk    :  0.50478E-01 0.40761E+03
   Dimensionless distance   yplus :  0.43048E+00 0.36862E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        125
   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    0.72451E+06    2744   0.99238E+00   0.27147E+06 
c  VelocityY    0.72451E+06    2744   0.99238E+00   0.00000E+00 
c  VelocityZ    0.72451E+06    2744   0.99238E+00   0.00000E+00 
c  Pressure     0.15740E+02     514   0.11197E-01   0.11908E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.7201e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -5321.1          2853.4         -3.7766         -1.0972
v  Velocity[Y]                 -3312.9          6415.8          -3.928        -0.46897
v  Velocity[Z]                 -3803.7          6307.8        -0.56255          1.8634
v  ǁVelocityǁ                 0.053524          7968.7           48.43          34.088
v  Pressure                -2.1023e+06      3.5688e+06          -51619          -37858
v  turbulent_viscosity       0.0069712           17197          3.7224          2.2066
v  CourantNb                   0.39617       7.937e+05          1204.2          668.86
v  FourierNb                    1.2929      9.0589e+06          821.15          252.46
v  total_pressure          -1.6023e+06      4.0688e+06      4.4838e+05      4.6214e+05
v  Local Time Step                0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.0814      9.3895e+06          2025.3          921.32


 TIME FOR THE TIME STEP              112:        0.41943E+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         0.490040087E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273322995E+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 0.96440E+04
   Friction velocity        uet   :  0.41132E-01 0.45026E+03
   Friction velocity        uk    :  0.41132E-01 0.45026E+03
   Dimensionless distance   yplus :  0.67949E+00 0.40720E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         89
   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    0.91264E+06    2832   0.99918E+00   0.26219E+06 
c  VelocityY    0.91264E+06    2832   0.99918E+00   0.00000E+00 
c  VelocityZ    0.91264E+06    2832   0.99918E+00   0.00000E+00 
c  Pressure     0.18206E+02     587   0.13221E-01   0.12290E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.2494e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                   -6488          3198.9         -3.1059         -1.2933
v  Velocity[Y]                 -3769.9          7110.1         -5.5344        -0.76128
v  Velocity[Z]                 -4142.5            7142          2.0922          2.1424
v  ǁVelocityǁ                  0.14848          8788.5            63.1          43.171
v  Pressure                -2.3294e+06      3.9906e+06          -25888          -17131
v  turbulent_viscosity       0.0089463           19231          3.6924          2.1427
v  CourantNb                   0.40029      8.7865e+05          1146.7             597
v  FourierNb                    1.6069      1.0118e+07          846.04          247.95
v  total_pressure          -1.8294e+06      4.4906e+06      4.7411e+05      4.8287e+05
v  Local Time Step                0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          5.0893       1.048e+07          1992.8          844.95


 TIME FOR THE TIME STEP              113:        0.43477E+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        -0.404825805E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273333868E+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 0.10669E+05
   Friction velocity        uet   :  0.40245E-01 0.49313E+03
   Friction velocity        uk    :  0.40245E-01 0.49313E+03
   Dimensionless distance   yplus :  0.65278E+00 0.44597E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         98
   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    0.11129E+07    2516   0.98753E+00   0.22100E+06 
c  VelocityY    0.11129E+07    2516   0.98753E+00   0.00000E+00 
c  VelocityZ    0.11129E+07    2516   0.98753E+00   0.00000E+00 
c  Pressure     0.19406E+02     603   0.11343E-01   0.11755E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.9744e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -6565.7          3556.9          3.1195         -1.5421
v  Velocity[Y]                 -4134.2          7945.4         -5.1194         -0.9192
v  Velocity[Z]                 -4701.8          7768.3          -3.659          3.1774
v  ǁVelocityǁ                 0.073282          9862.6          48.957           33.69
v  Pressure                -2.5205e+06      4.5198e+06           29717           23215
v  turbulent_viscosity        0.010339           21274          4.5912          2.6344
v  CourantNb                   0.43231      9.8824e+05          1486.7          764.35
v  FourierNb                      1.51      1.1222e+07          1027.3          307.54
v  total_pressure          -2.0205e+06      5.0198e+06      5.2972e+05      5.2322e+05
v  Local Time Step                0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4.3571      1.1629e+07          2514.1          1071.9


 TIME FOR THE TIME STEP              114:        0.38818E+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         0.231552246E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273333248E+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 0.11930E+05
   Friction velocity        uet   :  0.45158E-01 0.54539E+03
   Friction velocity        uk    :  0.45158E-01 0.54539E+03
   Dimensionless distance   yplus :  0.61875E+00 0.49322E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         88
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         15 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.14075E+07    2424   0.10031E+01   0.34575E+06 
c  VelocityY    0.14075E+07    2424   0.10031E+01   0.00000E+00 
c  VelocityZ    0.14075E+07    2424   0.10031E+01   0.00000E+00 
c  Pressure     0.22825E+02     538   0.13293E-01   0.12330E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.6374e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -8067.4          3804.3         -2.5104         -1.5718
v  Velocity[Y]                 -4620.1          8864.1         -4.2426         -0.7535
v  Velocity[Z]                 -5145.9          8980.2        0.035383           3.435
v  ǁVelocityǁ                 0.092107           10965          73.168          54.489
v  Pressure                -2.9687e+06      4.8639e+06         -1997.5            2304
v  turbulent_viscosity        0.009243           23823          4.7429          2.7456
v  CourantNb                   0.30339      1.0957e+06          1183.9          592.88
v  FourierNb                     1.483      1.4085e+07          1096.1          319.04
v  total_pressure          -2.4687e+06      5.3639e+06        4.98e+05       5.023e+05
v  Local Time Step                0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.1539      1.4529e+07            2280          911.92


 TIME FOR THE TIME STEP              115:        0.38272E+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         0.304635066E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273218135E+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 0.13412E+05
   Friction velocity        uet   :  0.44442E-01 0.60615E+03
   Friction velocity        uk    :  0.44442E-01 0.60615E+03
   Dimensionless distance   yplus :  0.41359E+00 0.54817E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         50
   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    0.17297E+07    2434   0.99253E+00   0.37970E+06 
c  VelocityY    0.17297E+07    2434   0.99253E+00   0.00000E+00 
c  VelocityZ    0.17297E+07    2434   0.99253E+00   0.00000E+00 
c  Pressure     0.25014E+02     625   0.14695E-01   0.12099E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.0393e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -8470.4          4485.9         -9.7205         -2.1094
v  Velocity[Y]                 -5239.7          9778.7         -11.635         -1.3795
v  Velocity[Z]                 -5981.5          9488.3          10.331          5.2738
v  ǁVelocityǁ                  0.22383           12207          59.764          45.768
v  Pressure                -3.2603e+06      5.4505e+06           72074           65659
v  turbulent_viscosity        0.012235           26499          5.8013          3.4573
v  CourantNb                   0.55055      1.2191e+06            1687          935.91
v  FourierNb                    1.8426      1.3981e+07          1277.5          392.05
v  total_pressure          -2.7603e+06      5.9505e+06      5.7207e+05      5.6566e+05
v  Local Time Step                0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.9713      1.4491e+07          2964.5            1328


 TIME FOR THE TIME STEP              116:        0.44604E+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         0.461498728E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273365682E+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 0.14792E+05
   Friction velocity        uet   :  0.71579E-01 0.66220E+03
   Friction velocity        uk    :  0.71579E-01 0.66220E+03
   Dimensionless distance   yplus :  0.83364E+00 0.59886E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         16
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         17 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.21345E+07    2617   0.98977E+00   0.11119E+07 
c  VelocityY    0.21345E+07    2617   0.98977E+00   0.00000E+00 
c  VelocityZ    0.21345E+07    2617   0.98977E+00   0.00000E+00 
c  Pressure     0.29600E+02     588   0.14974E-01   0.12802E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.5985e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -9424.7          4655.9         0.92798         -1.9808
v  Velocity[Y]                 -5577.6           11063         0.33315          -1.003
v  Velocity[Z]                 -6637.2           11184         -14.647          4.6124
v  ǁVelocityǁ                  0.12094           13904          120.05          85.293
v  Pressure                -3.8872e+06      5.8161e+06          -12966         -6925.2
v  turbulent_viscosity        0.013376           29308          6.4166          4.0228
v  CourantNb                    1.4669      1.3556e+06          1405.2           756.4
v  FourierNb                    2.7187       1.735e+07          1421.5          439.43
v  total_pressure          -3.3872e+06      6.3161e+06      4.8703e+05      4.9307e+05
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.284      1.7912e+07          2826.8          1195.8


 TIME FOR THE TIME STEP              117:        0.40805E+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         0.304653844E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273193264E+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 0.16843E+05
   Friction velocity        uet   :  0.26723E-01 0.74472E+03
   Friction velocity        uk    :  0.26723E-01 0.74472E+03
   Dimensionless distance   yplus :  0.69576E+00 0.67349E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         31
   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    0.27326E+07    2525   0.99789E+00   0.17282E+07 
c  VelocityY    0.27326E+07    2525   0.99789E+00   0.00000E+00 
c  VelocityZ    0.27326E+07    2525   0.99789E+00   0.00000E+00 
c  Pressure     0.32262E+02     590   0.14902E-01   0.12482E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.0905e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -10939          5656.1         -11.362         -2.7855
v  Velocity[Y]                 -6563.8           11988         -3.5252         -1.9588
v  Velocity[Z]                 -7018.2           12072          3.5746          5.3117
v  ǁVelocityǁ                  0.25279           14718           129.3          86.351
v  Pressure                -4.2042e+06      6.5754e+06           49260           28809
v  turbulent_viscosity        0.016416           33134          8.4478          5.1699
v  CourantNb                     0.774      1.5169e+06          2776.7          1488.3
v  FourierNb                    2.4979      1.7455e+07          1778.1          574.75
v  total_pressure          -3.7042e+06      7.0754e+06      5.4926e+05      5.2881e+05
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.6684       1.808e+07          4554.8            2063


 TIME FOR THE TIME STEP              118:        0.40105E+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         0.108834772E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273386282E+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 0.18035E+05
   Friction velocity        uet   :  0.70696E-01 0.79224E+03
   Friction velocity        uk    :  0.70696E-01 0.79224E+03
   Dimensionless distance   yplus :  0.49155E+00 0.71647E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         14
   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    0.31822E+07    3480   0.99602E+00   0.20415E+07 
c  VelocityY    0.31822E+07    3480   0.99602E+00   0.00000E+00 
c  VelocityZ    0.31822E+07    3480   0.99602E+00   0.00000E+00 
c  Pressure     0.35145E+02     600   0.12350E-01   0.12225E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.0178e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -11765          6084.9         -12.132         -2.7507
v  Velocity[Y]                 -6991.1           13512        -0.75376          -1.357
v  Velocity[Z]                 -7902.7           13621          12.744          3.5138
v  ǁVelocityǁ                  0.11653           16764          128.74          90.981
v  Pressure                -4.9574e+06      7.0362e+06          -48984          -57873
v  turbulent_viscosity        0.023314           35809           8.829          5.2802
v  CourantNb                   0.90932      1.6835e+06          3042.8          1533.1
v  FourierNb                    2.8522      1.8902e+07          1883.3           595.3
v  total_pressure          -4.4574e+06      7.5362e+06      4.5102e+05      4.4213e+05
v  Local Time Step                0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           8.036      1.9592e+07          4926.1          2128.4


 TIME FOR THE TIME STEP              119:        0.56723E+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         0.163392806E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273193416E+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 0.20497E+05
   Friction velocity        uet   :  0.55939E-01 0.88962E+03
   Friction velocity        uk    :  0.55939E-01 0.88962E+03
   Dimensionless distance   yplus :  0.66992E+00 0.80453E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         47
   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    0.40532E+07    2447   0.99119E+00   0.20656E+07 
c  VelocityY    0.40532E+07    2447   0.99119E+00   0.00000E+00 
c  VelocityZ    0.40532E+07    2447   0.99119E+00   0.00000E+00 
c  Pressure     0.38657E+02     590   0.12678E-01   0.12041E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.8443e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -12610          6747.2        -0.42575          -2.891
v  Velocity[Y]                 -8012.7           15025         -9.5712         -2.1116
v  Velocity[Z]                 -8997.3           14796         -4.6509          6.5315
v  ǁVelocityǁ                  0.13456           18663          123.01          86.466
v  Pressure                -5.4615e+06      7.8852e+06           22077         -4471.2
v  turbulent_viscosity        0.025407           40504          9.2168          5.4091
v  CourantNb                   0.87786      1.8766e+06            2979          1597.3
v  FourierNb                     3.643       2.134e+07          2010.8          620.52
v  total_pressure          -4.9615e+06      8.3852e+06      5.2208e+05      4.9553e+05
v  Local Time Step                0.01           0.011            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.2329      2.2119e+07          4989.9          2217.8


 TIME FOR THE TIME STEP              120:        0.42107E+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         0.743141435E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273402535E+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 0.22825E+05
   Friction velocity        uet   :  0.77870E-01 0.98079E+03
   Friction velocity        uk    :  0.77870E-01 0.98079E+03
   Dimensionless distance   yplus :  0.76649E+00 0.88698E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         20
   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    0.50391E+07    3063   0.99835E+00   0.21588E+07 
c  VelocityY    0.50391E+07    3063   0.99835E+00   0.00000E+00 
c  VelocityZ    0.50391E+07    3063   0.99835E+00   0.00000E+00 
c  Pressure     0.43883E+02     444   0.14020E-01   0.12214E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.3855e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -15295          7730.1         -15.502         -3.0475
v  Velocity[Y]                 -8656.7           16727         -11.905         -2.0728
v  Velocity[Z]                 -9735.6           16926          10.741          6.4184
v  ǁVelocityǁ                 0.058378           20605          163.69          115.29
v  Pressure                -6.3032e+06      8.5707e+06          605.15          -24853
v  turbulent_viscosity        0.035874           44962          9.6047          5.6487
v  CourantNb                   0.18582      2.0675e+06          2890.8          1513.4
v  FourierNb                      3.61      2.3679e+07          2123.9          644.08
v  total_pressure          -5.8032e+06      9.0707e+06      5.0061e+05      4.7515e+05
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.0812      2.4533e+07          5014.8          2157.5


 TIME FOR THE TIME STEP              121:        0.47304E+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        -0.563300672E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273341616E+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 0.25303E+05
   Friction velocity        uet   :  0.68489E-01 0.10769E+04
   Friction velocity        uk    :  0.68489E-01 0.10769E+04
   Dimensionless distance   yplus :  0.69678E+00 0.97394E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         59
   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    0.62057E+07    2422   0.98811E+00   0.17102E+07 
c  VelocityY    0.62057E+07    2422   0.98811E+00   0.00000E+00 
c  VelocityZ    0.62057E+07    2422   0.98811E+00   0.00000E+00 
c  Pressure     0.48506E+02     627   0.13056E-01   0.12071E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.4435e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -16481          8398.7          5.0152         -4.7414
v  Velocity[Y]                  -10039           18628         -15.959          -3.307
v  Velocity[Z]                  -11301           18281         -10.441          9.4944
v  ǁVelocityǁ                  0.25729           23230           122.4          84.592
v  Pressure                -6.7601e+06       9.791e+06      2.0478e+05      1.1793e+05
v  turbulent_viscosity        0.024625           50034          11.162          6.5872
v  CourantNb                    1.1581      2.3313e+06          3800.3            2015
v  FourierNb                    3.9909      2.9664e+07          2494.5           751.7
v  total_pressure          -6.2601e+06      1.0291e+07      7.0478e+05      6.1793e+05
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.393      3.0625e+07          6294.9          2766.7


 TIME FOR THE TIME STEP              122:        0.38497E+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        -0.365884312E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273439120E+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 0.28319E+05
   Friction velocity        uet   :  0.45011E-01 0.11930E+04
   Friction velocity        uk    :  0.45011E-01 0.11930E+04
   Dimensionless distance   yplus :  0.81783E+00 0.10789E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         10
   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    0.77691E+07    2622   0.99113E+00   0.17398E+07 
c  VelocityY    0.77691E+07    2622   0.99113E+00   0.00000E+00 
c  VelocityZ    0.77691E+07    2622   0.99113E+00   0.00000E+00 
c  Pressure     0.54192E+02     565   0.14369E-01   0.12049E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.1396e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -17324          9512.1         -15.454         -3.7128
v  Velocity[Y]                  -10616           21032         -9.0703         -2.3033
v  Velocity[Z]                  -12145           21105          5.1221          9.4432
v  ǁVelocityǁ                  0.51773           25861          177.45           130.5
v  Pressure                -7.6898e+06      1.0771e+07      2.6928e+05       1.783e+05
v  turbulent_viscosity        0.031253           55776          11.888          7.2274
v  CourantNb                    1.1775      2.6066e+06            2931          1464.4
v  FourierNb                    3.7621      3.3027e+07          2675.2          805.78
v  total_pressure          -7.1898e+06      1.1271e+07      7.6928e+05       6.783e+05
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.344      3.4092e+07          5606.2          2270.2


 TIME FOR THE TIME STEP              123:        0.40390E+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         0.202278350E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273431726E+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 0.31904E+05
   Friction velocity        uet   :  0.76748E-01 0.13295E+04
   Friction velocity        uk    :  0.76748E-01 0.13295E+04
   Dimensionless distance   yplus :  0.11767E+01 0.12024E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          6
   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    0.99032E+07    2746   0.99903E+00   0.25956E+07 
c  VelocityY    0.99032E+07    2746   0.99903E+00   0.00000E+00 
c  VelocityZ    0.99032E+07    2746   0.99903E+00   0.00000E+00 
c  Pressure     0.61571E+02     653   0.15360E-01   0.12212E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.4603e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -20776           10519         -23.858         -5.5999
v  Velocity[Y]                  -12798           22894         -30.055         -4.6365
v  Velocity[Z]                  -13516           23135          30.576          12.292
v  ǁVelocityǁ                  0.13222           28135          187.03          125.13
v  Pressure                -8.2907e+06      1.2232e+07       5.575e+05      3.7778e+05
v  turbulent_viscosity        0.060185           62914          13.761          8.5192
v  CourantNb                    3.0493      2.8872e+06          4117.1          2239.9
v  FourierNb                    4.6377      3.3114e+07          2996.9          937.85
v  total_pressure          -7.7907e+06      1.2732e+07      1.0575e+06      8.7778e+05
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.591      3.4292e+07            7114          3177.7


 TIME FOR THE TIME STEP              124:        0.44624E+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         0.133738288E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273433742E+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 0.34806E+05
   Friction velocity        uet   :  0.83179E-01 0.14392E+04
   Friction velocity        uk    :  0.83179E-01 0.14392E+04
   Dimensionless distance   yplus :  0.10982E+01 0.13015E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          4
   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    0.11654E+08    2544   0.99138E+00   0.54924E+07 
c  VelocityY    0.11654E+08    2544   0.99138E+00   0.00000E+00 
c  VelocityZ    0.11654E+08    2544   0.99138E+00   0.00000E+00 
c  Pressure     0.70198E+02     547   0.16568E-01   0.12448E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      8.0279e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -22681           11652          16.773         -7.9266
v  Velocity[Y]                  -13303           25788         -2.6411         -3.6495
v  Velocity[Z]                  -15625           25336         -45.696          13.072
v  ǁVelocityǁ                   1.2557           32209          257.09          187.27
v  Pressure                -9.9294e+06      1.2898e+07      4.4135e+05      2.5603e+05
v  turbulent_viscosity        0.046498           68333          16.582          9.8868
v  CourantNb                   0.80858      3.1927e+06          4423.2          2203.1
v  FourierNb                    4.0347      4.0553e+07          3615.2          1118.3
v  total_pressure          -9.4294e+06      1.3398e+07      9.4135e+05      7.5603e+05
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          18.634      4.1878e+07          8038.3          3321.4


 TIME FOR THE TIME STEP              125:        0.45385E+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         0.113798595E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273081016E+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 0.39487E+05
   Friction velocity        uet   :  0.76058E-01 0.16144E+04
   Friction velocity        uk    :  0.76058E-01 0.16144E+04
   Dimensionless distance   yplus :  0.10666E+01 0.14600E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         44 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.14877E+08    2625   0.98833E+00   0.70183E+07 
c  VelocityY    0.14877E+08    2625   0.98833E+00   0.00000E+00 
c  VelocityZ    0.14877E+08    2625   0.98833E+00   0.00000E+00 
c  Pressure     0.73552E+02     468   0.12898E-01   0.11699E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.6662e-07                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -24552           12501         -32.123         -6.2783
v  Velocity[Y]                  -15277           28941         -18.612         -3.3863
v  Velocity[Z]                  -17414           28446          36.488          12.722
v  ǁVelocityǁ                  0.39139           36082          250.06          162.75
v  Pressure                -1.1421e+07      1.4026e+07      3.6846e+05      2.0016e+05
v  turbulent_viscosity        0.085728           77260          19.477          12.347
v  CourantNb                    3.5926      3.5664e+06          5950.5          3212.5
v  FourierNb                     7.585      4.0695e+07          4073.4          1333.5
v  total_pressure          -1.0921e+07      1.4526e+07      8.6846e+05      7.0016e+05
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          24.645      4.2176e+07           10024          4545.9


 TIME FOR THE TIME STEP              126:        0.40460E+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         0.198966133E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273330180E+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 0.44218E+05
   Friction velocity        uet   :  0.49554E-01 0.17899E+04
   Friction velocity        uk    :  0.49554E-01 0.17899E+04
   Dimensionless distance   yplus :  0.82125E+00 0.16187E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         11
   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    0.18819E+08    2818   0.99591E+00   0.47979E+07 
c  VelocityY    0.18819E+08    2818   0.99591E+00   0.00000E+00 
c  VelocityZ    0.18819E+08    2818   0.99591E+00   0.00000E+00 
c  Pressure     0.83752E+02     674   0.14243E-01   0.11923E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step       5.689e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -29098           14730         -7.7893         -6.1117
v  Velocity[Y]                  -16634           32014         -16.571         -6.4067
v  Velocity[Z]                  -18654           32288         -7.5372          19.511
v  ǁVelocityǁ                   1.8714           39209          227.63          173.49
v  Pressure                -1.1657e+07      1.6695e+07      1.1571e+06      8.6254e+05
v  turbulent_viscosity        0.059921           86543          19.649          11.453
v  CourantNb                   0.46593      3.9857e+06          5912.6          2920.2
v  FourierNb                    4.5461       4.559e+07          4266.7          1314.6
v  total_pressure          -1.1157e+07      1.7195e+07      1.6571e+06      1.3625e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.571      4.7221e+07           10179          4234.8


 TIME FOR THE TIME STEP              127:        0.45327E+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         0.204856392E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273538110E+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 :  0.16226E+00 0.48645E+05
   Friction velocity        uet   :  0.76756E-01 0.19527E+04
   Friction velocity        uk    :  0.76756E-01 0.19527E+04
   Dimensionless distance   yplus :  0.12261E+01 0.17659E+05
   ------------------------------------------------------
   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         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.22896E+08    2468   0.99093E+00   0.60333E+07 
c  VelocityY    0.22896E+08    2468   0.99093E+00   0.00000E+00 
c  VelocityZ    0.22896E+08    2468   0.99093E+00   0.00000E+00 
c  Pressure     0.98960E+02     573   0.17461E-01   0.12562E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      7.8997e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -32637           15898          15.134         -6.5463
v  Velocity[Y]                  -19478           35523         -32.519         -6.6304
v  Velocity[Z]                  -21464           35125         -20.952          21.377
v  ǁVelocityǁ                  0.22655           44232          362.21          252.79
v  Pressure                -1.3385e+07      1.8753e+07      1.2608e+06      9.1282e+05
v  turbulent_viscosity         0.23658           95625          21.499          13.868
v  CourantNb                    4.9885       4.453e+06          5336.4          2864.5
v  FourierNb                    15.815      5.0433e+07          4631.5          1472.7
v  total_pressure          -1.2885e+07      1.9253e+07      1.7608e+06      1.4128e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           60.42      5.2257e+07          9967.9          4337.3


 TIME FOR THE TIME STEP              128:        0.45085E+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        -0.118063349E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273566233E+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 0.54428E+05
   Friction velocity        uet   :  0.63818E-01 0.21636E+04
   Friction velocity        uk    :  0.63818E-01 0.21636E+04
   Dimensionless distance   yplus :  0.11228E+01 0.19567E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          4
   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    0.28318E+08    2518   0.99300E+00   0.60432E+07 
c  VelocityY    0.28318E+08    2518   0.99300E+00   0.00000E+00 
c  VelocityZ    0.28318E+08    2518   0.99300E+00   0.00000E+00 
c  Pressure     0.10431E+03     483   0.12888E-01   0.11852E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      7.6844e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -34497           18564         -34.966         -9.2595
v  Velocity[Y]                  -20445           39948         -18.913           -5.36
v  Velocity[Z]                  -23766           39631           22.96          23.263
v  ǁVelocityǁ                  0.76089           49236          234.04          185.25
v  Pressure                -1.5116e+07      2.0576e+07      1.2332e+06      8.8457e+05
v  turbulent_viscosity          0.1433      1.0622e+05          28.346          17.362
v  CourantNb                    1.7015      4.9678e+06          8424.9          4383.7
v  FourierNb                    9.0452      6.2961e+07          6023.1          1923.4
v  total_pressure          -1.4616e+07      2.1076e+07      1.7332e+06      1.3846e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          20.689      6.5004e+07           14448          6307.1


 TIME FOR THE TIME STEP              129:        0.38938E+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         0.138886307E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273566831E+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 :  0.45840E+00 0.61111E+05
   Friction velocity        uet   :  0.14984E+00 0.24052E+04
   Friction velocity        uk    :  0.14984E+00 0.24052E+04
   Dimensionless distance   yplus :  0.16404E+01 0.21751E+05
   ------------------------------------------------------
   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         42 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.35811E+08    2472   0.99055E+00   0.62544E+07 
c  VelocityY    0.35811E+08    2472   0.99055E+00   0.00000E+00 
c  VelocityZ    0.35811E+08    2472   0.99055E+00   0.00000E+00 
c  Pressure     0.12220E+03     572   0.17201E-01   0.12366E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      8.1473e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -38000           19283         -14.883         -8.7059
v  Velocity[Y]                  -24417           44443         -31.617         -7.3971
v  Velocity[Z]                  -27026           43694         -21.573          26.212
v  ǁVelocityǁ                  0.54962           55417          364.55          252.93
v  Pressure                -1.7196e+07      2.3861e+07      1.3159e+06      9.3826e+05
v  turbulent_viscosity         0.21881       1.195e+05           26.43          16.565
v  CourantNb                    1.0221      5.5068e+06          5447.2          3037.3
v  FourierNb                    13.311      6.2956e+07          5708.2          1800.4
v  total_pressure          -1.6696e+07      2.4361e+07      1.8159e+06      1.4383e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          41.045      6.5239e+07           11155          4837.7


 TIME FOR THE TIME STEP              130:        0.40829E+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        -0.262182616E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273711627E+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 0.68365E+05
   Friction velocity        uet   :  0.69642E-01 0.26650E+04
   Friction velocity        uk    :  0.69642E-01 0.26650E+04
   Dimensionless distance   yplus :  0.11017E+01 0.24101E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   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    0.44417E+08    2543   0.98929E+00   0.82418E+07 
c  VelocityY    0.44417E+08    2543   0.98929E+00   0.00000E+00 
c  VelocityZ    0.44417E+08    2543   0.98929E+00   0.00000E+00 
c  Pressure     0.12807E+03     591   0.13441E-01   0.11632E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.6565e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -41204           22486         -36.238         -8.8346
v  Velocity[Y]                  -25156           49510         -32.708         -8.0735
v  Velocity[Z]                  -29075           49369          33.669          28.495
v  ǁVelocityǁ                  0.70731           60722          346.45          260.39
v  Pressure                -1.8841e+07      2.6827e+07      1.6099e+06      1.1667e+06
v  turbulent_viscosity        0.097507      1.3276e+05          32.268          19.905
v  CourantNb                    2.4185      6.1042e+06            8599          4381.8
v  FourierNb                     8.672      7.8661e+07          6981.2          2194.4
v  total_pressure          -1.8341e+07      2.7327e+07      2.1099e+06      1.6667e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          21.464      8.1192e+07           15580          6576.2


 TIME FOR THE TIME STEP              131:        0.42399E+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         0.156928557E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273724068E+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 0.75539E+05
   Friction velocity        uet   :  0.19185E+00 0.29199E+04
   Friction velocity        uk    :  0.19185E+00 0.29199E+04
   Dimensionless distance   yplus :  0.14762E+01 0.26407E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          3
   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    0.55257E+08    2679   0.99679E+00   0.17445E+08 
c  VelocityY    0.55257E+08    2679   0.99679E+00   0.00000E+00 
c  VelocityZ    0.55257E+08    2679   0.99679E+00   0.00000E+00 
c  Pressure     0.14953E+03     475   0.15171E-01   0.12133E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      5.8324e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -51147           24233          18.131          -9.843
v  Velocity[Y]                  -30189           54116         -43.826         -9.2676
v  Velocity[Z]                  -31754           55664         -27.487          32.124
v  ǁVelocityǁ                  0.21937           66488          509.15           358.2
v  Pressure                -2.1319e+07       3.006e+07       1.613e+06      1.1294e+06
v  turbulent_viscosity         0.13191      1.4793e+05          33.423          20.851
v  CourantNb                    6.4447      6.7933e+06          8089.6          4372.9
v  FourierNb                    12.027       7.791e+07          7173.9          2273.6
v  total_pressure          -2.0819e+07       3.056e+07       2.113e+06      1.6294e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          42.736      8.0674e+07           15263          6646.4


 TIME FOR THE TIME STEP              132:        0.40470E+01

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


 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         0.340999100E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273634116E+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 0.82904E+05
   Friction velocity        uet   :  0.71667E-01 0.31797E+04
   Friction velocity        uk    :  0.71667E-01 0.31797E+04
   Dimensionless distance   yplus :  0.11369E+01 0.28756E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          5
   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    0.65594E+08    2673   0.98883E+00   0.25179E+08 
c  VelocityY    0.65594E+08    2673   0.98883E+00   0.00000E+00 
c  VelocityZ    0.65594E+08    2673   0.98883E+00   0.00000E+00 
c  Pressure     0.16103E+03     463   0.13950E-01   0.11724E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.1453e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -54639           27930         -32.688         -14.564
v  Velocity[Y]                  -31552           60574         -31.133         -9.2606
v  Velocity[Z]                  -36399           60063          1.4267          33.437
v  ǁVelocityǁ                   3.2016           75139          478.11          373.85
v  Pressure                -2.4078e+07        3.32e+07      1.6405e+06      1.1322e+06
v  turbulent_viscosity        0.081308      1.6143e+05          40.521          24.603
v  CourantNb                   0.24284      7.6053e+06           11923          6229.6
v  FourierNb                    6.8149      9.5863e+07          8792.7          2740.7
v  total_pressure          -2.3578e+07        3.37e+07      2.1405e+06      1.6322e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          14.046      9.8988e+07           20715          8970.3


 TIME FOR THE TIME STEP              133:        0.47480E+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         0.541564965E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273756621E+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 0.93035E+05
   Friction velocity        uet   :  0.17119E+00 0.35342E+04
   Friction velocity        uk    :  0.17119E+00 0.35342E+04
   Dimensionless distance   yplus :  0.14782E+01 0.31961E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          2
   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    0.82853E+08    2672   0.99417E+00   0.30655E+08 
c  VelocityY    0.82853E+08    2672   0.99417E+00   0.00000E+00 
c  VelocityZ    0.82853E+08    2672   0.99417E+00   0.00000E+00 
c  Pressure     0.18359E+03     470   0.15022E-01   0.11952E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      6.4586e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -60493           30031          9.8479         -16.921
v  Velocity[Y]                  -36818           67474         -52.992         -9.8615
v  Velocity[Z]                  -40614           67740         -38.989          40.256
v  ǁVelocityǁ                  0.67167           83700          663.63          443.62
v  Pressure                -2.7551e+07      3.6808e+07      1.6257e+06      1.0833e+06
v  turbulent_viscosity         0.22587      1.8139e+05          41.841          26.743
v  CourantNb                    7.3921      8.4955e+06           10993          6226.4
v  FourierNb                    17.607      1.0741e+08          9075.4          2873.2
v  total_pressure          -2.7051e+07      3.7308e+07      2.1257e+06      1.5833e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          95.325      1.1089e+08           20068          9099.6


 TIME FOR THE TIME STEP              134:        0.44151E+01

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


 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        -0.267870951E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273984290E+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 0.10414E+06
   Friction velocity        uet   :  0.10015E+00 0.39193E+04
   Friction velocity        uk    :  0.10015E+00 0.39193E+04
   Dimensionless distance   yplus :  0.11313E+01 0.35445E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          2
   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    0.10242E+09    3033   0.98625E+00   0.38811E+08 
c  VelocityY    0.10242E+09    3033   0.98625E+00   0.00000E+00 
c  VelocityZ    0.10242E+09    3033   0.98625E+00   0.00000E+00 
c  Pressure     0.20309E+03     588   0.15290E-01   0.11849E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.9303e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -62357           34594         -32.567         -17.712
v  Velocity[Y]                  -38391           75575         -48.988         -12.673
v  Velocity[Z]                  -44994           74654         -23.106          44.551
v  ǁVelocityǁ                   1.5513           93292             668          500.13
v  Pressure                -3.0533e+07       4.207e+07      2.0711e+06      1.4291e+06
v  turbulent_viscosity         0.12245      2.0157e+05          49.631          30.449
v  CourantNb                    3.6556       9.417e+06           15665            7837
v  FourierNb                    8.8511      1.0641e+08           10573          3356.8
v  total_pressure          -3.0033e+07       4.257e+07      2.5711e+06      1.9291e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          32.797      1.1033e+08           26238           11194


 TIME FOR THE TIME STEP              135:        0.53692E+01

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


 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         0.970126350E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273827186E+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 0.11596E+06
   Friction velocity        uet   :  0.23934E+00 0.43261E+04
   Friction velocity        uk    :  0.23934E+00 0.43261E+04
   Dimensionless distance   yplus :  0.17912E+01 0.39123E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          2
   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    0.12943E+09    2723   0.99575E+00   0.43160E+08 
c  VelocityY    0.12943E+09    2723   0.99575E+00   0.00000E+00 
c  VelocityZ    0.12943E+09    2723   0.99575E+00   0.00000E+00 
c  Pressure     0.22643E+03     552   0.14529E-01   0.11829E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.5438e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -78315           37142          12.674         -20.241
v  Velocity[Y]                  -46040           83004         -77.447          -14.37
v  Velocity[Z]                  -48899           84938         -54.159          50.761
v  ǁVelocityǁ                  0.51608      1.0213e+05          723.64          504.76
v  Pressure                -3.4231e+07      4.6437e+07      2.1727e+06       1.452e+06
v  turbulent_viscosity         0.24401      2.2611e+05          53.089          33.924
v  CourantNb                    26.208       1.049e+07           15487            8493
v  FourierNb                     21.95      1.1902e+08           11264          3636.1
v  total_pressure          -3.3731e+07      4.6937e+07      2.6727e+06       1.952e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          85.483      1.2328e+08           26751           12129


 TIME FOR THE TIME STEP              136:        0.49275E+01

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


 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        -0.326385088E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274013684E+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 :  0.12697E+00 0.12769E+06
   Friction velocity        uet   :  0.62975E-01 0.47265E+04
   Friction velocity        uk    :  0.62975E-01 0.47265E+04
   Dimensionless distance   yplus :  0.10710E+01 0.42744E+05
   ------------------------------------------------------
   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         34 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.15491E+09    2898   0.98867E+00   0.67815E+08 
c  VelocityY    0.15491E+09    2898   0.98867E+00   0.00000E+00 
c  VelocityZ    0.15491E+09    2898   0.98867E+00   0.00000E+00 
c  Pressure     0.25322E+03     531   0.15431E-01   0.11853E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.5965e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -83951           43183         -47.204         -25.684
v  Velocity[Y]                  -47906           92917         -39.357         -15.552
v  Velocity[Z]                  -55490           92190         -53.065          51.262
v  ǁVelocityǁ                   1.0254      1.1486e+05          899.85          670.96
v  Pressure                -3.9087e+07      5.2235e+07      2.2776e+06      1.4912e+06
v  turbulent_viscosity         0.18251      2.4759e+05          61.236          37.478
v  CourantNb                    1.4444      1.1724e+07           16960          8749.7
v  FourierNb                    10.582      1.3086e+08           13067            4146
v  total_pressure          -3.8587e+07      5.2735e+07      2.7776e+06      1.9912e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          34.744      1.3568e+08           30027           12896


 TIME FOR THE TIME STEP              137:        0.51177E+01

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


 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        -0.817955698E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273961795E+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 0.14309E+06
   Friction velocity        uet   :  0.13417E+00 0.52478E+04
   Friction velocity        uk    :  0.13417E+00 0.52478E+04
   Dimensionless distance   yplus :  0.13203E+01 0.47459E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          1
   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    0.19541E+09    2718   0.99375E+00   0.73303E+08 
c  VelocityY    0.19541E+09    2718   0.99375E+00   0.00000E+00 
c  VelocityZ    0.19541E+09    2718   0.99375E+00   0.00000E+00 
c  Pressure     0.27572E+03     600   0.13298E-01   0.11574E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.3663e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -92911           46406         -8.1431         -27.401
v  Velocity[Y]                  -56658      1.0332e+05         -104.89         -18.706
v  Velocity[Z]                  -62093      1.0366e+05         -28.594          59.873
v  ǁVelocityǁ                   1.7721      1.2791e+05          828.84          572.97
v  Pressure                -4.2957e+07      5.7793e+07      2.7041e+06      1.7413e+06
v  turbulent_viscosity         0.15374      2.7814e+05          66.698            42.3
v  CourantNb                    4.2036      1.3061e+07           20667           11460
v  FourierNb                    11.886      1.4651e+08           14118          4565.3
v  total_pressure          -4.2457e+07      5.8293e+07      3.2041e+06      2.2413e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          43.481      1.5185e+08           34786           16025


 TIME FOR THE TIME STEP              138:        0.46399E+01

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


 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        -0.366295976E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273968194E+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 :  0.45821E+00 0.15993E+06
   Friction velocity        uet   :  0.14079E+00 0.58136E+04
   Friction velocity        uk    :  0.14079E+00 0.58136E+04
   Dimensionless distance   yplus :  0.11852E+01 0.52575E+05
   ------------------------------------------------------
   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         27 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.24083E+09    2906   0.98563E+00   0.77780E+08 
c  VelocityY    0.24083E+09    2906   0.98563E+00   0.00000E+00 
c  VelocityZ    0.24083E+09    2906   0.98563E+00   0.00000E+00 
c  Pressure     0.31511E+03     614   0.15967E-01   0.11844E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.1359e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -96309           52371         -77.791         -19.146
v  Velocity[Y]                  -58919      1.1567e+05         -41.042         -19.387
v  Velocity[Z]                  -69248      1.1441e+05         -73.272          74.123
v  ǁVelocityǁ                   8.3087      1.4307e+05            1034          816.87
v  Pressure                -4.7196e+07      6.6641e+07      3.9651e+06      2.8336e+06
v  turbulent_viscosity         0.19126      3.0857e+05          73.626          45.247
v  CourantNb                    6.5701      1.4466e+07           19530          9976.5
v  FourierNb                    13.783      1.8306e+08           16081          4999.3
v  total_pressure          -4.6696e+07      6.7141e+07      4.4651e+06      3.3336e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          34.724      1.8907e+08           35611           14976


 TIME FOR THE TIME STEP              139:        0.44500E+01

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


 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         0.133464271E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274448767E+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 :  0.43074E+01 0.17839E+06
   Friction velocity        uet   :  0.74693E+00 0.64286E+04
   Friction velocity        uk    :  0.74693E+00 0.64286E+04
   Dimensionless distance   yplus :  0.29461E+01 0.58137E+05
   ------------------------------------------------------
   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         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30414E+09    2627   0.99460E+00   0.10315E+09 
c  VelocityY    0.30414E+09    2627   0.99460E+00   0.00000E+00 
c  VelocityZ    0.30414E+09    2627   0.99460E+00   0.00000E+00 
c  Pressure     0.34483E+03     573   0.14111E-01   0.11621E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.3402e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1955e+05           57446         -35.726         -28.158
v  Velocity[Y]                  -70487      1.2736e+05         -93.197          -23.96
v  Velocity[Z]                  -75096       1.305e+05         -19.903          79.406
v  ǁVelocityǁ                  0.46717      1.5642e+05          1065.8          737.98
v  Pressure                -5.2167e+07      7.3945e+07      4.3388e+06      3.0683e+06
v  turbulent_viscosity         0.68923      3.4602e+05          84.446          55.964
v  CourantNb                    98.612      1.6112e+07           23634           13532
v  FourierNb                    45.395      2.0476e+08           17942          5851.1
v  total_pressure          -5.1667e+07      7.4445e+07      4.8388e+06      3.5683e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          371.96      2.1132e+08           41576           19383


 TIME FOR THE TIME STEP              140:        0.47344E+01

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


 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         0.197610395E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274526444E+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 :  0.63916E+00 0.19643E+06
   Friction velocity        uet   :  0.16308E+00 0.70254E+04
   Friction velocity        uk    :  0.16308E+00 0.70254E+04
   Dimensionless distance   yplus :  0.11066E+01 0.63535E+05
   ------------------------------------------------------
   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         34 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.36602E+09    3025   0.98858E+00   0.15817E+09 
c  VelocityY    0.36602E+09    3025   0.98858E+00   0.00000E+00 
c  VelocityZ    0.36602E+09    3025   0.98858E+00   0.00000E+00 
c  Pressure     0.38764E+03     549   0.15053E-01   0.11720E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.6543e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.2959e+05           66249         -69.703         -36.834
v  Velocity[Y]                  -73590      1.4225e+05         -59.729         -26.232
v  Velocity[Z]                  -84973      1.4131e+05         -34.354            72.7
v  ǁVelocityǁ                   1.5263      1.7571e+05          1363.5          1024.8
v  Pressure                -6.1648e+07      8.3004e+07      4.6145e+06      3.1552e+06
v  turbulent_viscosity         0.40804      3.7984e+05          95.193          58.457
v  CourantNb                    3.5923      1.8007e+07           24967           12760
v  FourierNb                    23.345      2.2557e+08           20564          6464.7
v  total_pressure          -6.1148e+07      8.3504e+07      5.1145e+06      3.6552e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           50.73      2.3295e+08           45530           19224


 TIME FOR THE TIME STEP              141:        0.45934E+01

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


 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         0.791366077E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274225441E+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 0.21981E+06
   Friction velocity        uet   :  0.12004E+00 0.77926E+04
   Friction velocity        uk    :  0.12004E+00 0.77926E+04
   Dimensionless distance   yplus :  0.16302E+01 0.70472E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          2
   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    0.45903E+09    2726   0.99317E+00   0.16225E+09 
c  VelocityY    0.45903E+09    2726   0.99317E+00   0.00000E+00 
c  VelocityZ    0.45903E+09    2726   0.99317E+00   0.00000E+00 
c  Pressure     0.42471E+03     599   0.13656E-01   0.11525E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.8648e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.4211e+05           72066         -34.401         -41.724
v  Velocity[Y]                  -86820      1.5815e+05         -160.64         -28.657
v  Velocity[Z]                  -94853      1.5902e+05         -21.208          95.814
v  ǁVelocityǁ                  0.97312       1.954e+05          1169.6          820.85
v  Pressure                -6.7553e+07      9.1324e+07      5.1925e+06      3.5113e+06
v  turbulent_viscosity         0.20322      4.2565e+05          101.69          64.723
v  CourantNb                    4.9124      2.0051e+07           31262           17517
v  FourierNb                    17.278      2.2426e+08           21500            6974
v  total_pressure          -6.7053e+07      9.1824e+07      5.6925e+06      4.0113e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          95.822      2.3246e+08           52762           24491


 TIME FOR THE TIME STEP              142:        0.41932E+01

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


 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         0.271508347E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274391858E+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 :  0.24630E+00 0.24540E+06
   Friction velocity        uet   :  0.96695E-01 0.86260E+04
   Friction velocity        uk    :  0.96695E-01 0.86260E+04
   Dimensionless distance   yplus :  0.11082E+01 0.78010E+05
   ------------------------------------------------------
   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         35 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.56579E+09    2847   0.98516E+00   0.20129E+09 
c  VelocityY    0.56579E+09    2847   0.98516E+00   0.00000E+00 
c  VelocityZ    0.56579E+09    2847   0.98516E+00   0.00000E+00 
c  Pressure     0.49536E+03     636   0.17215E-01   0.12023E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step       1.568e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.4842e+05           79637         -91.744         -30.795
v  Velocity[Y]                  -90300      1.7708e+05         -53.199         -32.365
v  Velocity[Z]             -1.0631e+05      1.7529e+05         -146.84          120.79
v  ǁVelocityǁ                   3.7376      2.1917e+05          1755.3          1372.9
v  Pressure                 -7.589e+07      1.0613e+08      7.3241e+06      5.3779e+06
v  turbulent_viscosity         0.20446      4.7228e+05          113.94          70.944
v  CourantNb                    3.4707      2.2193e+07           27577           14146
v  FourierNb                    25.082       2.802e+08           24785            7763
v  total_pressure           -7.539e+07      1.0663e+08      7.8241e+06      5.8779e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          74.608      2.8941e+08           52362           21909


 TIME FOR THE TIME STEP              143:        0.44868E+01

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


 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         0.761211908E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274618038E+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 :  0.84276E+01 0.27416E+06
   Friction velocity        uet   :  0.99550E+00 0.95551E+04
   Friction velocity        uk    :  0.99550E+00 0.95551E+04
   Dimensionless distance   yplus :  0.12090E+02 0.86412E+05
   ------------------------------------------------------
   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         35 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.71459E+09    2745   0.99375E+00   0.25264E+09 
c  VelocityY    0.71459E+09    2745   0.99375E+00   0.00000E+00 
c  VelocityZ    0.71459E+09    2745   0.99375E+00   0.00000E+00 
c  Pressure     0.52458E+03     588   0.13594E-01   0.11442E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.4976e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8233e+05           89890         -150.81          -45.45
v  Velocity[Y]             -1.0819e+05      1.9487e+05         -145.19         -36.925
v  Velocity[Z]             -1.1496e+05      1.9915e+05          156.87          118.15
v  ǁVelocityǁ                   2.0128      2.3887e+05          1486.4          980.54
v  Pressure                -8.2238e+07      1.1815e+08      8.1048e+06      5.8868e+06
v  turbulent_viscosity           1.099      5.2958e+05          134.52          90.829
v  CourantNb                    68.958      2.4724e+07           39991           22789
v  FourierNb                     80.84      2.7885e+08           27694          9343.9
v  total_pressure          -8.1738e+07      1.1865e+08      8.6048e+06      6.3868e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          482.64      2.8892e+08           67685           32133


 TIME FOR THE TIME STEP              144:        0.42750E+01

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


 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         0.850300868E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275119141E+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 0.30115E+06
   Friction velocity        uet   :  0.13523E+00 0.10421E+05
   Friction velocity        uk    :  0.13523E+00 0.10421E+05
   Dimensionless distance   yplus :  0.14397E+01 0.94240E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          1
   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    0.85925E+09    2855   0.98824E+00   0.43397E+09 
c  VelocityY    0.85925E+09    2855   0.98824E+00   0.00000E+00 
c  VelocityZ    0.85925E+09    2855   0.98824E+00   0.00000E+00 
c  Pressure     0.60274E+03     620   0.15956E-01   0.11788E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.1252e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9876e+05      1.0056e+05         -140.93         -44.003
v  Velocity[Y]             -1.1226e+05      2.1786e+05         -18.482         -41.388
v  Velocity[Z]             -1.2987e+05      2.1764e+05         -338.49          131.97
v  ǁVelocityǁ                   4.3087      2.6882e+05          2247.6          1710.1
v  Pressure                -9.7648e+07      1.3303e+08      9.8022e+06      7.1133e+06
v  turbulent_viscosity          0.7427      5.8109e+05          146.39          88.983
v  CourantNb                    2.1006      2.7604e+07           35439           17251
v  FourierNb                     44.08      3.0715e+08           31079          9899.7
v  total_pressure          -9.7148e+07      1.3353e+08      1.0302e+07      7.6133e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          77.629      3.1844e+08           66518           27151


 TIME FOR THE TIME STEP              145:        0.44780E+01

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


 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         0.127647452E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274870633E+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 :  0.38923E+01 0.33763E+06
   Friction velocity        uet   :  0.74095E+00 0.11582E+05
   Friction velocity        uk    :  0.74095E+00 0.11582E+05
   Dimensionless distance   yplus :  0.45828E+01 0.10474E+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         39 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10795E+10    2568   0.99190E+00   0.40280E+09 
c  VelocityY    0.10795E+10    2568   0.99190E+00   0.00000E+00 
c  VelocityZ    0.10795E+10    2568   0.99190E+00   0.00000E+00 
c  Pressure     0.66322E+03     589   0.15338E-01   0.11642E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.1491e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.1813e+05      1.1065e+05         -102.09         -66.928
v  Velocity[Y]             -1.3367e+05      2.4207e+05         -136.09         -43.698
v  Velocity[Z]              -1.466e+05      2.4227e+05         -60.309          163.02
v  ǁVelocityǁ                   1.4622      2.9953e+05          1838.8          1309.7
v  Pressure                -1.0548e+08      1.4666e+08      1.0793e+07       7.821e+06
v  turbulent_viscosity          1.1863      6.5175e+05          169.01          111.63
v  CourantNb                    42.402      3.0788e+07           51609           28837
v  FourierNb                    100.16        3.86e+08           35549           11722
v  total_pressure          -1.0498e+08      1.4716e+08      1.1293e+07       8.321e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          347.44      3.9857e+08           87158           40559


 TIME FOR THE TIME STEP              146:        0.44394E+01

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


 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        -0.652163734E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275659666E+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 :  0.18866E+01 0.37711E+06
   Friction velocity        uet   :  0.36144E+00 0.12830E+05
   Friction velocity        uk    :  0.36144E+00 0.12830E+05
   Dimensionless distance   yplus :  0.37459E+01 0.11602E+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         31 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.13300E+10    3285   0.98511E+00   0.56823E+09 
c  VelocityY    0.13300E+10    3285   0.98511E+00   0.00000E+00 
c  VelocityZ    0.13300E+10    3285   0.98511E+00   0.00000E+00 
c  Pressure     0.76638E+03     589   0.16499E-01   0.12043E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.2114e-08                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.2872e+05      1.2127e+05         -183.66         -65.501
v  Velocity[Y]             -1.3738e+05      2.7116e+05         -88.661         -50.048
v  Velocity[Z]             -1.6246e+05      2.7008e+05         -6.2284          150.11
v  ǁVelocityǁ                   7.6944      3.3536e+05          2818.1          2108.7
v  Pressure                -1.2335e+08      1.6727e+08      1.1996e+07      8.5824e+06
v  turbulent_viscosity         0.57885      7.2265e+05          180.97          115.53
v  CourantNb                    3.4692       3.403e+07           43057           22296
v  FourierNb                     69.11      4.2878e+08           38717           12410
v  total_pressure          -1.2285e+08      1.6777e+08      1.2496e+07      9.0824e+06
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          106.92      4.4292e+08           81774           34706


 TIME FOR THE TIME STEP              147:        0.49959E+01

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


 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        -0.214348464E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275892449E+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 :  0.83569E+00 0.42117E+06
   Friction velocity        uet   :  0.20984E+00 0.14211E+05
   Friction velocity        uk    :  0.20984E+00 0.14211E+05
   Dimensionless distance   yplus :  0.25238E+01 0.12851E+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         39 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.16793E+10    2945   0.99292E+00   0.73974E+09 
c  VelocityY    0.16793E+10    2945   0.99292E+00   0.00000E+00 
c  VelocityZ    0.16793E+10    2945   0.99292E+00   0.00000E+00 
c  Pressure     0.81032E+03     602   0.13637E-01   0.11456E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      9.4668e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7813e+05      1.3945e+05          -192.5         -73.795
v  Velocity[Y]             -1.6671e+05      2.9745e+05         -237.23         -56.428
v  Velocity[Z]             -1.7575e+05       3.041e+05          242.88          173.32
v  ǁVelocityǁ                   1.7539      3.6398e+05          2466.6          1656.7
v  Pressure                 -1.317e+08      1.8609e+08      1.3748e+07      9.6583e+06
v  turbulent_viscosity         0.71987      8.1074e+05          203.46          131.29
v  CourantNb                    32.798      3.7946e+07           64506           36098
v  FourierNb                    59.207      4.2696e+08           42382           14005
v  total_pressure           -1.312e+08      1.8659e+08      1.4248e+07      1.0158e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          162.54      4.4242e+08      1.0689e+05           50103


 TIME FOR THE TIME STEP              148:        0.47017E+01

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


 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        -0.111665628E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275423657E+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 :  0.35620E+00 0.46061E+06
   Friction velocity        uet   :  0.13171E+00 0.15439E+05
   Friction velocity        uk    :  0.13171E+00 0.15439E+05
   Dimensionless distance   yplus :  0.15712E+01 0.13962E+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         30 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.20075E+10    3345   0.98810E+00   0.10008E+10 
c  VelocityY    0.20075E+10    3345   0.98810E+00   0.00000E+00 
c  VelocityZ    0.20075E+10    3345   0.98810E+00   0.00000E+00 
c  Pressure     0.91851E+03     567   0.14381E-01   0.11680E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      7.6934e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.0601e+05      1.5247e+05         -267.37         -75.726
v  Velocity[Y]             -1.7055e+05      3.3371e+05         -29.019         -61.571
v  Velocity[Z]             -1.9841e+05       3.349e+05         -46.643          175.07
v  ǁVelocityǁ                    9.618      4.1179e+05          3129.1          2315.1
v  Pressure                -1.5803e+08      2.0509e+08      1.4974e+07      1.0384e+07
v  turbulent_viscosity         0.32875      8.8678e+05          221.31          135.28
v  CourantNb                    1.7965      4.2284e+07           58544           29139
v  FourierNb                    49.888      5.2673e+08           47792           15022
v  total_pressure          -1.5753e+08      2.0559e+08      1.5474e+07      1.0884e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           123.1        5.44e+08      1.0634e+05           44161


 TIME FOR THE TIME STEP              149:        0.54673E+01

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


 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        -0.382634022E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.276647193E+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 :  0.34185E+01 0.51908E+06
   Friction velocity        uet   :  0.56543E+00 0.17246E+05
   Friction velocity        uk    :  0.56543E+00 0.17246E+05
   Dimensionless distance   yplus :  0.49467E+01 0.15597E+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         38 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:    0.93872E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.25380E+10    2608   0.99152E+00   0.10811E+10 
c  VelocityY    0.25380E+10    2608   0.99152E+00   0.00000E+00 
c  VelocityZ    0.25380E+10    2608   0.99152E+00   0.00000E+00 
c  Pressure     0.10127E+04     583   0.13915E-01   0.11568E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      6.8346e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.3255e+05      1.7283e+05         -50.764         -86.288
v  Velocity[Y]             -2.0558e+05      3.6975e+05         -321.18         -67.023
v  Velocity[Z]              -2.233e+05      3.7093e+05         -18.834          231.13
v  ǁVelocityǁ                   2.7898      4.5607e+05          2989.3          2191.2
v  Pressure                -1.7125e+08      2.2526e+08      1.5993e+07      1.1039e+07
v  turbulent_viscosity         0.66107      9.9826e+05          242.13          154.43
v  CourantNb                    10.182      4.7207e+07           72198           39912
v  FourierNb                    51.542      5.2602e+08           50997           16614
v  total_pressure          -1.7075e+08      2.2576e+08      1.6493e+07      1.1539e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          424.91      5.4532e+08      1.2319e+05           56526


 TIME FOR THE TIME STEP              150:        0.40661E+01

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


 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         0.254615686E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275852910E+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 :  0.16389E+01 0.57677E+06
   Friction velocity        uet   :  0.32643E+00 0.19016E+05
   Friction velocity        uk    :  0.32643E+00 0.19016E+05
   Dimensionless distance   yplus :  0.28907E+01 0.17197E+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         42 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.31097E+10    3238   0.98511E+00   0.14456E+10 
c  VelocityY    0.31097E+10    3238   0.98511E+00   0.00000E+00 
c  VelocityZ    0.31097E+10    3238   0.98511E+00   0.00000E+00 
c  Pressure     0.11482E+04     534   0.15261E-01   0.11768E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step       6.568e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -3.503e+05      1.8649e+05         -272.29         -97.303
v  Velocity[Y]              -2.105e+05      4.1441e+05           14.86         -73.872
v  Velocity[Z]             -2.4755e+05      4.1423e+05         -141.26          226.69
v  ǁVelocityǁ                   1.2074      5.1177e+05          4090.7          2975.6
v  Pressure                -2.0103e+08      2.5061e+08      1.6565e+07      1.1151e+07
v  turbulent_viscosity          0.6837      1.1035e+06          267.91          167.89
v  CourantNb                    32.964      5.2084e+07           69735           37349
v  FourierNb                    63.704      5.8277e+08           57017           18249
v  total_pressure          -2.0053e+08      2.5111e+08      1.7065e+07      1.1651e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           164.1      6.0436e+08      1.2675e+05           55598


 TIME FOR THE TIME STEP              151:        0.56772E+01

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


 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         0.341187446E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.277078224E+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 :  0.96927E+00 0.64538E+06
   Friction velocity        uet   :  0.18304E+00 0.21105E+05
   Friction velocity        uk    :  0.18304E+00 0.21105E+05
   Dimensionless distance   yplus :  0.20236E+01 0.19086E+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         44 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.39300E+10    2887   0.99279E+00   0.19174E+10 
c  VelocityY    0.39300E+10    2887   0.99279E+00   0.00000E+00 
c  VelocityZ    0.39300E+10    2887   0.99279E+00   0.00000E+00 
c  Pressure     0.12460E+04     592   0.14156E-01   0.11482E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      6.1912e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2952e+05      2.0877e+05         -213.97         -118.48
v  Velocity[Y]               -2.54e+05      4.5433e+05          -365.6         -87.232
v  Velocity[Z]             -2.7009e+05      4.6439e+05           216.5          269.81
v  ǁVelocityǁ                    1.465      5.5767e+05          4171.5          2833.1
v  Pressure                  -2.17e+08       2.794e+08      1.8661e+07       1.246e+07
v  turbulent_viscosity         0.69068       1.239e+06          304.37          192.15
v  CourantNb                    18.201      5.8094e+07           94567           51635
v  FourierNb                    36.351       6.526e+08           64150           20841
v  total_pressure           -2.165e+08       2.799e+08      1.9161e+07       1.296e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          110.87      6.7625e+08      1.5872e+05           72476


 TIME FOR THE TIME STEP              152:        0.44033E+01

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


 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         0.395469410E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.278188284E+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 0.70713E+06
   Friction velocity        uet   :  0.13161E+00 0.22973E+05
   Friction velocity        uk    :  0.13161E+00 0.22973E+05
   Dimensionless distance   yplus :  0.15516E+01 0.20776E+06
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          1
   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    0.46942E+10    3430   0.98717E+00   0.23574E+10 
c  VelocityY    0.46942E+10    3430   0.98717E+00   0.00000E+00 
c  VelocityZ    0.46942E+10    3430   0.98717E+00   0.00000E+00 
c  Pressure     0.13924E+04     568   0.14278E-01   0.11531E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      5.0453e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.6704e+05       2.362e+05         -288.59         -122.32
v  Velocity[Y]             -2.6083e+05      5.0991e+05         -84.838         -96.088
v  Velocity[Z]             -3.0456e+05      5.1102e+05         -200.09          275.99
v  ǁVelocityǁ                   8.7384      6.2916e+05          4666.3          3486.7
v  Pressure                -2.5375e+08      3.0977e+08       2.042e+07      1.3492e+07
v  turbulent_viscosity         0.87368      1.3543e+06          344.97          209.65
v  CourantNb                    19.651       6.477e+07           98164           49740
v  FourierNb                    56.719      8.0452e+08           74537           23396
v  total_pressure          -2.5325e+08      3.1027e+08       2.092e+07      1.3992e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          113.85      8.3102e+08       1.727e+05           73136


 TIME FOR THE TIME STEP              153:        0.51695E+01

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


 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         0.587236883E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.276721381E+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 :  0.25848E+01 0.79523E+06
   Friction velocity        uet   :  0.43237E+00 0.25619E+05
   Friction velocity        uk    :  0.43237E+00 0.25619E+05
   Dimensionless distance   yplus :  0.49404E+01 0.23168E+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         35 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.59426E+10    2693   0.99109E+00   0.24191E+10 
c  VelocityY    0.59426E+10    2693   0.99109E+00   0.00000E+00 
c  VelocityZ    0.59426E+10    2693   0.99109E+00   0.00000E+00 
c  Pressure     0.15438E+04     574   0.14239E-01   0.11480E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      5.3122e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.1127e+05       2.606e+05          -205.4         -139.67
v  Velocity[Y]             -3.1379e+05      5.6627e+05         -544.23          -104.8
v  Velocity[Z]             -3.4272e+05      5.6966e+05          174.56          347.89
v  ǁVelocityǁ                   3.9296      6.9911e+05          4865.3          3354.8
v  Pressure                -2.7567e+08      3.4302e+08      2.1967e+07      1.4463e+07
v  turbulent_viscosity          0.7873      1.5253e+06          367.29          232.14
v  CourantNb                    57.309       7.224e+07      1.0766e+05           59943
v  FourierNb                    59.964      8.0385e+08           77866           25135
v  total_pressure          -2.7517e+08      3.4352e+08      2.2467e+07      1.4963e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          320.22      8.3333e+08      1.8553e+05           85078


 TIME FOR THE TIME STEP              154:        0.46319E+01

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


 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         0.561965137E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.279202580E+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 :  0.23242E+01 0.88649E+06
   Friction velocity        uet   :  0.36489E+00 0.28339E+05
   Friction velocity        uk    :  0.36489E+00 0.28339E+05
   Dimensionless distance   yplus :  0.50528E+01 0.25629E+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         43 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.73109E+10    3301   0.98423E+00   0.32704E+10 
c  VelocityY    0.73109E+10    3301   0.98423E+00   0.00000E+00 
c  VelocityZ    0.73109E+10    3301   0.98423E+00   0.00000E+00 
c  Pressure     0.17519E+04     589   0.15134E-01   0.11685E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.5453e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.367e+05      2.8746e+05         -486.78         -121.05
v  Velocity[Y]             -3.2269e+05      6.3454e+05          -13.32         -120.52
v  Velocity[Z]             -3.8092e+05      6.3241e+05         -319.84          385.66
v  ǁVelocityǁ                   7.5459      7.8352e+05          6078.6          4575.4
v  Pressure                -3.1644e+08      3.8521e+08      2.5263e+07      1.6905e+07
v  turbulent_viscosity         0.59294      1.6897e+06          417.61          256.99
v  CourantNb                    41.102      7.9808e+07       1.145e+05           58352
v  FourierNb                    57.141      8.9249e+08           88668           28314
v  total_pressure          -3.1594e+08      3.8571e+08      2.5763e+07      1.7405e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          126.09      9.2557e+08      2.0317e+05           86665


 TIME FOR THE TIME STEP              155:        0.48746E+01

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


 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         0.509356080E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.278259662E+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 :  0.13963E+02 0.99090E+06
   Friction velocity        uet   :  0.16915E+01 0.31430E+05
   Friction velocity        uk    :  0.16915E+01 0.31430E+05
   Dimensionless distance   yplus :  0.57910E+01 0.28423E+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         35 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.92380E+10    2742   0.99226E+00   0.40964E+10 
c  VelocityY    0.92380E+10    2742   0.99226E+00   0.00000E+00 
c  VelocityZ    0.92380E+10    2742   0.99226E+00   0.00000E+00 
c  Pressure     0.19050E+04     600   0.13824E-01   0.11425E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.8347e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5899e+05      3.1913e+05         -239.48         -153.44
v  Velocity[Y]             -3.8865e+05       6.969e+05         -501.58         -138.12
v  Velocity[Z]             -4.1453e+05      7.1403e+05           104.5          434.59
v  ǁVelocityǁ                   4.5924      8.5479e+05          6107.4          4226.7
v  Pressure                -3.4159e+08      4.2616e+08      2.8049e+07      1.8621e+07
v  turbulent_viscosity          1.5976      1.8966e+06          472.02          304.52
v  CourantNb                    79.645      8.8941e+07      1.3985e+05           77932
v  FourierNb                    117.71      1.1228e+09      1.0093e+05           32507
v  total_pressure          -3.4109e+08      4.2666e+08      2.8549e+07      1.9121e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          478.34       1.159e+09      2.4079e+05      1.1044e+05


 TIME FOR THE TIME STEP              156:        0.42752E+01

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


 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        -0.309027326E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.278069828E+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 :  0.11371E+01 0.10876E+07
   Friction velocity        uet   :  0.24629E+00 0.34272E+05
   Friction velocity        uk    :  0.24629E+00 0.34272E+05
   Dimensionless distance   yplus :  0.35083E+01 0.30994E+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         38 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.11070E+11    3404   0.98623E+00   0.56482E+10 
c  VelocityY    0.11070E+11    3404   0.98623E+00   0.00000E+00 
c  VelocityZ    0.11070E+11    3404   0.98623E+00   0.00000E+00 
c  Pressure     0.21582E+04     542   0.15086E-01   0.11622E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.3175e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1677e+05      3.6433e+05         -416.27         -202.37
v  Velocity[Y]             -4.0169e+05      7.8078e+05         -222.68         -153.87
v  Velocity[Z]             -4.6761e+05      7.8129e+05         -203.45          415.55
v  ǁVelocityǁ                   3.7026      9.6261e+05          7679.1          5717.5
v  Pressure                -4.0157e+08      4.7648e+08      2.9773e+07      1.9229e+07
v  turbulent_viscosity          1.3442      2.0769e+06          528.59          323.79
v  CourantNb                    50.722      9.9254e+07      1.4343e+05           73316
v  FourierNb                    106.66      1.2338e+09      1.1418e+05           35903
v  total_pressure          -4.0107e+08      4.7698e+08      3.0273e+07      1.9729e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          249.02      1.2744e+09       2.576e+05      1.0922e+05


 TIME FOR THE TIME STEP              157:        0.52184E+01

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


 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         0.189306402E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.281281399E+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 :  0.34814E+00 0.12206E+07
   Friction velocity        uet   :  0.10203E+00 0.38157E+05
   Friction velocity        uk    :  0.10203E+00 0.38157E+05
   Dimensionless distance   yplus :  0.14059E+01 0.34508E+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         46 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.13964E+11    2756   0.99069E+00   0.54845E+10 
c  VelocityY    0.13964E+11    2756   0.99069E+00   0.00000E+00 
c  VelocityZ    0.13964E+11    2756   0.99069E+00   0.00000E+00 
c  Pressure     0.23446E+04     608   0.13209E-01   0.11356E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.4429e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8549e+05      3.9613e+05         -254.25         -223.08
v  Velocity[Y]             -4.7908e+05      8.6662e+05         -930.19         -174.16
v  Velocity[Z]             -5.2597e+05      8.7249e+05          185.22          544.15
v  ǁVelocityǁ                   25.552      1.0703e+06          6604.3          4675.1
v  Pressure                -4.2824e+08      5.2624e+08      3.6113e+07      2.4162e+07
v  turbulent_viscosity         0.86317      2.3347e+06          570.51          361.13
v  CourantNb                    31.884      1.1063e+08      1.7652e+05           98510
v  FourierNb                    51.379      1.2306e+09      1.2047e+05           39061
v  total_pressure          -4.2774e+08      5.2674e+08      3.6613e+07      2.4662e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           187.8      1.2757e+09      2.9699e+05      1.3757e+05


 TIME FOR THE TIME STEP              158:        0.41938E+01

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


 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        -0.108029192E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.280353970E+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 :  0.59082E+01 0.13608E+07
   Friction velocity        uet   :  0.82215E+00 0.42220E+05
   Friction velocity        uk    :  0.82215E+00 0.42220E+05
   Dimensionless distance   yplus :  0.66833E+01 0.38182E+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         34 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.17161E+11    3020   0.98345E+00   0.77304E+10 
c  VelocityY    0.17161E+11    3020   0.98345E+00   0.00000E+00 
c  VelocityZ    0.17161E+11    3020   0.98345E+00   0.00000E+00 
c  Pressure     0.27539E+04     591   0.17155E-01   0.11943E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.8322e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.253e+05      4.3802e+05         -424.68         -206.65
v  Velocity[Y]             -4.9584e+05       9.716e+05         -45.915          -188.4
v  Velocity[Z]             -5.8629e+05       9.677e+05         -1209.3          687.57
v  ǁVelocityǁ                   35.251       1.201e+06          9694.9          7578.9
v  Pressure                -4.9181e+08      5.9483e+08      4.0734e+07      2.7615e+07
v  turbulent_viscosity          2.7316      2.5854e+06          626.79           391.7
v  CourantNb                    28.255      1.2232e+08      1.5573e+05           80586
v  FourierNb                     163.6      1.5346e+09       1.361e+05           42755
v  total_pressure          -4.9131e+08      5.9533e+08      4.1234e+07      2.8115e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          943.97      1.5852e+09      2.9182e+05      1.2334e+05


 TIME FOR THE TIME STEP              159:        0.45470E+01

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


 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         0.966666580E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.282608063E+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 :  0.11353E+02 0.15224E+07
   Friction velocity        uet   :  0.14317E+01 0.46874E+05
   Friction velocity        uk    :  0.14317E+01 0.46874E+05
   Dimensionless distance   yplus :  0.13486E+02 0.42390E+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         41 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.21712E+11    2651   0.99161E+00   0.91894E+10 
c  VelocityY    0.21712E+11    2651   0.99161E+00   0.00000E+00 
c  VelocityZ    0.21712E+11    2651   0.99161E+00   0.00000E+00 
c  Pressure     0.29356E+04     620   0.14140E-01   0.11446E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.8608e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0062e+06      4.9577e+05         -826.17          -259.5
v  Velocity[Y]             -5.9789e+05       1.069e+06         -646.27         -224.07
v  Velocity[Z]             -6.3479e+05       1.098e+06          869.27          701.13
v  ǁVelocityǁ                   5.2198      1.3079e+06          8570.3          5729.5
v  Pressure                -5.2315e+08      6.6824e+08      4.8792e+07      3.3499e+07
v  turbulent_viscosity           2.708      2.9034e+06          760.27           508.4
v  CourantNb                    199.23      1.3624e+08       2.208e+05      1.2598e+05
v  FourierNb                    286.51      1.5295e+09      1.5592e+05           52807
v  total_pressure          -5.2265e+08      6.6874e+08      4.9292e+07      3.3999e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          802.13       1.585e+09      3.7672e+05      1.7878e+05


 TIME FOR THE TIME STEP              160:        0.44970E+01

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


 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        -0.808667830E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.281165501E+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 :  0.17526E+01 0.16708E+07
   Friction velocity        uet   :  0.30397E+00 0.51116E+05
   Friction velocity        uk    :  0.30397E+00 0.51116E+05
   Dimensionless distance   yplus :  0.56835E+01 0.46227E+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         33 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.26112E+11    3113   0.98574E+00   0.12277E+11 
c  VelocityY    0.26112E+11    3113   0.98574E+00   0.00000E+00 
c  VelocityZ    0.26112E+11    3113   0.98574E+00   0.00000E+00 
c  Pressure     0.33126E+04     622   0.14843E-01   0.11596E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.4853e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0963e+06      5.5847e+05         -1154.1         -266.02
v  Velocity[Y]             -6.1771e+05      1.1952e+06         -197.26         -265.33
v  Velocity[Z]             -7.1647e+05       1.199e+06         -781.27          720.76
v  ǁVelocityǁ                   41.258      1.4708e+06           11731          8745.6
v  Pressure                -6.0014e+08      7.5347e+08      6.1267e+07      4.2606e+07
v  turbulent_viscosity          2.5431      3.1854e+06          826.35           509.8
v  CourantNb                    3.2028      1.5205e+08      2.0333e+05      1.0006e+05
v  FourierNb                    173.92      1.6845e+09      1.7357e+05           56148
v  total_pressure          -5.9964e+08      7.5397e+08      6.1767e+07      4.3106e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          347.11      1.7465e+09       3.769e+05      1.5621e+05


 TIME FOR THE TIME STEP              161:        0.54118E+01

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


 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         0.398722613E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.282101364E+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 :  0.44425E+02 0.18718E+07
   Friction velocity        uet   :  0.38505E+01 0.56827E+05
   Friction velocity        uk    :  0.38505E+01 0.56827E+05
   Dimensionless distance   yplus :  0.39584E+02 0.51392E+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         34 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.32806E+11    2535   0.99005E+00   0.11486E+11 
c  VelocityY    0.32806E+11    2535   0.99005E+00   0.00000E+00 
c  VelocityZ    0.32806E+11    2535   0.99005E+00   0.00000E+00 
c  Pressure     0.36866E+04     606   0.14652E-01   0.11593E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.8367e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.2047e+06      6.1106e+05         -222.18         -324.26
v  Velocity[Y]             -7.3774e+05      1.3267e+06         -1013.6         -269.39
v  Velocity[Z]             -8.0716e+05       1.336e+06         -278.61          905.46
v  ǁVelocityǁ                   17.351      1.6376e+06          9538.1          7073.7
v  Pressure                -6.4191e+08      8.2563e+08      6.8132e+07      4.7394e+07
v  turbulent_viscosity          3.2432      3.5729e+06           915.5          598.41
v  CourantNb                    466.85      1.6959e+08      2.7064e+05       1.489e+05
v  FourierNb                    416.88      1.8834e+09       1.895e+05           63230
v  total_pressure          -6.4141e+08      8.2613e+08      6.8632e+07      4.7894e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4025.7      1.9525e+09      4.6014e+05      2.1213e+05


 TIME FOR THE TIME STEP              162:        0.41256E+01

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


 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        -0.468140419E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.283310290E+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 :  0.65463E+01 0.20886E+07
   Friction velocity        uet   :  0.86992E+00 0.62945E+05
   Friction velocity        uk    :  0.86992E+00 0.62945E+05
   Dimensionless distance   yplus :  0.11900E+02 0.56925E+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         43 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.40308E+11    3127   0.98312E+00   0.19812E+11 
c  VelocityY    0.40308E+11    3127   0.98312E+00   0.00000E+00 
c  VelocityZ    0.40308E+11    3127   0.98312E+00   0.00000E+00 
c  Pressure     0.42576E+04     556   0.16820E-01   0.11993E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.2077e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.2725e+06      6.6706e+05         -936.93         -368.44
v  Velocity[Y]             -7.5723e+05      1.4848e+06          -177.4         -282.51
v  Velocity[Z]              -8.994e+05       1.476e+06         -361.52          856.04
v  ǁVelocityǁ                   8.7397      1.8376e+06           16208           12204
v  Pressure                -7.5187e+08      9.3122e+08       7.093e+07      4.8594e+07
v  turbulent_viscosity          2.4948      3.9567e+06          979.95          627.62
v  CourantNb                    124.46      1.8729e+08      2.2292e+05      1.1942e+05
v  FourierNb                     207.4      2.3488e+09      2.0994e+05           67315
v  total_pressure          -7.5137e+08      9.3172e+08       7.143e+07      4.9094e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          809.39      2.4265e+09      4.3286e+05      1.8673e+05


 TIME FOR THE TIME STEP              163:        0.54497E+01

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


 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        -0.445135628E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.285148250E+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 :  0.35154E+01 0.23343E+07
   Friction velocity        uet   :  0.60945E+00 0.69831E+05
   Friction velocity        uk    :  0.60945E+00 0.69831E+05
   Dimensionless distance   yplus :  0.56894E+01 0.63152E+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         44 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.50796E+11    2989   0.99091E+00   0.25161E+11 
c  VelocityY    0.50796E+11    2989   0.99091E+00   0.00000E+00 
c  VelocityZ    0.50796E+11    2989   0.99091E+00   0.00000E+00 
c  Pressure     0.45089E+04     607   0.14004E-01   0.11438E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step       1.948e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.5308e+06       7.651e+05         -1021.8         -522.47
v  Velocity[Y]             -9.0963e+05      1.6311e+06           -1483         -326.76
v  Velocity[Z]             -9.6958e+05      1.6754e+06            2057          999.05
v  ǁVelocityǁ                   40.552      1.9934e+06           13167            9051
v  Pressure                  -8.04e+08      1.0364e+09      8.1021e+07      5.5239e+07
v  turbulent_viscosity          1.8447      4.4362e+06          1139.1          731.91
v  CourantNb                   0.20198      2.0859e+08      3.6926e+05      2.0885e+05
v  FourierNb                    174.37       2.627e+09      2.4125e+05           78553
v  total_pressure           -8.035e+08      1.0369e+09      8.1521e+07      5.5739e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          658.63      2.7119e+09      6.1052e+05       2.874e+05


 TIME FOR THE TIME STEP              164:        0.45660E+01

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


 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         0.204309009E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.286173271E+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 :  0.13570E+02 0.25532E+07
   Friction velocity        uet   :  0.15781E+01 0.75925E+05
   Friction velocity        uk    :  0.15781E+01 0.75925E+05
   Dimensionless distance   yplus :  0.18679E+02 0.68663E+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         38 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.60926E+11    3000   0.98542E+00   0.33031E+11 
c  VelocityY    0.60926E+11    3000   0.98542E+00   0.00000E+00 
c  VelocityZ    0.60926E+11    3000   0.98542E+00   0.00000E+00 
c  Pressure     0.51812E+04     590   0.16023E-01   0.11783E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.3393e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6937e+06      8.3726e+05         -1106.7         -523.77
v  Velocity[Y]             -9.4184e+05      1.8291e+06         -503.06         -379.09
v  Velocity[Z]             -1.1024e+06      1.8353e+06         -2034.3          1086.7
v  ǁVelocityǁ                    56.43      2.2582e+06           19053           13606
v  Pressure                -9.5355e+08      1.1629e+09      9.0931e+07      6.0912e+07
v  turbulent_viscosity          5.9145      4.8601e+06          1266.6           784.3
v  CourantNb                    124.33      2.3276e+08      3.1274e+05      1.5722e+05
v  FourierNb                    379.52      2.5704e+09      2.6621e+05           86082
v  total_pressure          -9.5305e+08      1.1634e+09      9.1431e+07      6.1412e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1627.7      2.6652e+09      5.7895e+05       2.433e+05


 TIME FOR THE TIME STEP              165:        0.52261E+01

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


 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         0.283828570E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.291705737E+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 :  0.94878E+01 0.28778E+07
   Friction velocity        uet   :  0.11764E+01 0.84908E+05
   Friction velocity        uk    :  0.11764E+01 0.84908E+05
   Dimensionless distance   yplus :  0.11011E+02 0.76787E+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         39 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.76962E+11    2590   0.98939E+00   0.30643E+11 
c  VelocityY    0.76962E+11    2590   0.98939E+00   0.00000E+00 
c  VelocityZ    0.76962E+11    2590   0.98939E+00   0.00000E+00 
c  Pressure     0.56901E+04     642   0.15325E-01   0.11633E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step       1.322e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8425e+06      9.4746e+05         -662.42         -646.54
v  Velocity[Y]              -1.125e+06      2.0305e+06         -1186.7          -425.4
v  Velocity[Z]             -1.2384e+06      2.0369e+06          162.31          1662.2
v  ǁVelocityǁ                   87.544      2.5049e+06           15712           11717
v  Pressure                -9.9875e+08      1.2993e+09      1.1889e+08      8.4848e+07
v  turbulent_viscosity           3.284      5.4669e+06          1420.4           911.6
v  CourantNb                    6.8984      2.5962e+08       4.404e+05      2.3633e+05
v  FourierNb                    281.01      2.8821e+09      2.9602e+05           97660
v  total_pressure          -9.9825e+08      1.2998e+09      1.1939e+08      8.5348e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1113.2       2.988e+09      7.3642e+05      3.3399e+05


 TIME FOR THE TIME STEP              166:        0.46345E+01

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


 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         0.145811802E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.294279802E+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 :  0.44099E+02 0.32030E+07
   Friction velocity        uet   :  0.42440E+01 0.93842E+05
   Friction velocity        uk    :  0.42440E+01 0.93842E+05
   Dimensionless distance   yplus :  0.75403E+01 0.84866E+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         26 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.94595E+11    3442   0.98268E+00   0.42679E+11 
c  VelocityY    0.94595E+11    3442   0.98268E+00   0.00000E+00 
c  VelocityZ    0.94595E+11    3442   0.98268E+00   0.00000E+00 
c  Pressure     0.65201E+04     573   0.16017E-01   0.11939E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.4154e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9473e+06      1.0374e+06         -1901.5          -602.1
v  Velocity[Y]             -1.1719e+06      2.2822e+06         -336.72         -427.89
v  Velocity[Z]             -1.3731e+06      2.2911e+06          -171.8          1359.9
v  ǁVelocityǁ                   45.279      2.8145e+06           24143           17900
v  Pressure                -1.1629e+09      1.4596e+09      1.2586e+08      8.9016e+07
v  turbulent_viscosity          8.2867      6.0551e+06          1543.9          1026.5
v  CourantNb                     105.8      2.8647e+08       3.653e+05      1.9396e+05
v  FourierNb                    583.75       3.199e+09      3.2095e+05      1.0662e+05
v  total_pressure          -1.1624e+09      1.4601e+09      1.2636e+08      8.9516e+07
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3470.8      3.3177e+09      6.8625e+05      3.0058e+05


 TIME FOR THE TIME STEP              167:        0.53497E+01

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


 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         0.129152678E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.293903577E+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 :  0.64941E+01 0.35922E+07
   Friction velocity        uet   :  0.10163E+01 0.10446E+06
   Friction velocity        uk    :  0.10163E+01 0.10446E+06
   Dimensionless distance   yplus :  0.73869E+01 0.94471E+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         33 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.12022E+12    3022   0.99021E+00   0.51666E+11 
c  VelocityY    0.12022E+12    3022   0.99021E+00   0.00000E+00 
c  VelocityZ    0.12022E+12    3022   0.99021E+00   0.00000E+00 
c  Pressure     0.68545E+04     619   0.13574E-01   0.11306E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      9.5866e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.3531e+06      1.1899e+06         -1518.4         -672.84
v  Velocity[Y]             -1.4135e+06      2.5002e+06           -1806         -501.15
v  Velocity[Z]             -1.4903e+06      2.5598e+06          2355.9          1559.6
v  ǁVelocityǁ                   23.873       3.052e+06           20366           13839
v  Pressure                -1.2317e+09      1.6264e+09      1.4453e+08      1.0123e+08
v  turbulent_viscosity          9.5693      6.8164e+06          1740.7            1122
v  CourantNb                    204.55      3.1947e+08        5.54e+05      3.0786e+05
v  FourierNb                    502.12      3.5918e+09      3.6241e+05      1.1981e+05
v  total_pressure          -1.2312e+09      1.6269e+09      1.4503e+08      1.0173e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1781.4      3.7218e+09      9.1641e+05      4.2767e+05


 TIME FOR THE TIME STEP              168:        0.45835E+01

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


 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        -0.443117439E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.293864835E+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 :  0.58484E+01 0.39210E+07
   Friction velocity        uet   :  0.87635E+00 0.11338E+06
   Friction velocity        uk    :  0.87635E+00 0.11338E+06
   Dimensionless distance   yplus :  0.67433E+01 0.10254E+07
   ------------------------------------------------------
   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         46 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.14335E+12    3427   0.98545E+00   0.69030E+11 
c  VelocityY    0.14335E+12    3427   0.98545E+00   0.00000E+00 
c  VelocityZ    0.14335E+12    3427   0.98545E+00   0.00000E+00 
c  Pressure     0.77466E+04     587   0.13982E-01   0.11500E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.0262e-09                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6008e+06      1.2831e+06         -2702.3         -617.97
v  Velocity[Y]             -1.4438e+06      2.8077e+06          -283.3         -554.14
v  Velocity[Z]             -1.6831e+06      2.8346e+06          307.47            1537
v  ǁVelocityǁ                   81.197      3.4601e+06           25985           19143
v  Pressure                -1.4528e+09      1.7866e+09      1.5869e+08      1.1049e+08
v  turbulent_viscosity          4.9191      7.4457e+06          1886.9          1163.3
v  CourantNb                    39.607      3.5582e+08      4.8327e+05      2.4258e+05
v  FourierNb                    444.36       3.938e+09      3.9852e+05      1.2821e+05
v  total_pressure          -1.4523e+09      1.7871e+09      1.5919e+08      1.1099e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1450.9      4.0828e+09      8.8179e+05      3.7079e+05


 TIME FOR THE TIME STEP              169:        0.59365E+01

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


 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         0.126260699E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.294593316E+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 :  0.82933E+01 0.44252E+07
   Friction velocity        uet   :  0.10662E+01 0.12697E+06
   Friction velocity        uk    :  0.10662E+01 0.12697E+06
   Dimensionless distance   yplus :  0.13234E+02 0.11483E+07
   ------------------------------------------------------
   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         35 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.18156E+12    2673   0.98874E+00   0.72334E+11 
c  VelocityY    0.18156E+12    2673   0.98874E+00   0.00000E+00 
c  VelocityZ    0.18156E+12    2673   0.98874E+00   0.00000E+00 
c  Pressure     0.86511E+04     603   0.14303E-01   0.11543E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      8.1471e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.8182e+06      1.4643e+06         -364.03         -735.55
v  Velocity[Y]             -1.7409e+06      3.1065e+06         -2851.9         -601.27
v  Velocity[Z]             -1.9015e+06      3.1149e+06          107.23          2089.3
v  ǁVelocityǁ                    29.88      3.8295e+06           23743           17744
v  Pressure                -1.5613e+09      1.9622e+09      1.7048e+08      1.1835e+08
v  turbulent_viscosity          7.1153      8.3897e+06          2058.2          1317.1
v  CourantNb                    111.19      3.9758e+08      6.0006e+05      3.3079e+05
v  FourierNb                    653.67      4.4233e+09      4.3316e+05       1.414e+05
v  total_pressure          -1.5608e+09      1.9627e+09      1.7098e+08      1.1885e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            3167      4.5853e+09      1.0332e+06      4.7219e+05


 TIME FOR THE TIME STEP              170:        0.41120E+01

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


 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         0.329353439E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.297149382E+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 :  0.75477E+01 0.49089E+07
   Friction velocity        uet   :  0.98177E+00 0.13992E+06
   Friction velocity        uk    :  0.98177E+00 0.13992E+06
   Dimensionless distance   yplus :  0.12154E+02 0.12654E+07
   ------------------------------------------------------
   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         44 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.22188E+12    3197   0.98174E+00   0.11037E+12 
c  VelocityY    0.22188E+12    3197   0.98174E+00   0.00000E+00 
c  VelocityZ    0.22188E+12    3197   0.98174E+00   0.00000E+00 
c  Pressure     0.99927E+04     568   0.16091E-01   0.11941E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      8.4733e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.9798e+06      1.5947e+06         -2219.4          -780.6
v  Velocity[Y]             -1.7916e+06      3.4959e+06          141.14         -654.23
v  Velocity[Z]             -2.1115e+06      3.5025e+06         -1690.5          2061.6
v  ǁVelocityǁ                    38.38      4.3135e+06           37282           27281
v  Pressure                -1.8307e+09      2.1927e+09      1.7823e+08      1.2196e+08
v  turbulent_viscosity          7.2187      9.2605e+06          2275.8          1445.6
v  CourantNb                    56.115      4.3825e+08      5.5422e+05       3.005e+05
v  FourierNb                    513.65       5.498e+09      4.9047e+05      1.5585e+05
v  total_pressure          -1.8302e+09      2.1932e+09      1.7873e+08      1.2246e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1432.4      5.6792e+09      1.0447e+06      4.5635e+05


 TIME FOR THE TIME STEP              171:        0.54666E+01

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


 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         0.326617032E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.299411132E+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 :  0.81512E+01 0.55156E+07
   Friction velocity        uet   :  0.11695E+01 0.15606E+06
   Friction velocity        uk    :  0.11695E+01 0.15606E+06
   Dimensionless distance   yplus :  0.94239E+01 0.14113E+07
   ------------------------------------------------------
   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         44 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.28275E+12    2932   0.99038E+00   0.13672E+12 
c  VelocityY    0.28275E+12    2932   0.99038E+00   0.00000E+00 
c  VelocityZ    0.28275E+12    2932   0.99038E+00   0.00000E+00 
c  Pressure     0.10580E+05     610   0.13913E-01   0.11382E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      7.8459e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -3.643e+06      1.7841e+06         -2032.8         -1113.1
v  Velocity[Y]             -2.1637e+06      3.8258e+06           -3220         -775.23
v  Velocity[Z]              -2.298e+06      3.9125e+06            4040          2414.8
v  ǁVelocityǁ                   96.724      4.6854e+06           32702           22332
v  Pressure                -1.9523e+09      2.4494e+09      2.0408e+08      1.3947e+08
v  turbulent_viscosity          5.1361      1.0441e+07          2661.8          1697.6
v  CourantNb                    54.099      4.8929e+08      8.5919e+05      4.7173e+05
v  FourierNb                     474.8      5.5022e+09      5.5651e+05      1.8278e+05
v  total_pressure          -1.9518e+09      2.4499e+09      2.0458e+08      1.3997e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1407.9      5.7009e+09      1.4157e+06      6.5451e+05


 TIME FOR THE TIME STEP              172:        0.51295E+01

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


 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         0.911394332E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.304863888E+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 :  0.55645E+02 0.60255E+07
   Friction velocity        uet   :  0.49308E+01 0.16954E+06
   Friction velocity        uk    :  0.49308E+01 0.16954E+06
   Dimensionless distance   yplus :  0.16062E+02 0.15332E+07
   ------------------------------------------------------
   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         39 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.33626E+12    3349   0.98440E+00   0.16911E+12 
c  VelocityY    0.33626E+12    3349   0.98440E+00   0.00000E+00 
c  VelocityZ    0.33626E+12    3349   0.98440E+00   0.00000E+00 
c  Pressure     0.11963E+05     600   0.14907E-01   0.11555E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      6.6202e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.9719e+06      1.9877e+06         -2846.7         -874.94
v  Velocity[Y]             -2.2081e+06      4.2946e+06         -261.31         -833.76
v  Velocity[Z]             -2.5911e+06      4.3153e+06         -3622.6            2628
v  ǁVelocityǁ                   141.32      5.2942e+06           40951           30847
v  Pressure                -2.2676e+09      2.7249e+09      2.3375e+08      1.6081e+08
v  turbulent_viscosity          11.228       1.139e+07          2946.2          1815.9
v  CourantNb                    478.48      5.4504e+08      7.7437e+05      3.9017e+05
v  FourierNb                    884.77      6.0255e+09      6.2047e+05      2.0021e+05
v  total_pressure          -2.2671e+09      2.7254e+09      2.3425e+08      1.6131e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3332.6      6.2477e+09      1.3948e+06      5.9038e+05


 TIME FOR THE TIME STEP              173:        0.48996E+01

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


 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         0.403139501E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.308941970E+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 :  0.40776E+02 0.67828E+07
   Friction velocity        uet   :  0.36404E+01 0.18944E+06
   Friction velocity        uk    :  0.36404E+01 0.18944E+06
   Dimensionless distance   yplus :  0.55723E+02 0.17132E+07
   ------------------------------------------------------
   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         33 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.42592E+12    2626   0.98860E+00   0.17365E+12 
c  VelocityY    0.42592E+12    2626   0.98860E+00   0.00000E+00 
c  VelocityZ    0.42592E+12    2626   0.98860E+00   0.00000E+00 
c  Pressure     0.13258E+05     609   0.14935E-01   0.11508E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      6.3361e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.3419e+06        2.21e+06           -2156         -1232.6
v  Velocity[Y]             -2.6587e+06       4.765e+06         -3547.9         -951.26
v  Velocity[Z]             -2.9192e+06      4.7926e+06          1929.9          3446.2
v  ǁVelocityǁ                   107.98      5.8789e+06           39994           29003
v  Pressure                -2.4218e+09      3.0369e+09      2.6509e+08      1.8646e+08
v  turbulent_viscosity           10.71      1.2833e+07          3219.6          2096.4
v  CourantNb                    109.85      6.0841e+08      9.4163e+05      5.2626e+05
v  FourierNb                    1063.5      6.7663e+09       6.732e+05      2.2244e+05
v  total_pressure          -2.4213e+09      3.0374e+09      2.6559e+08      1.8696e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3394.6       7.014e+09      1.6148e+06       7.487e+05


 TIME FOR THE TIME STEP              174:        0.40842E+01

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


 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        -0.120676169E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.314499660E+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 :  0.48012E+02 0.75526E+07
   Friction velocity        uet   :  0.43318E+01 0.20953E+06
   Friction velocity        uk    :  0.43318E+01 0.20953E+06
   Dimensionless distance   yplus :  0.15416E+02 0.18949E+07
   ------------------------------------------------------
   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         35 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.52292E+12    3464   0.98193E+00   0.23538E+12 
c  VelocityY    0.52292E+12    3464   0.98193E+00   0.00000E+00 
c  VelocityZ    0.52292E+12    3464   0.98193E+00   0.00000E+00 
c  Pressure     0.14950E+05     568   0.15221E-01   0.11650E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      5.6529e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.5759e+06       2.411e+06         -4104.9         -1257.7
v  Velocity[Y]             -2.7274e+06      5.3341e+06         -594.88         -1040.9
v  Velocity[Z]             -3.2349e+06      5.3319e+06         -632.59          3138.2
v  ǁVelocityǁ                     35.8       6.585e+06           53483           39717
v  Pressure                -2.8106e+09       3.391e+09      2.8152e+08       1.944e+08
v  turbulent_viscosity          9.2871      1.4202e+07          3606.1          2305.1
v  CourantNb                    808.18      6.7147e+08      9.3225e+05      4.9113e+05
v  FourierNb                    1168.1      7.5055e+09      7.5576e+05      2.4681e+05
v  total_pressure          -2.8101e+09      3.3915e+09      2.8202e+08       1.949e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4422.1      7.7833e+09       1.688e+06      7.3795e+05


 TIME FOR THE TIME STEP              175:        0.60902E+01

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


 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         0.504471855E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.314187998E+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 :  0.15509E+02 0.84357E+07
   Friction velocity        uet   :  0.17454E+01 0.23244E+06
   Friction velocity        uk    :  0.17454E+01 0.23244E+06
   Dimensionless distance   yplus :  0.16399E+02 0.21021E+07
   ------------------------------------------------------
   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         46 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.65939E+12    2933   0.98955E+00   0.28701E+12 
c  VelocityY    0.65939E+12    2933   0.98955E+00   0.00000E+00 
c  VelocityZ    0.65939E+12    2933   0.98955E+00   0.00000E+00 
c  Pressure     0.16077E+05     619   0.13470E-01   0.11286E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.2163e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5618e+06       2.729e+06         -3393.8         -1293.7
v  Velocity[Y]             -3.2924e+06      5.8475e+06         -3808.1           -1200
v  Velocity[Z]             -3.5075e+06      6.0011e+06          3620.2          3738.8
v  ǁVelocityǁ                   87.519      7.1588e+06           50320           34496
v  Pressure                -2.9974e+09      3.7539e+09      3.2273e+08      2.2309e+08
v  turbulent_viscosity          10.246      1.5928e+07          4066.8          2587.5
v  CourantNb                    188.13      7.4924e+08      1.2287e+06      6.8388e+05
v  FourierNb                    753.55      8.3947e+09      8.5036e+05      2.7868e+05
v  total_pressure          -2.9969e+09      3.7544e+09      3.2323e+08      2.2359e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2285.8      8.6988e+09      2.0791e+06      9.6256e+05


 TIME FOR THE TIME STEP              176:        0.44597E+01

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


 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         0.174528621E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.323767286E+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 :  0.67384E+02 0.92299E+07
   Friction velocity        uet   :  0.53690E+01 0.25293E+06
   Friction velocity        uk    :  0.53690E+01 0.25293E+06
   Dimensionless distance   yplus :  0.36919E+02 0.22873E+07
   ------------------------------------------------------
   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         38 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.78721E+12    3528   0.98406E+00   0.38828E+12 
c  VelocityY    0.78721E+12    3528   0.98406E+00   0.00000E+00 
c  VelocityZ    0.78721E+12    3528   0.98406E+00   0.00000E+00 
c  Pressure     0.18264E+05     570   0.14607E-01   0.11526E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.5886e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.0708e+06      3.0552e+06         -5722.8         -1491.7
v  Velocity[Y]              -3.386e+06      6.5607e+06           -1580         -1294.8
v  Velocity[Z]             -3.9518e+06      6.6062e+06          498.59          3584.8
v  ǁVelocityǁ                   26.792      8.0779e+06           63352           46615
v  Pressure                -3.5081e+09      4.1589e+09      3.4431e+08      2.3391e+08
v  turbulent_viscosity          13.344      1.7412e+07          4491.4          2773.8
v  CourantNb                    136.02      8.3492e+08      1.1856e+06       6.011e+05
v  FourierNb                    955.46      9.2119e+09      9.4773e+05      3.0519e+05
v  total_pressure          -3.5076e+09      4.1594e+09      3.4481e+08      2.3441e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2235.4      9.5521e+09      2.1334e+06      9.0629e+05


 TIME FOR THE TIME STEP              177:        0.52271E+01

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


 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         0.734766891E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.322696013E+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 :  0.13017E+02 0.10380E+08
   Friction velocity        uet   :  0.14671E+01 0.28240E+06
   Friction velocity        uk    :  0.14671E+01 0.28240E+06
   Dimensionless distance   yplus :  0.20955E+02 0.25539E+07
   ------------------------------------------------------
   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         40 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.99589E+12    2802   0.98564E+00   0.39763E+12 
c  VelocityY    0.99589E+12    2802   0.98564E+00   0.00000E+00 
c  VelocityZ    0.99589E+12    2802   0.98564E+00   0.00000E+00 
c  Pressure     0.20008E+05     600   0.13604E-01   0.11361E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.7014e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8216e+06      3.3743e+06         -1761.9         -1713.2
v  Velocity[Y]             -4.0612e+06      7.2624e+06         -7046.8         -1443.5
v  Velocity[Z]             -4.4197e+06      7.3489e+06          1010.5          4662.8
v  ǁVelocityǁ                   38.557      8.9452e+06           56371           40660
v  Pressure                -3.7592e+09      4.5734e+09      3.7574e+08      2.5489e+08
v  turbulent_viscosity           15.15      1.9603e+07          4823.9          3064.5
v  CourantNb                    53.317      9.3163e+08      1.4625e+06      8.0627e+05
v  FourierNb                    947.95      1.1617e+10      1.0356e+06      3.3198e+05
v  total_pressure          -3.7587e+09      4.5739e+09      3.7624e+08      2.5539e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            3012      1.1996e+10      2.4981e+06      1.1382e+06


 TIME FOR THE TIME STEP              178:        0.42975E+01

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


 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         0.218425234E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.325923395E+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 :  0.28027E+02 0.11507E+08
   Friction velocity        uet   :  0.25426E+01 0.31113E+06
   Friction velocity        uk    :  0.25426E+01 0.31113E+06
   Dimensionless distance   yplus :  0.21748E+02 0.28137E+07
   ------------------------------------------------------
   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         44 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.12200E+13    3200   0.98575E+00   0.62654E+12 
c  VelocityY    0.12200E+13    3200   0.98575E+00   0.00000E+00 
c  VelocityZ    0.12200E+13    3200   0.98575E+00   0.00000E+00 
c  Pressure     0.22820E+05     621   0.15601E-01   0.11621E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.2479e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5111e+06      3.7619e+06         -5248.5           -1600
v  Velocity[Y]             -4.1897e+06      8.0788e+06         -1800.5         -1738.9
v  Velocity[Z]             -4.8058e+06      8.2604e+06         -5142.2          5123.3
v  ǁVelocityǁ                   159.24       9.889e+06           86384           63580
v  Pressure                 -4.315e+09      5.1791e+09      4.4022e+08      3.0432e+08
v  turbulent_viscosity           11.66      2.1648e+07          5339.2          3339.3
v  CourantNb                    330.68      1.0356e+09      1.3246e+06      6.9837e+05
v  FourierNb                    894.29       1.144e+10      1.1329e+06      3.6368e+05
v  total_pressure          -4.3145e+09      5.1796e+09      4.4072e+08      3.0482e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2940.2      1.1861e+10      2.4575e+06       1.062e+06


 TIME FOR THE TIME STEP              179:        0.48757E+01

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


 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         0.518426968E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.332903781E+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 :  0.23815E+02 0.12791E+08
   Friction velocity        uet   :  0.24236E+01 0.34364E+06
   Friction velocity        uk    :  0.24236E+01 0.34364E+06
   Dimensionless distance   yplus :  0.31282E+02 0.31077E+07
   ------------------------------------------------------
   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         40 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.15106E+13    2703   0.98522E+00   0.60991E+12 
c  VelocityY    0.15106E+13    2703   0.98522E+00   0.00000E+00 
c  VelocityZ    0.15106E+13    2703   0.98522E+00   0.00000E+00 
c  Pressure     0.24921E+05     611   0.14292E-01   0.11406E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.6264e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5513e+06      4.0651e+06         -2691.8         -2137.9
v  Velocity[Y]             -5.0233e+06      8.9596e+06         -9922.6         -2058.4
v  Velocity[Z]             -5.5113e+06      8.9908e+06          3894.1          6183.5
v  ǁVelocityǁ                   98.374        1.11e+07           62520           44991
v  Pressure                -4.5928e+09      5.7678e+09      4.9946e+08      3.4477e+08
v  turbulent_viscosity          22.387      2.4115e+07          6173.9          4006.2
v  CourantNb                    1576.3      1.1515e+09      1.9884e+06      1.0903e+06
v  FourierNb                      1453      1.2722e+10      1.2904e+06      4.2568e+05
v  total_pressure          -4.5923e+09      5.7683e+09      4.9996e+08      3.4527e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6834.8       1.319e+10      3.2788e+06       1.516e+06


 TIME FOR THE TIME STEP              180:        0.42606E+01

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


 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         0.651514541E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.351672658E+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 :  0.66339E+02 0.14244E+08
   Friction velocity        uet   :  0.56910E+01 0.38022E+06
   Friction velocity        uk    :  0.56910E+01 0.38022E+06
   Dimensionless distance   yplus :  0.50806E+02 0.34385E+07
   ------------------------------------------------------
   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         43 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.18592E+13    3128   0.98693E+00   0.72339E+12 
c  VelocityY    0.18592E+13    3128   0.98693E+00   0.00000E+00 
c  VelocityZ    0.18592E+13    3128   0.98693E+00   0.00000E+00 
c  Pressure     0.28286E+05     593   0.15301E-01   0.11613E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      3.0419e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9811e+06      4.6734e+06         -7991.6         -1889.7
v  Velocity[Y]             -5.1186e+06      1.0052e+07         -2662.7         -1920.9
v  Velocity[Z]             -6.0613e+06      1.0153e+07         -9291.5          6893.6
v  ǁVelocityǁ                   234.09      1.2327e+07      1.0094e+05           74507
v  Pressure                -5.2416e+09      6.4529e+09      5.6122e+08      3.9919e+08
v  turbulent_viscosity          9.9654      2.6717e+07          6707.9          4264.9
v  CourantNb                    343.28      1.2813e+09      1.4743e+06      7.6408e+05
v  FourierNb                    1611.7      1.5863e+10      1.4367e+06      4.5953e+05
v  total_pressure          -5.2411e+09      6.4534e+09      5.6172e+08      3.9969e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4059.9      1.6385e+10       2.911e+06      1.2236e+06


 TIME FOR THE TIME STEP              181:        0.54813E+01

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


 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         0.674303755E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.365493406E+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 :  0.23384E+03 0.15961E+08
   Friction velocity        uet   :  0.17220E+02 0.42317E+06
   Friction velocity        uk    :  0.17220E+02 0.42317E+06
   Dimensionless distance   yplus :  0.15134E+03 0.38269E+07
   ------------------------------------------------------
   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         41 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.23377E+13    2601   0.98197E+00   0.74074E+12 
c  VelocityY    0.23377E+13    2601   0.98197E+00   0.00000E+00 
c  VelocityZ    0.23377E+13    2601   0.98197E+00   0.00000E+00 
c  Pressure     0.30234E+05     622   0.13362E-01   0.11179E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.6234e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -9.683e+06      5.0458e+06         -5023.9         -2330.8
v  Velocity[Y]             -6.1859e+06      1.1121e+07         -7919.3         -2526.3
v  Velocity[Z]             -6.7737e+06      1.1241e+07          4550.4          7617.3
v  ǁVelocityǁ                   64.664      1.3705e+07           73645           53570
v  Pressure                -5.5258e+09      7.1563e+09       6.456e+08      4.5763e+08
v  turbulent_viscosity          48.394       3.001e+07          7789.5            5171
v  CourantNb                    954.19      1.4149e+09      2.3318e+06       1.266e+06
v  FourierNb                    2754.7      1.7789e+10      1.6437e+06       5.407e+05
v  total_pressure          -5.5253e+09      7.1568e+09       6.461e+08      4.5813e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           13048      1.8373e+10      3.9755e+06      1.8067e+06


 TIME FOR THE TIME STEP              182:        0.41687E+01

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


 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         0.860937363E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.369087924E+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 :  0.48305E+02 0.17682E+08
   Friction velocity        uet   :  0.39099E+01 0.46596E+06
   Friction velocity        uk    :  0.39099E+01 0.46596E+06
   Dimensionless distance   yplus :  0.47045E+02 0.42139E+07
   ------------------------------------------------------
   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         47 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.28749E+13    3231   0.98747E+00   0.10921E+13 
c  VelocityY    0.28749E+13    3231   0.98747E+00   0.00000E+00 
c  VelocityZ    0.28749E+13    3231   0.98747E+00   0.00000E+00 
c  Pressure     0.35387E+05     594   0.16191E-01   0.11720E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.6821e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1635e+07      5.7211e+06          -11965         -2751.8
v  Velocity[Y]             -6.3637e+06      1.2335e+07         -7046.4           -2709
v  Velocity[Z]             -7.3233e+06      1.2622e+07         -5724.6          7688.7
v  ǁVelocityǁ                   72.459      1.5078e+07      1.3539e+05           94574
v  Pressure                -6.3464e+09       8.138e+09      7.1749e+08      5.0481e+08
v  turbulent_viscosity          36.345      3.3146e+07            8152          5197.4
v  CourantNb                    123.16      1.5682e+09      1.7372e+06      9.0568e+05
v  FourierNb                    2350.4      1.7497e+10      1.7201e+06      5.5748e+05
v  total_pressure          -6.3459e+09      8.1385e+09      7.1799e+08      5.0531e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6627.6      1.8135e+10      3.4573e+06      1.4632e+06


 TIME FOR THE TIME STEP              183:        0.48611E+01

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


 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        -0.296171507E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.405653564E+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 :  0.13115E+02 0.19512E+08
   Friction velocity        uet   :  0.14842E+01 0.51120E+06
   Friction velocity        uk    :  0.14842E+01 0.51120E+06
   Dimensionless distance   yplus :  0.20639E+02 0.46231E+07
   ------------------------------------------------------
   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         42 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.35165E+13    2651   0.98049E+00   0.10727E+13 
c  VelocityY    0.35165E+13    2651   0.98049E+00   0.00000E+00 
c  VelocityZ    0.35165E+13    2651   0.98049E+00   0.00000E+00 
c  Pressure     0.37233E+05     624   0.12434E-01   0.11123E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step       1.689e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1864e+07      6.3428e+06         -3347.3           -2936
v  Velocity[Y]              -7.669e+06      1.3759e+07          -11624         -2869.9
v  Velocity[Z]             -8.3281e+06      1.3922e+07         -3163.7          9287.7
v  ǁVelocityǁ                   148.64      1.6917e+07           84235           64085
v  Pressure                -6.6503e+09      8.8958e+09      8.3138e+08      5.8867e+08
v  turbulent_viscosity          23.539      3.6785e+07          9829.3          6299.9
v  CourantNb                    798.67      1.7567e+09      3.1508e+06      1.6536e+06
v  FourierNb                    1977.9      2.1829e+10      2.0741e+06      6.7775e+05
v  total_pressure          -6.6498e+09      8.8963e+09      8.3188e+08      5.8917e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3662.8       2.254e+10      5.2249e+06      2.3313e+06


 TIME FOR THE TIME STEP              184:        0.42621E+01

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


 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         0.878740310E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.405079228E+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 :  0.25606E+02 0.21854E+08
   Friction velocity        uet   :  0.29249E+01 0.56878E+06
   Friction velocity        uk    :  0.29249E+01 0.56878E+06
   Dimensionless distance   yplus :  0.19944E+02 0.51438E+07
   ------------------------------------------------------
   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         41 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.44114E+13    2859   0.99205E+00   0.21887E+13 
c  VelocityY    0.44114E+13    2859   0.99205E+00   0.00000E+00 
c  VelocityZ    0.44114E+13    2859   0.99205E+00   0.00000E+00 
c  Pressure     0.44522E+05     574   0.17795E-01   0.11896E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      2.1008e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.429e+07      6.9296e+06         -6715.8         -3966.6
v  Velocity[Y]             -7.9376e+06      1.5253e+07         -6253.6         -3270.1
v  Velocity[Z]             -9.0973e+06      1.5635e+07          -15394          9512.2
v  ǁVelocityǁ                   66.229      1.8666e+07        1.91e+05      1.3622e+05
v  Pressure                -7.8717e+09      1.0123e+10      8.9243e+08      6.2273e+08
v  turbulent_viscosity          30.672      4.1037e+07          9762.9          6277.1
v  CourantNb                    163.56      1.9382e+09      1.9946e+06      1.0739e+06
v  FourierNb                    2421.4      2.1661e+10        2.07e+06      6.6903e+05
v  total_pressure          -7.8712e+09      1.0124e+10      8.9293e+08      6.2323e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4260.5      2.2444e+10      4.0646e+06      1.7429e+06


 TIME FOR THE TIME STEP              185:        0.45991E+01

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


 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        -0.120592755E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.432652441E+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 :  0.36643E+02 0.24285E+08
   Friction velocity        uet   :  0.32967E+01 0.62819E+06
   Friction velocity        uk    :  0.32967E+01 0.62819E+06
   Dimensionless distance   yplus :  0.41033E+02 0.56810E+07
   ------------------------------------------------------
   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         40 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.53604E+13    2804   0.97830E+00   0.21640E+13 
c  VelocityY    0.53604E+13    2804   0.97830E+00   0.00000E+00 
c  VelocityZ    0.53604E+13    2804   0.97830E+00   0.00000E+00 
c  Pressure     0.46650E+05     625   0.13101E-01   0.11237E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.8504e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.4633e+07      7.7645e+06         -9686.3           -4624
v  Velocity[Y]             -9.3642e+06       1.704e+07          -15423         -3477.9
v  Velocity[Z]             -1.0576e+07      1.6967e+07          6854.2           12383
v  ǁVelocityǁ                   276.62      2.1123e+07           93140           71485
v  Pressure                -8.2704e+09      1.1162e+10      1.0332e+09       7.258e+08
v  turbulent_viscosity          20.835      4.5452e+07           12470            8025
v  CourantNb                    983.78      2.1458e+09      4.3913e+06      2.3643e+06
v  FourierNb                      2137      2.4013e+10      2.5666e+06      8.5941e+05
v  total_pressure          -8.2699e+09      1.1163e+10      1.0337e+09       7.263e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6378.7      2.4901e+10      6.9579e+06      3.2237e+06


 TIME FOR THE TIME STEP              186:        0.49641E+01

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


 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         0.195460714E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.440224657E+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 :  0.45298E+03 0.27123E+08
   Friction velocity        uet   :  0.28056E+02 0.69713E+06
   Friction velocity        uk    :  0.28056E+02 0.69713E+06
   Dimensionless distance   yplus :  0.13920E+03 0.63045E+07
   ------------------------------------------------------
   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         35 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.68040E+13    2934   0.98208E+00   0.32810E+13 
c  VelocityY    0.68040E+13    2934   0.98208E+00   0.00000E+00 
c  VelocityZ    0.68040E+13    2934   0.98208E+00   0.00000E+00 
c  Pressure     0.55855E+05     625   0.17327E-01   0.12024E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.8162e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6635e+07      8.4248e+06          -10054         -2568.6
v  Velocity[Y]             -9.7346e+06      1.9218e+07         -2244.5         -3523.4
v  Velocity[Z]             -1.1707e+07      1.9809e+07          -24725           13508
v  ǁVelocityǁ                   633.53      2.3764e+07      2.4212e+05      1.7481e+05
v  Pressure                -9.6243e+09      1.2745e+10      1.2411e+09      9.0769e+08
v  turbulent_viscosity          60.039      5.0852e+07           12203          7960.5
v  CourantNb                    1199.7       2.392e+09      2.2195e+06      1.1826e+06
v  FourierNb                    3595.7      2.6834e+10      2.5688e+06      8.3991e+05
v  total_pressure          -9.6238e+09      1.2745e+10      1.2416e+09      9.0819e+08
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           19291      2.7803e+10      4.7883e+06      2.0226e+06


 TIME FOR THE TIME STEP              187:        0.46457E+01

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


 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        -0.191010489E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.417784106E+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 :  0.67007E+03 0.30657E+08
   Friction velocity        uet   :  0.40530E+02 0.78244E+06
   Friction velocity        uk    :  0.40530E+02 0.78244E+06
   Dimensionless distance   yplus :  0.38608E+03 0.70760E+07
   ------------------------------------------------------
   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         35 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.85989E+13    2761   0.98720E+00   0.35078E+13 
c  VelocityY    0.85989E+13    2761   0.98720E+00   0.00000E+00 
c  VelocityZ    0.85989E+13    2761   0.98720E+00   0.00000E+00 
c  Pressure     0.58493E+05     663   0.13941E-01   0.11346E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.1449e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.9987e+07      9.8351e+06          -15674         -4824.4
v  Velocity[Y]             -1.1996e+07      2.0852e+07          -22993         -6162.3
v  Velocity[Z]             -1.2726e+07      2.1342e+07           14150           14363
v  ǁVelocityǁ                   480.39      2.5539e+07      1.3219e+05           97813
v  Pressure                -9.6215e+09      1.4657e+10      1.6862e+09       1.222e+09
v  turbulent_viscosity          150.61      5.7265e+07           16151           10666
v  CourantNb                    975.67      2.6598e+09      5.5643e+06      2.9915e+06
v  FourierNb                    9278.3      3.0245e+10      3.2928e+06      1.1196e+06
v  total_pressure           -9.621e+09      1.4657e+10      1.6867e+09      1.2225e+09
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           34527      3.1327e+10      8.8572e+06      4.1111e+06


 TIME FOR THE TIME STEP              188:        0.49430E+01

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


 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         0.141354081E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.465059553E+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 :  0.13705E+02 0.33090E+08
   Friction velocity        uet   :  0.15596E+01 0.84085E+06
   Friction velocity        uk    :  0.15596E+01 0.84085E+06
   Dimensionless distance   yplus :  0.20218E+02 0.76042E+07
   ------------------------------------------------------
   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         41 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10108E+14    2913   0.98044E+00   0.49313E+13 
c  VelocityY    0.10108E+14    2913   0.98044E+00   0.00000E+00 
c  VelocityZ    0.10108E+14    2913   0.98044E+00   0.00000E+00 
c  Pressure     0.69176E+05     537   0.17420E-01   0.12034E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.4986e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.2196e+07      1.0488e+07          -25241         -8810.7
v  Velocity[Y]             -1.2142e+07      2.3576e+07         -2738.7         -4413.7
v  Velocity[Z]             -1.4755e+07      2.4054e+07          -15867           15436
v  ǁVelocityǁ                   395.11      2.9489e+07      2.6391e+05      1.9166e+05
v  Pressure                -1.1858e+10      1.6014e+10      1.6557e+09      1.1697e+09
v  turbulent_viscosity          84.107      6.2006e+07           15789           10177
v  CourantNb                     877.9      2.9593e+09      3.1243e+06      1.6551e+06
v  FourierNb                      6712      3.2818e+10       3.288e+06       1.084e+06
v  total_pressure          -1.1857e+10      1.6015e+10      1.6562e+09      1.1702e+09
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           24663      3.4019e+10      6.4123e+06      2.7391e+06


 TIME FOR THE TIME STEP              189:        0.48263E+01

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


 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        -0.275787743E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.454746228E+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 :  0.80986E+03 0.37760E+08
   Friction velocity        uet   :  0.43499E+02 0.95235E+06
   Friction velocity        uk    :  0.43499E+02 0.95235E+06
   Dimensionless distance   yplus :  0.28593E+03 0.86126E+07
   ------------------------------------------------------
   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         43 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.12957E+14    2720   0.98219E+00   0.93392E+13 
c  VelocityY    0.12957E+14    2720   0.98219E+00   0.00000E+00 
c  VelocityZ    0.12957E+14    2720   0.98219E+00   0.00000E+00 
c  Pressure     0.74231E+05     605   0.14655E-01   0.11630E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.2934e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.3055e+07      1.2028e+07         -765.58         -6098.3
v  Velocity[Y]             -1.4596e+07      2.6095e+07          -18229         -5459.7
v  Velocity[Z]             -1.5917e+07      2.6205e+07          -25795           16097
v  ǁVelocityǁ                   178.34      3.2164e+07      2.7672e+05        1.99e+05
v  Pressure                -1.2789e+10      1.7639e+10      1.8081e+09      1.2647e+09
v  turbulent_viscosity          137.51        7.04e+07           20197           13096
v  CourantNb                    762.94      3.3231e+09      6.0747e+06      3.2947e+06
v  FourierNb                     13163      3.7181e+10      4.1397e+06      1.3942e+06
v  total_pressure          -1.2789e+10       1.764e+10      1.8086e+09      1.2652e+09
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           49430      3.8536e+10      1.0214e+07      4.6889e+06


 TIME FOR THE TIME STEP              190:        0.45385E+01

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


 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        -0.278236115E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.465890773E+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 :  0.16685E+03 0.41598E+08
   Friction velocity        uet   :  0.13076E+02 0.10434E+07
   Friction velocity        uk    :  0.13076E+02 0.10434E+07
   Dimensionless distance   yplus :  0.10725E+03 0.94361E+07
   ------------------------------------------------------
   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         46 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.15915E+14    3221   0.98776E+00   0.81314E+13 
c  VelocityY    0.15915E+14    3221   0.98776E+00   0.00000E+00 
c  VelocityZ    0.15915E+14    3221   0.98776E+00   0.00000E+00 
c  Pressure     0.81448E+05     593   0.15073E-01   0.11480E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      8.2074e-11                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6712e+07      1.3698e+07          -34414         -8458.3
v  Velocity[Y]             -1.5214e+07      2.8997e+07          -14940         -6066.1
v  Velocity[Z]             -1.7714e+07      3.0001e+07           26388           17276
v  ǁVelocityǁ                   373.53      3.5689e+07      2.5511e+05      1.8731e+05
v  Pressure                -1.4532e+10      1.9689e+10      1.9935e+09      1.3925e+09
v  turbulent_viscosity          67.565      7.7681e+07           20793           13091
v  CourantNb                    1213.5      3.6586e+09      6.4174e+06      3.4559e+06
v  FourierNb                    6313.2      4.6108e+10      4.3929e+06       1.423e+06
v  total_pressure          -1.4532e+10       1.969e+10       1.994e+09       1.393e+09
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7655.8      4.7589e+10       1.081e+07      4.8789e+06


 TIME FOR THE TIME STEP              191:        0.50721E+01

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


 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        -0.433716778E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.585844002E+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 :  0.20716E+03 0.46311E+08
   Friction velocity        uet   :  0.14256E+02 0.11547E+07
   Friction velocity        uk    :  0.14256E+02 0.11547E+07
   Dimensionless distance   yplus :  0.17564E+03 0.10442E+08
   ------------------------------------------------------
   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         35 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.19496E+14    2647   0.97904E+00   0.90322E+13 
c  VelocityY    0.19496E+14    2647   0.97904E+00   0.00000E+00 
c  VelocityZ    0.19496E+14    2647   0.97904E+00   0.00000E+00 
c  Pressure     0.91940E+05     627   0.14593E-01   0.11645E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      1.2484e-10                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.8534e+07       1.415e+07         -2476.1         -7241.9
v  Velocity[Y]              -1.818e+07      3.2315e+07          -26007         -7217.4
v  Velocity[Z]             -2.0283e+07      3.2243e+07          -28911           21851
v  ǁVelocityǁ                   537.34      4.0345e+07      3.1636e+05      2.1895e+05
v  Pressure                -1.5433e+10      2.2046e+10      2.3172e+09      1.6204e+09
v  turbulent_viscosity          64.865       8.643e+07           22312           13999
v  CourantNb                      1216      4.0605e+09        5.88e+06       3.224e+06
v  FourierNb                    6467.1      4.5712e+10       4.674e+06      1.5267e+06
v  total_pressure          -1.5432e+10      2.2046e+10      2.3177e+09      1.6209e+09
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           21485      4.7384e+10      1.0554e+07      4.7507e+06


 TIME FOR THE TIME STEP              192:        0.43615E+01

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


 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         0.862736271E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.589361422E+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 :  0.35450E+03 0.51788E+08
   Friction velocity        uet   :  0.23291E+02 0.12832E+07
   Friction velocity        uk    :  0.23291E+02 0.12832E+07
   Dimensionless distance   yplus :  0.75033E+02 0.11604E+08
   ------------------------------------------------------
   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         40 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.24373E+14    3097   0.98105E+00   0.96953E+13 
c  VelocityY    0.24373E+14    3097   0.98105E+00   0.00000E+00 
c  VelocityZ    0.24373E+14    3097   0.98105E+00   0.00000E+00 
c  Pressure     0.98439E+05     596   0.13957E-01   0.11238E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      5.6517e-11                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.0217e+07      1.6809e+07          -30670         -8656.3
v  Velocity[Y]             -1.8346e+07      3.6159e+07          -20768         -7359.1
v  Velocity[Z]             -2.1332e+07      3.6954e+07           18398           20933
v  ǁVelocityǁ                   1091.7      4.3952e+07      2.7872e+05      2.1375e+05
v  Pressure                -1.7322e+10       2.447e+10        2.58e+09      1.8098e+09
v  turbulent_viscosity          55.044      9.6319e+07           25429           15936
v  CourantNb                    251.13      4.5252e+09       7.442e+06      3.8354e+06
v  FourierNb                    7843.2      5.0862e+10      5.3147e+06      1.7332e+06
v  total_pressure          -1.7321e+10       2.447e+10      2.5805e+09      1.8103e+09
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           16327      5.2703e+10      1.2757e+07      5.5687e+06


 TIME FOR THE TIME STEP              193:        0.46038E+01

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


 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         0.280386929E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.650427052E+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 :  0.88656E+02 0.57318E+08
   Friction velocity        uet   :  0.72296E+01 0.14122E+07
   Friction velocity        uk    :  0.72296E+01 0.14122E+07
   Dimensionless distance   yplus :  0.87048E+02 0.12771E+08
   ------------------------------------------------------
   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         35 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30502E+14    2668   0.98890E+00   0.12523E+14 
c  VelocityY    0.30502E+14    2668   0.98890E+00   0.00000E+00 
c  VelocityZ    0.30502E+14    2668   0.98890E+00   0.00000E+00 
c  Pressure     0.11439E+06     630   0.15339E-01   0.11712E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      9.9474e-11                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.8604e+07      1.7782e+07         -3513.3         -9868.3
v  Velocity[Y]             -2.2521e+07      3.9442e+07          -43340         -9721.7
v  Velocity[Z]             -2.3843e+07       4.093e+07          -15484           27478
v  ǁVelocityǁ                   507.03      4.8384e+07      3.9233e+05      2.6307e+05
v  Pressure                -1.8394e+10      2.7607e+10      3.0208e+09      2.1086e+09
v  turbulent_viscosity          122.88      1.0776e+08           26438           16604
v  CourantNb                     856.8      5.0248e+09      6.4303e+06      3.6216e+06
v  FourierNb                    7388.4      5.6855e+10        5.59e+06      1.8075e+06
v  total_pressure          -1.8393e+10      2.7608e+10      3.0213e+09      2.1091e+09
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           28723      5.8862e+10       1.202e+07      5.4291e+06


 TIME FOR THE TIME STEP              194:        0.41111E+01

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


 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         0.253931424E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.698076218E+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 :  0.23852E+03 0.62963E+08
   Friction velocity        uet   :  0.15554E+02 0.15433E+07
   Friction velocity        uk    :  0.15554E+02 0.15433E+07
   Dimensionless distance   yplus :  0.28847E+03 0.13957E+08
   ------------------------------------------------------
   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         40 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.36051E+14    2961   0.98129E+00   0.14975E+14 
c  VelocityY    0.36051E+14    2961   0.98129E+00   0.00000E+00 
c  VelocityZ    0.36051E+14    2961   0.98129E+00   0.00000E+00 
c  Pressure     0.12198E+06     608   0.13959E-01   0.11255E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.1222e-11                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.1384e+07      2.0691e+07          -28436         -8949.5
v  Velocity[Y]             -2.2928e+07      4.4417e+07          -16724         -8796.9
v  Velocity[Z]             -2.7157e+07      4.4576e+07         -5619.1           28242
v  ǁVelocityǁ                   1666.4      5.4806e+07      3.3802e+05       2.809e+05
v  Pressure                -2.0727e+10      3.0477e+10      3.4701e+09       2.499e+09
v  turbulent_viscosity           43.89      1.1731e+08           32610           20270
v  CourantNb                    944.62      5.6035e+09      9.2626e+06      4.6417e+06
v  FourierNb                    5134.1      6.2116e+10      6.7733e+06      2.2186e+06
v  total_pressure          -2.0727e+10      3.0477e+10      3.4706e+09      2.4995e+09
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           13565      6.4394e+10      1.6036e+07      6.8603e+06


 TIME FOR THE TIME STEP              195:        0.52893E+01

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


 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         0.299021294E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.707350983E+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 :  0.17218E+03 0.70937E+08
   Friction velocity        uet   :  0.11947E+02 0.17273E+07
   Friction velocity        uk    :  0.11947E+02 0.17273E+07
   Dimensionless distance   yplus :  0.21464E+03 0.15621E+08
   ------------------------------------------------------
   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         33 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.46031E+14    2714   0.98458E+00   0.19369E+14 
c  VelocityY    0.46031E+14    2714   0.98458E+00   0.00000E+00 
c  VelocityZ    0.46031E+14    2714   0.98458E+00   0.00000E+00 
c  Pressure     0.14160E+06     591   0.16400E-01   0.11714E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      9.7465e-11                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.713e+07      2.1994e+07          -10362          -12285
v  Velocity[Y]             -2.7516e+07      4.9294e+07          -51090           -9652
v  Velocity[Z]             -3.0327e+07      5.0276e+07         -7545.2           34954
v  ǁVelocityǁ                   458.97      6.0913e+07       5.115e+05      3.4813e+05
v  Pressure                -2.2815e+10      3.4026e+10       3.655e+09      2.6219e+09
v  turbulent_viscosity          233.17      1.3267e+08           33326           21763
v  CourantNb                     11698      6.2589e+09      7.6956e+06      4.5921e+06
v  FourierNb                     15885      6.9995e+10      6.9696e+06      2.3017e+06
v  total_pressure          -2.2815e+10      3.4027e+10      3.6555e+09      2.6224e+09
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      1.3445e+05      7.2529e+10      1.4665e+07      6.8937e+06


 TIME FOR THE TIME STEP              196:        0.47640E+01

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


 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        -0.930871526E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.665364856E+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 :  0.34699E+03 0.78953E+08
   Friction velocity        uet   :  0.22787E+02 0.19113E+07
   Friction velocity        uk    :  0.22787E+02 0.19113E+07
   Dimensionless distance   yplus :  0.23718E+03 0.17285E+08
   ------------------------------------------------------
   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         50 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.56594E+14    3239   0.98358E+00   0.28879E+14 
c  VelocityY    0.56594E+14    3239   0.98358E+00   0.00000E+00 
c  VelocityZ    0.56594E+14    3239   0.98358E+00   0.00000E+00 
c  Pressure     0.15386E+06     617   0.14873E-01   0.11457E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.0457e-11                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.0754e+07      2.6103e+07          -28281          -14489
v  Velocity[Y]             -2.8515e+07      5.4757e+07          -36857          -12432
v  Velocity[Z]             -3.2806e+07       5.581e+07          -11663           32949
v  ǁVelocityǁ                   138.36      6.6816e+07      5.1901e+05      3.8986e+05
v  Pressure                -2.6102e+10      3.8128e+10      4.0904e+09      2.9216e+09
v  turbulent_viscosity          164.65      1.4683e+08           40416           25382
v  CourantNb                      2336      6.9772e+09         1.2e+07      6.0849e+06
v  FourierNb                     12329      7.7644e+10      8.4049e+06      2.7577e+06
v  total_pressure          -2.6101e+10      3.8129e+10      4.0909e+09      2.9221e+09
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           34909      8.0483e+10      2.0404e+07      8.8426e+06


 TIME FOR THE TIME STEP              197:        0.55902E+01

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


 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         0.178906490E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.670453966E+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 :  0.37498E+03 0.87285E+08
   Friction velocity        uet   :  0.23201E+02 0.21015E+07
   Friction velocity        uk    :  0.23201E+02 0.21015E+07
   Dimensionless distance   yplus :  0.34231E+03 0.19005E+08
   ------------------------------------------------------
   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         41 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.69942E+14    2526   0.98451E+00   0.28844E+14 
c  VelocityY    0.69942E+14    2526   0.98451E+00   0.00000E+00 
c  VelocityZ    0.69942E+14    2526   0.98451E+00   0.00000E+00 
c  Pressure     0.17550E+06     625   0.15367E-01   0.11730E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.7331e-11                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.9005e+07      2.7062e+07           36212          -15519
v  Velocity[Y]             -3.4017e+07      6.0798e+07          -63446          -14773
v  Velocity[Z]             -3.7555e+07      6.1376e+07          -54807           43390
v  ǁVelocityǁ                   853.99      7.5403e+07      5.0933e+05       3.762e+05
v  Pressure                -2.8196e+10      4.2383e+10      4.6752e+09      3.3176e+09
v  turbulent_viscosity          116.87      1.6335e+08           41410           26453
v  CourantNb                    6923.7      7.7548e+09      1.1953e+07      6.6676e+06
v  FourierNb                    7606.2      8.6203e+10      8.6891e+06      2.8427e+06
v  total_pressure          -2.8195e+10      4.2384e+10      4.6757e+09      3.3181e+09
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           38219      8.9335e+10      2.0642e+07      9.5103e+06


 TIME FOR THE TIME STEP              198:        0.40860E+01

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


 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         0.943069789E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.831939640E+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 :  0.52994E+03 0.97619E+08
   Friction velocity        uet   :  0.32310E+02 0.23362E+07
   Friction velocity        uk    :  0.32310E+02 0.23362E+07
   Dimensionless distance   yplus :  0.37234E+03 0.21127E+08
   ------------------------------------------------------
   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         42 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.86140E+14    2880   0.98256E+00   0.33240E+14 
c  VelocityY    0.86140E+14    2880   0.98256E+00   0.00000E+00 
c  VelocityZ    0.86140E+14    2880   0.98256E+00   0.00000E+00 
c  Pressure     0.19127E+06     614   0.15301E-01   0.11492E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.5458e-11                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.2766e+07      3.2183e+07          -50622          -14888
v  Velocity[Y]              -3.504e+07      6.7983e+07          -48931          -13229
v  Velocity[Z]             -4.0917e+07      6.9015e+07          -12619           46662
v  ǁVelocityǁ                   2599.2      8.3062e+07      6.6047e+05       4.956e+05
v  Pressure                -3.1752e+10      4.7553e+10      5.4601e+09      4.0629e+09
v  turbulent_viscosity          86.371      1.8118e+08           47057           30211
v  CourantNb                    1356.4      8.6435e+09      1.1871e+07      6.3867e+06
v  FourierNb                    7940.5      9.5795e+10      9.8377e+06      3.2281e+06
v  total_pressure          -3.1752e+10      4.7553e+10      5.4606e+09      4.0634e+09
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           34099      9.9322e+10      2.1708e+07      9.6148e+06


 TIME FOR THE TIME STEP              199:        0.51013E+01

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


 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         0.594297805E-10
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.103159089E+01
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.13364E+04 0.10847E+09
   Friction velocity        uet   :  0.74306E+02 0.25812E+07
   Friction velocity        uk    :  0.74306E+02 0.25812E+07
   Dimensionless distance   yplus :  0.70687E+03 0.23343E+08
   ------------------------------------------------------
   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         34 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:    0.93533E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10794E+15    2609   0.98477E+00   0.33900E+14 
c  VelocityY    0.10794E+15    2609   0.98477E+00   0.00000E+00 
c  VelocityZ    0.10794E+15    2609   0.98477E+00   0.00000E+00 
c  Pressure     0.20827E+06     605   0.13546E-01   0.11256E+00 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  Local Time Step      4.6286e-11                         16761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1992e+07      3.3928e+07          2599.1          -18398
v  Velocity[Y]             -4.2526e+07      7.4946e+07          -82428          -17043
v  Velocity[Z]             -4.5833e+07      7.6686e+07          828.47           50455
v  ǁVelocityǁ                   641.24      9.2323e+07      5.5809e+05      3.9566e+05
v  Pressure                -3.4125e+10      5.2274e+10      5.8916e+09      4.3507e+09
v  turbulent_viscosity          286.44      2.0287e+08           51945           34298
v  CourantNb                     22999      9.6117e+09      1.5227e+07      8.3687e+06
v  FourierNb                     26140      1.0704e+11      1.0804e+07      3.5944e+06
v  total_pressure          -3.4125e+10      5.2274e+10      5.8921e+09      4.3512e+09
v  Local Time Step                0.01            0.01            0.01            0.01


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      1.5807e+05      1.1092e+11      2.6031e+07      1.1963e+07


 TIME FOR THE TIME STEP              200:        0.46600E+01

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.11153E-03
      -----------------------                                



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




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


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

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:            602.832 s
  System CPU time:            2.012 s
  Total CPU time:          2419.724 s

  Elapsed time:             606.619 s
  CPU / elapsed time          0.997

Memory use summary:

  Total memory used:                             564.602 MiB
                             local minimum:      140.820 MiB  (rank 2)
                             local maximum:      141.438 MiB  (rank 1)
  Theoretical instrumented dynamic memory:        71.822 MiB
                             local minimum:       16.587 MiB  (rank 2)
                             local maximum:       21.771 MiB  (rank 0)
