command: 
 /usr/local/libexec/code_saturne/cs_solver --param CilCurs_1ms_test03.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:                Tue 15 Jul 2014 01:42:55 PM 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/20140715-1342
  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 =              0 (0 cst; 1,2 var (t, t-space  )
       IPTLRO =              0 (1: rho-related DT clipping  )
       COUMAX =    0.10000E+01 (Maximum target CFL          )
       FOUMAX =    0.10000E+02 (Maximum target Fourier      )
       VARRDT =    0.10000E+00 (For var. DT, max. increase  )
       DTMIN  =    0.10000E-01 (Minimum time step           )
       DTMAX  =    0.10000E+03 (Maximum time step           )
       DTREF  =    0.10000E+00 (Reference time step         )

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

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

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

       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 =              2 (Reconstruction mode         )
       ANOMAX =    0.78540E+00 (Non-ortho angle: limit for  )
                               (least squares ext. neighbors)

-------------------------------------------------------------------
 Variable         NSWRGR NSWRSM      EPSRGR      EPSRSM      EXTRAG
-------------------------------------------------------------------
 Velocity            100      1  0.1000E-04  0.1000E-06  0.0000E+00
 Pressure            100      2  0.1000E-04  0.1000E-06  0.0000E+00
-----------------------------------------------------------

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

 --- 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
         --           --                --

 --- 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
         --           --                --

 --- 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 (0.243 s)


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

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

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

 Histogram of the number of cells per rank:

    minimum value =              16761
    maximum value =              16762

      1 : [      16761 ;      16762 ] =          4

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

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

    minimum value =              21699
    maximum value =              22863

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

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

 Histogram of the number of ghost cells per rank:

    minimum value =               4938
    maximum value =               6102

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

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

    minimum value =               1984
    maximum value =               2619

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

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

 Histogram of the number of interior faces per rank:

    minimum value =              33363
    maximum value =              34101

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

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

 Histogram of the number of boundary faces per rank:

    minimum value =               1114
    maximum value =               2357

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

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

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

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  3
    maximum value =                  3

      1 : [          3 ;          3 ] =          4

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

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

 Renumbering mesh:

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


 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =              19569
    maximum value =              21943

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

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =               9266
    maximum value =               9412

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

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

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

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

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

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

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 2 -->   0 %

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

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

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

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

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

 Computing geometric quantities (0.0501 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    0.22766E-02     446   0.94908E-01   0.12351E+01 
c  VelocityY    0.22766E-02     446   0.94908E-01   0.00000E+00 
c  VelocityZ    0.22766E-02     446   0.94908E-01   0.00000E+00 
c  Pressure     0.15989E-01    1004   0.72440E+00   0.97513E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6281          1.7259       -0.063105       -0.064919
v  Velocity[Y]                -0.73109          2.4957         0.23886         0.22739
v  Velocity[Z]                 -1.7389          1.6055        0.061891      0.00037971
v  ǁVelocityǁ                 0.014535          2.7313         0.39569         0.39818
v  Pressure                      2.444          718.93          469.08          388.02
v  turbulent_viscosity               0               0               0               0
v  CourantNb                         0               0               0               0
v  FourierNb                    5.8385          1248.2          55.507          30.486
v  total_pressure                5e+05      5.0072e+05      5.0047e+05      5.0039e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          5.8385          1248.2          55.507          30.486


 TIME FOR THE TIME STEP                1:        0.15273E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282688E+00
Free inlet               13           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 0.14649E+01
   Friction velocity        uet   :  0.23892E-01 0.12386E+01
   Friction velocity        uk    :  0.23892E-01 0.12386E+01
   Dimensionless distance   yplus :  0.32591E+00 0.48621E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4353
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.38981E-01     608   0.50809E+00   0.89000E-01 
c  VelocityY    0.38981E-01     608   0.50809E+00   0.00000E+00 
c  VelocityZ    0.38981E-01     608   0.50809E+00   0.00000E+00 
c  Pressure     0.28283E-01     962   0.36460E+00   0.97794E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5187           1.593       -0.074706       -0.067343
v  Velocity[Y]                -0.63911          2.4287          0.2496         0.23117
v  Velocity[Z]                 -1.5633          1.4403        0.091643     -0.00083745
v  ǁVelocityǁ                0.0033399           2.694         0.44397          0.4188
v  Pressure                     2.0778          473.44          377.41          310.04
v  turbulent_viscosity      6.2774e-05         0.10938       0.0077042       0.0069503
v  CourantNb                0.00033406          1252.2          81.586          62.248
v  FourierNb                    6.1159          1911.4          65.765          36.351
v  total_pressure                5e+05      5.0047e+05      5.0038e+05      5.0031e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.5614          2740.9          147.35          98.599


 TIME FOR THE TIME STEP                2:        0.19729E+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         0.341050620E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282692E+00
Free inlet               13           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 0.14608E+01
   Friction velocity        uet   :  0.17951E-01 0.11870E+01
   Friction velocity        uk    :  0.17951E-01 0.11870E+01
   Dimensionless distance   yplus :  0.13984E+00 0.49520E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4504
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.36707E-01     600   0.43243E+00   0.43300E-01 
c  VelocityY    0.36707E-01     600   0.43243E+00   0.00000E+00 
c  VelocityZ    0.36707E-01     600   0.43243E+00   0.00000E+00 
c  Pressure     0.30143E-01     911   0.16412E+00   0.58644E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5078          1.5675       -0.082526       -0.068044
v  Velocity[Y]                -0.59544          2.4826         0.25942         0.23305
v  Velocity[Z]                 -1.4732          1.4379         0.11164      -0.0010229
v  ǁVelocityǁ                0.0049298          2.7272         0.48855         0.44385
v  Pressure                     2.6738          847.22          668.82          547.86
v  turbulent_viscosity      0.00027611         0.10294       0.0096346       0.0084843
v  CourantNb                  0.025854          1215.1          93.134          66.406
v  FourierNb                     6.226          3126.7          68.907           37.99
v  total_pressure                5e+05      5.0085e+05      5.0067e+05      5.0055e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.6127          3175.3          162.04           104.4


 TIME FOR THE TIME STEP                3:        0.18527E+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         0.558858111E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282697E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.14483E+01
   Friction velocity        uet   :  0.16113E-01 0.10465E+01
   Friction velocity        uk    :  0.16113E-01 0.10465E+01
   Dimensionless distance   yplus :  0.14122E+00 0.49564E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4535
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.38440E-01     592   0.49672E+00   0.24180E-01 
c  VelocityY    0.38440E-01     592   0.49672E+00   0.00000E+00 
c  VelocityZ    0.38440E-01     592   0.49672E+00   0.00000E+00 
c  Pressure     0.36440E-01     872   0.10089E+00   0.48837E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5008           1.422       -0.085155       -0.068576
v  Velocity[Y]                -0.52819          2.4932          0.2664          0.2346
v  Velocity[Z]                 -1.4512          1.3592         0.11382     -0.00085856
v  ǁVelocityǁ                0.0017586          2.7523         0.51004           0.456
v  Pressure                     2.2067          1153.9          904.08          738.27
v  turbulent_viscosity      0.00017826         0.12154        0.010998       0.0095706
v  CourantNb                  0.047894          1211.6           103.6          71.022
v  FourierNb                    6.2937            2815          70.992          38.948
v  total_pressure                5e+05      5.0115e+05       5.009e+05      5.0074e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.5471          2826.1          174.59          109.97


 TIME FOR THE TIME STEP                4:        0.16035E+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         0.180126850E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282703E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.14679E+01
   Friction velocity        uet   :  0.11661E-01 0.93541E+00
   Friction velocity        uk    :  0.11661E-01 0.93541E+00
   Dimensionless distance   yplus :  0.12693E+00 0.49835E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4574
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.37050E-01     583   0.42404E+00   0.17295E-01 
c  VelocityY    0.37050E-01     583   0.42404E+00   0.00000E+00 
c  VelocityZ    0.37050E-01     583   0.42404E+00   0.00000E+00 
c  Pressure     0.40710E-01     843   0.71263E-01   0.41675E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4816          1.3875       -0.085241        -0.06916
v  Velocity[Y]                 -0.4954           2.583          0.2707         0.23612
v  Velocity[Z]                 -1.4586          1.3727         0.11408     -0.00083188
v  ǁVelocityǁ                0.0025402          2.8028         0.51784         0.46178
v  Pressure                     1.1679          1416.4          1103.8          898.34
v  turbulent_viscosity      0.00015981         0.12298        0.011653        0.010189
v  CourantNb                   0.15695          1183.5          108.59          73.176
v  FourierNb                    6.2746          2692.6          71.946          39.428
v  total_pressure                5e+05      5.0142e+05       5.011e+05       5.009e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.2074          2729.7          180.53           112.6


 TIME FOR THE TIME STEP                5:        0.17432E+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         0.364478277E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282713E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.15200E+01
   Friction velocity        uet   :  0.86480E-02 0.85378E+00
   Friction velocity        uk    :  0.86480E-02 0.85378E+00
   Dimensionless distance   yplus :  0.78469E-01 0.49428E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4577
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.39082E-01     575   0.49900E+00   0.10456E-01 
c  VelocityY    0.39082E-01     575   0.49900E+00   0.00000E+00 
c  VelocityZ    0.39082E-01     575   0.49900E+00   0.00000E+00 
c  Pressure     0.43702E-01     823   0.55094E-01   0.35869E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5079          1.3851        -0.08562       -0.069594
v  Velocity[Y]                -0.51423          2.6292          0.2744         0.23715
v  Velocity[Z]                 -1.4266          1.3504         0.11552      -0.0010185
v  ǁVelocityǁ                0.0015032          2.8771         0.52932         0.46972
v  Pressure                  -0.076391          1646.1          1279.6          1038.2
v  turbulent_viscosity      0.00011757          0.1237        0.011946        0.010562
v  CourantNb                   0.06768          1134.1           110.2          74.084
v  FourierNb                    6.2291          2735.7          72.333          39.655
v  total_pressure                5e+05      5.0165e+05      5.0128e+05      5.0104e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.5113          2794.6          182.53          113.74


 TIME FOR THE TIME STEP                6:        0.15501E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.102213054E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282729E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.15825E+01
   Friction velocity        uet   :  0.95003E-02 0.80943E+00
   Friction velocity        uk    :  0.95003E-02 0.80943E+00
   Dimensionless distance   yplus :  0.75945E-01 0.50219E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4547
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.37720E-01     573   0.42865E+00   0.52291E-02 
c  VelocityY    0.37720E-01     573   0.42865E+00   0.00000E+00 
c  VelocityZ    0.37720E-01     573   0.42865E+00   0.00000E+00 
c  Pressure     0.46290E-01     805   0.44447E-01   0.31898E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4861          1.4066       -0.085595       -0.070086
v  Velocity[Y]                -0.54219          2.7604          0.2776           0.238
v  Velocity[Z]                 -1.4232           1.388         0.11564      -0.0011014
v  ǁVelocityǁ                0.0029573          2.9179         0.53954         0.47821
v  Pressure                    -1.2518          1853.7          1439.6          1164.4
v  turbulent_viscosity      8.6242e-05         0.12722        0.012249        0.010906
v  CourantNb                    0.1829          1083.9          112.72          75.434
v  FourierNb                    6.2114          2805.4          72.774          39.903
v  total_pressure                5e+05      5.0185e+05      5.0144e+05      5.0116e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.2467            2872           185.5          115.34


 TIME FOR THE TIME STEP                7:        0.15625E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.515181982E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282728E+00
Free inlet               13           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 0.16493E+01
   Friction velocity        uet   :  0.18516E-02 0.78226E+00
   Friction velocity        uk    :  0.18516E-02 0.78226E+00
   Dimensionless distance   yplus :  0.28289E-01 0.50002E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4513
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.39408E-01     571   0.48377E+00   0.41584E-02 
c  VelocityY    0.39408E-01     571   0.48377E+00   0.00000E+00 
c  VelocityZ    0.39408E-01     571   0.48377E+00   0.00000E+00 
c  Pressure     0.47767E-01     790   0.36895E-01   0.28328E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5343          1.3929        -0.08626       -0.070555
v  Velocity[Y]                -0.58368          2.8271         0.27935          0.2384
v  Velocity[Z]                 -1.4162          1.4127         0.11509      -0.0012196
v  ǁVelocityǁ                0.0021169          2.9855         0.54661         0.48652
v  Pressure                    -2.7776          2044.4          1587.2          1279.9
v  turbulent_viscosity      7.3448e-05         0.13003        0.012449        0.011167
v  CourantNb                    0.1984          1017.3           114.9          76.808
v  FourierNb                    6.2133          2849.2          73.044          40.075
v  total_pressure                5e+05      5.0204e+05      5.0159e+05      5.0128e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.6301          2922.9          187.94          116.88


 TIME FOR THE TIME STEP                8:        0.16922E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.978718116E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282756E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.16979E+01
   Friction velocity        uet   :  0.11656E-01 0.77145E+00
   Friction velocity        uk    :  0.11656E-01 0.77145E+00
   Dimensionless distance   yplus :  0.13031E+00 0.50465E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4481
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.38541E-01     571   0.43539E+00   0.35405E-02 
c  VelocityY    0.38541E-01     571   0.43539E+00   0.00000E+00 
c  VelocityZ    0.38541E-01     571   0.43539E+00   0.00000E+00 
c  Pressure     0.49089E-01     782   0.30613E-01   0.25670E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.508          1.4087       -0.086054       -0.071004
v  Velocity[Y]                -0.61748          2.9078         0.28126         0.23865
v  Velocity[Z]                 -1.4578          1.4166         0.11487      -0.0012791
v  ǁVelocityǁ                0.0015576          3.1614         0.55528         0.49488
v  Pressure                    -5.8584          2223.6          1726.2          1387.9
v  turbulent_viscosity       7.526e-05         0.13087        0.012698        0.011472
v  CourantNb                  0.055115          975.72          116.22          78.028
v  FourierNb                    6.2186            2910          73.399          40.285
v  total_pressure           4.9999e+05      5.0222e+05      5.0173e+05      5.0139e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.9154          2989.1          189.62          118.31


 TIME FOR THE TIME STEP                9:        0.15489E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.118424537E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282756E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18428E+01
   Friction velocity        uet   :  0.16304E-01 0.76756E+00
   Friction velocity        uk    :  0.16304E-01 0.76756E+00
   Dimensionless distance   yplus :  0.14682E+00 0.50792E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4452
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.40060E-01     568   0.48364E+00   0.28101E-02 
c  VelocityY    0.40060E-01     568   0.48364E+00   0.00000E+00 
c  VelocityZ    0.40060E-01     568   0.48364E+00   0.00000E+00 
c  Pressure     0.49763E-01     770   0.26034E-01   0.23269E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5917          1.4091       -0.085773       -0.071517
v  Velocity[Y]                 -0.6942          2.8954         0.28227         0.23874
v  Velocity[Z]                 -1.4876          1.6053         0.11513       -0.001106
v  ǁVelocityǁ                0.0028933          3.1735         0.56267         0.50325
v  Pressure                    -9.0117          2392.7          1857.6          1489.2
v  turbulent_viscosity      7.7935e-05         0.13407         0.01295        0.011735
v  CourantNb                   0.21845           882.4          118.02          79.322
v  FourierNb                    6.2138          2954.3          73.783          40.481
v  total_pressure           4.9999e+05      5.0239e+05      5.0186e+05      5.0149e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.8577          3038.7           191.8           119.8


 TIME FOR THE TIME STEP               10:        0.16406E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.106788620E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282755E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.18180E+01
   Friction velocity        uet   :  0.16117E-01 0.77333E+00
   Friction velocity        uk    :  0.16117E-01 0.77333E+00
   Dimensionless distance   yplus :  0.16778E+00 0.51062E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4414
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.39448E-01     568   0.44466E+00   0.23697E-02 
c  VelocityY    0.39448E-01     568   0.44466E+00   0.00000E+00 
c  VelocityZ    0.39448E-01     568   0.44466E+00   0.00000E+00 
c  Pressure     0.50516E-01     768   0.22914E-01   0.21426E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6146          1.4839       -0.085306       -0.071949
v  Velocity[Y]                -0.73534          3.0833         0.28298         0.23848
v  Velocity[Z]                 -1.5668          1.4294         0.11512     -0.00090395
v  ǁVelocityǁ                0.0040412          3.3494         0.56949         0.51108
v  Pressure                    -11.989          2553.9          1983.3          1585.4
v  turbulent_viscosity      7.8424e-05         0.13492        0.013231        0.012049
v  CourantNb                   0.20211          915.06          119.49           80.56
v  FourierNb                    6.2152            2999           74.16          40.707
v  total_pressure           4.9999e+05      5.0255e+05      5.0198e+05      5.0159e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.2242          3081.8          193.65          121.27


 TIME FOR THE TIME STEP               11:        0.16393E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.276407100E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282756E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.19084E+01
   Friction velocity        uet   :  0.18014E-01 0.77230E+00
   Friction velocity        uk    :  0.18014E-01 0.77230E+00
   Dimensionless distance   yplus :  0.14746E+00 0.51179E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4350
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.41187E-01     568   0.49473E+00   0.20744E-02 
c  VelocityY    0.41187E-01     568   0.49473E+00   0.00000E+00 
c  VelocityZ    0.41187E-01     568   0.49473E+00   0.00000E+00 
c  Pressure     0.51072E-01     762   0.20526E-01   0.19803E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6613          1.4516       -0.084546       -0.072466
v  Velocity[Y]                -0.77068           3.225         0.28372          0.2384
v  Velocity[Z]                 -1.6193          1.6397         0.11507     -0.00072608
v  ǁVelocityǁ                0.0041435          3.4733         0.57594          0.5191
v  Pressure                    -15.042          2707.1          2102.6          1675.9
v  turbulent_viscosity      7.7167e-05         0.13882        0.013515        0.012352
v  CourantNb                    0.1481          959.34          120.87          81.753
v  FourierNb                    6.2322          3021.7           74.59          40.942
v  total_pressure           4.9998e+05      5.0271e+05       5.021e+05      5.0168e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.3464          3107.9          195.46          122.69


 TIME FOR THE TIME STEP               12:        0.16636E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.185995267E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282758E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.19983E+01
   Friction velocity        uet   :  0.20580E-01 0.78115E+00
   Friction velocity        uk    :  0.20580E-01 0.78115E+00
   Dimensionless distance   yplus :  0.16846E+00 0.51613E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4287
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.41040E-01     570   0.47476E+00   0.18960E-02 
c  VelocityY    0.41040E-01     570   0.47476E+00   0.00000E+00 
c  VelocityZ    0.41040E-01     570   0.47476E+00   0.00000E+00 
c  Pressure     0.51776E-01     752   0.18444E-01   0.18514E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5843          1.5037       -0.083863        -0.07287
v  Velocity[Y]                -0.83496          3.2726         0.28436          0.2382
v  Velocity[Z]                 -1.7026          1.4444         0.11518     -0.00063285
v  ǁVelocityǁ                0.0029764           3.501         0.58205         0.52672
v  Pressure                    -19.315          2853.1          2216.4          1761.5
v  turbulent_viscosity      7.4127e-05         0.14155        0.013786        0.012661
v  CourantNb                   0.12677           999.9          122.14          82.917
v  FourierNb                    6.2683          3063.4          74.959          41.168
v  total_pressure           4.9998e+05      5.0285e+05      5.0222e+05      5.0176e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.9857          3151.2           197.1          124.08


 TIME FOR THE TIME STEP               13:        0.15260E+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        -0.649737798E-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 0.20304E+01
   Friction velocity        uet   :  0.16519E-01 0.78273E+00
   Friction velocity        uk    :  0.16519E-01 0.78273E+00
   Dimensionless distance   yplus :  0.18391E+00 0.51914E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4213
   Total number of wall faces                   :       6590
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.42596E-01     570   0.51807E+00   0.18269E-02 
c  VelocityY    0.42596E-01     570   0.51807E+00   0.00000E+00 
c  VelocityZ    0.42596E-01     570   0.51807E+00   0.00000E+00 
c  Pressure     0.52347E-01     738   0.16961E-01   0.17354E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5936          1.4928       -0.082931       -0.073212
v  Velocity[Y]                -0.87849           3.352         0.28488         0.23803
v  Velocity[Z]                 -1.7748          1.4021         0.11512      -0.0006038
v  ǁVelocityǁ                0.0046583          3.5861         0.58796         0.53463
v  Pressure                    -25.671          2993.2          2325.3          1842.8
v  turbulent_viscosity      6.4786e-05         0.16942        0.014056        0.012966
v  CourantNb                  0.082014          1037.4          123.39          84.051
v  FourierNb                    6.2801          3076.1          75.336          41.397
v  total_pressure           4.9997e+05      5.0299e+05      5.0233e+05      5.0184e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.2385          3161.4          198.73          125.45


 TIME FOR THE TIME STEP               14:        0.15794E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.147793187E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282808E+00
Free inlet               13           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 0.20853E+01
   Friction velocity        uet   :  0.15875E-01 0.78944E+00
   Friction velocity        uk    :  0.15875E-01 0.78944E+00
   Dimensionless distance   yplus :  0.17450E+00 0.51875E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4130
   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    0.42200E-01     573   0.48626E+00   0.17704E-02 
c  VelocityY    0.42200E-01     573   0.48626E+00   0.00000E+00 
c  VelocityZ    0.42200E-01     573   0.48626E+00   0.00000E+00 
c  Pressure     0.53405E-01     735   0.15648E-01   0.16517E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5964          1.5406       -0.082264       -0.073684
v  Velocity[Y]                -0.92928          3.3385         0.28541         0.23788
v  Velocity[Z]                 -1.8596          1.5309         0.11515     -0.00055962
v  ǁVelocityǁ                0.0037106          3.5977         0.59367          0.5421
v  Pressure                    -31.936          3128.5          2430.7          1920.8
v  turbulent_viscosity      6.4281e-05         0.16207        0.014325        0.013276
v  CourantNb                   0.10582          1081.7          124.54           85.17
v  FourierNb                    6.2707          3149.4          75.697          41.609
v  total_pressure           4.9997e+05      5.0313e+05      5.0243e+05      5.0192e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           7.138          3185.3          200.24          126.78


 TIME FOR THE TIME STEP               15:        0.15590E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.136606694E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282806E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.21258E+01
   Friction velocity        uet   :  0.14191E-01 0.80322E+00
   Friction velocity        uk    :  0.14191E-01 0.80322E+00
   Dimensionless distance   yplus :  0.17919E+00 0.52318E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4067
   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    0.43502E-01     576   0.52161E+00   0.18404E-02 
c  VelocityY    0.43502E-01     576   0.52161E+00   0.00000E+00 
c  VelocityZ    0.43502E-01     576   0.52161E+00   0.00000E+00 
c  Pressure     0.54278E-01     734   0.14625E-01   0.15696E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6764          1.6137       -0.081313       -0.073947
v  Velocity[Y]                -0.93679          3.4073         0.28584         0.23784
v  Velocity[Z]                 -1.8176          1.3425         0.11526     -0.00044425
v  ǁVelocityǁ                0.0026037          3.6583          0.5989         0.54968
v  Pressure                    -37.196          3258.3          2531.6            1995
v  turbulent_viscosity      6.2756e-05         0.16979        0.014581        0.013549
v  CourantNb                  0.082591          1173.2          125.71          86.266
v  FourierNb                    6.2441            3239          76.075           41.82
v  total_pressure           4.9996e+05      5.0326e+05      5.0253e+05      5.0199e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.7544          3265.7          201.79          128.09


 TIME FOR THE TIME STEP               16:        0.15512E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.184156609E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282806E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.21666E+01
   Friction velocity        uet   :  0.16232E-01 0.81415E+00
   Friction velocity        uk    :  0.16232E-01 0.81415E+00
   Dimensionless distance   yplus :  0.16664E+00 0.53002E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       4011
   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    0.43617E-01     578   0.50441E+00   0.16265E-02 
c  VelocityY    0.43617E-01     578   0.50441E+00   0.00000E+00 
c  VelocityZ    0.43617E-01     578   0.50441E+00   0.00000E+00 
c  Pressure     0.55057E-01     732   0.13656E-01   0.14944E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.835          1.6911       -0.080509        -0.07431
v  Velocity[Y]                 -1.0031           3.454          0.2866         0.23788
v  Velocity[Z]                 -1.9979           1.343          0.1153     -0.00045969
v  ǁVelocityǁ                0.0018339          3.6561         0.60464         0.55698
v  Pressure                    -43.431          3383.7          2628.9            2066
v  turbulent_viscosity      6.4631e-05         0.17852        0.014862        0.013865
v  CourantNb                  0.092066          1244.9          126.73          87.332
v  FourierNb                    6.2201          3275.6          76.458          42.057
v  total_pressure           4.9996e+05      5.0338e+05      5.0263e+05      5.0207e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          7.2469            3303          203.19          129.39


 TIME FOR THE TIME STEP               17:        0.15048E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.278080089E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282806E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.21985E+01
   Friction velocity        uet   :  0.15934E-01 0.81858E+00
   Friction velocity        uk    :  0.15934E-01 0.81858E+00
   Dimensionless distance   yplus :  0.14672E+00 0.54065E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3951
   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    0.44953E-01     581   0.53823E+00   0.15831E-02 
c  VelocityY    0.44953E-01     581   0.53823E+00   0.00000E+00 
c  VelocityZ    0.44953E-01     581   0.53823E+00   0.00000E+00 
c  Pressure     0.56314E-01     730   0.12952E-01   0.14385E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0867          1.7646       -0.079505       -0.074488
v  Velocity[Y]                 -1.0358           3.489         0.28716         0.23795
v  Velocity[Z]                 -1.9402          1.3997         0.11534     -0.00044916
v  ǁVelocityǁ                0.0026851          3.6912         0.60981         0.56456
v  Pressure                    -49.288          3504.9          2722.9          2134.1
v  turbulent_viscosity      6.4295e-05         0.17779        0.015139        0.014137
v  CourantNb                  0.067719            1340          127.91          88.406
v  FourierNb                    6.2314          3338.5          76.868           42.29
v  total_pressure           4.9995e+05       5.035e+05      5.0272e+05      5.0213e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           7.449          3365.6          204.78           130.7


 TIME FOR THE TIME STEP               18:        0.15402E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.806084198E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282808E+00
Free inlet               13           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 0.22451E+01
   Friction velocity        uet   :  0.19798E-01 0.81854E+00
   Friction velocity        uk    :  0.19798E-01 0.81854E+00
   Dimensionless distance   yplus :  0.13060E+00 0.54634E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3887
   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    0.45231E-01     584   0.52295E+00   0.15077E-02 
c  VelocityY    0.45231E-01     584   0.52295E+00   0.00000E+00 
c  VelocityZ    0.45231E-01     584   0.52295E+00   0.00000E+00 
c  Pressure     0.57707E-01     725   0.12253E-01   0.13907E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1446          1.8531       -0.078649       -0.074747
v  Velocity[Y]                 -1.0869          3.5946         0.28791         0.23812
v  Velocity[Z]                 -2.1519          1.4427         0.11532     -0.00046859
v  ǁVelocityǁ                0.0036039          3.8092         0.61514         0.57181
v  Pressure                    -60.306          3621.8          2813.4          2199.1
v  turbulent_viscosity      6.4783e-05         0.20334        0.015425        0.014441
v  CourantNb                   0.15541          1426.6          128.91          89.469
v  FourierNb                    6.3095          3319.7          77.266          42.517
v  total_pressure           4.9994e+05      5.0362e+05      5.0281e+05       5.022e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.7158          3348.2          206.17          131.99


 TIME FOR THE TIME STEP               19:        0.15207E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.431551872E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282808E+00
Free inlet               13           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 0.23154E+01
   Friction velocity        uet   :  0.20090E-01 0.83051E+00
   Friction velocity        uk    :  0.20090E-01 0.83051E+00
   Dimensionless distance   yplus :  0.14089E+00 0.55835E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3831
   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    0.46765E-01     587   0.55490E+00   0.15487E-02 
c  VelocityY    0.46765E-01     587   0.55490E+00   0.00000E+00 
c  VelocityZ    0.46765E-01     587   0.55490E+00   0.00000E+00 
c  Pressure     0.59639E-01     721   0.11662E-01   0.13584E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2666          1.9377       -0.077746       -0.075081
v  Velocity[Y]                 -1.1319          3.6929         0.28861         0.23824
v  Velocity[Z]                 -2.0719          1.5241         0.11512      -0.0004399
v  ǁVelocityǁ                0.0040787          4.1005         0.61995         0.57863
v  Pressure                    -70.395          3736.1          2901.6            2262
v  turbulent_viscosity      6.5903e-05         0.20586        0.015706        0.014718
v  CourantNb                  0.013429          1525.1          130.02          90.548
v  FourierNb                    6.4176          3363.9          77.666          42.754
v  total_pressure           4.9993e+05      5.0374e+05       5.029e+05      5.0226e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6.8485            3391          207.69           133.3


 TIME FOR THE TIME STEP               20:        0.16905E+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        -0.390513655E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282810E+00
Free inlet               13           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 0.23408E+01
   Friction velocity        uet   :  0.11514E-01 0.82999E+00
   Friction velocity        uk    :  0.11514E-01 0.82999E+00
   Dimensionless distance   yplus :  0.15605E+00 0.56269E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3767
   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    0.47034E-01     590   0.54437E+00   0.16724E-02 
c  VelocityY    0.47034E-01     590   0.54437E+00   0.00000E+00 
c  VelocityZ    0.47034E-01     590   0.54437E+00   0.00000E+00 
c  Pressure     0.61333E-01     710   0.11152E-01   0.13231E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3594          2.0775        -0.07723       -0.075516
v  Velocity[Y]                 -1.1705          3.6622         0.28941         0.23862
v  Velocity[Z]                 -2.2771          1.5712         0.11501     -0.00051625
v  ǁVelocityǁ                0.0055166          4.3051         0.62527         0.58517
v  Pressure                    -79.825          3847.8          2987.7          2323.2
v  turbulent_viscosity      6.6849e-05         0.22945        0.016007           0.015
v  CourantNb                   0.09578            1625          131.03          91.562
v  FourierNb                    6.4376          3317.8          78.086          42.977
v  total_pressure           4.9992e+05      5.0385e+05      5.0299e+05      5.0232e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.1842            3464          209.12          134.54


 TIME FOR THE TIME STEP               21:        0.16750E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.200232691E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282812E+00
Free inlet               13           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 0.23599E+01
   Friction velocity        uet   :  0.16152E-01 0.83652E+00
   Friction velocity        uk    :  0.16152E-01 0.83652E+00
   Dimensionless distance   yplus :  0.15443E+00 0.56592E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3722
   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    0.48939E-01     593   0.57345E+00   0.16196E-02 
c  VelocityY    0.48939E-01     593   0.57345E+00   0.00000E+00 
c  VelocityZ    0.48939E-01     593   0.57345E+00   0.00000E+00 
c  Pressure     0.63859E-01     702   0.10877E-01   0.13076E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7366          2.1078        -0.07666       -0.075757
v  Velocity[Y]                 -1.1925          3.7589         0.29026         0.23894
v  Velocity[Z]                 -2.2783          1.6587         0.11492     -0.00051795
v  ǁVelocityǁ                0.0052699          4.2453         0.63029         0.59169
v  Pressure                    -88.069          3957.5          3072.3          2382.9
v  turbulent_viscosity      6.6581e-05         0.23706        0.016315        0.015278
v  CourantNb                   0.12483          1727.7          132.16          92.579
v  FourierNb                    6.4314          3318.8          78.534           43.23
v  total_pressure           4.9991e+05      5.0396e+05      5.0307e+05      5.0238e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.6805          3567.4          210.69          135.81


 TIME FOR THE TIME STEP               22:        0.16884E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.160058754E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282896E+00
Free inlet               13           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 0.24063E+01
   Friction velocity        uet   :  0.10005E-01 0.84624E+00
   Friction velocity        uk    :  0.10005E-01 0.84624E+00
   Dimensionless distance   yplus :  0.12963E+00 0.57379E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3685
   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    0.51099E-01     594   0.61388E+00   0.17200E-02 
c  VelocityY    0.51099E-01     594   0.61388E+00   0.00000E+00 
c  VelocityZ    0.51099E-01     594   0.61388E+00   0.00000E+00 
c  Pressure     0.66015E-01     699   0.10411E-01   0.12842E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7629          2.2423       -0.076186        -0.07608
v  Velocity[Y]                 -1.2415          4.0142          0.2912         0.23941
v  Velocity[Z]                 -2.4416          1.7193         0.11494     -0.00059011
v  ǁVelocityǁ                0.0056208          4.6484         0.63553         0.59812
v  Pressure                     -100.6          4065.3          3155.4          2441.2
v  turbulent_viscosity      6.8138e-05         0.24238        0.016624        0.015563
v  CourantNb                  0.056902          1836.9          133.24          93.562
v  FourierNb                    6.4443          3294.1          78.979          43.466
v  total_pressure            4.999e+05      5.0407e+05      5.0316e+05      5.0244e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.4959          3656.9          212.22          137.03


 TIME FOR THE TIME STEP               23:        0.16790E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.800904559E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282903E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.24337E+01
   Friction velocity        uet   :  0.76028E-02 0.84860E+00
   Friction velocity        uk    :  0.76028E-02 0.84860E+00
   Dimensionless distance   yplus :  0.58858E-01 0.57840E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3649
   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    0.54626E-01     597   0.65581E+00   0.16019E-02 
c  VelocityY    0.54626E-01     597   0.65581E+00   0.00000E+00 
c  VelocityZ    0.54626E-01     597   0.65581E+00   0.00000E+00 
c  Pressure     0.68799E-01     699   0.10171E-01   0.12738E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9867          2.2933       -0.075406        -0.07619
v  Velocity[Y]                 -1.2455           4.239         0.29259         0.23996
v  Velocity[Z]                  -2.593          1.7946          0.1149     -0.00053153
v  ǁVelocityǁ                 0.005154          4.6578         0.64059           0.604
v  Pressure                    -115.21            4174          3236.7          2497.9
v  turbulent_viscosity       6.579e-05           0.265        0.016941         0.01583
v  CourantNb                   0.03091          1960.7           134.4          94.574
v  FourierNb                     6.457          3274.5          79.428          43.699
v  total_pressure           4.9988e+05      5.0417e+05      5.0324e+05       5.025e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.2934          3764.2          213.83          138.27


 TIME FOR THE TIME STEP               24:        0.17072E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.190298657E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282901E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.25006E+01
   Friction velocity        uet   :  0.86854E-02 0.85356E+00
   Friction velocity        uk    :  0.86854E-02 0.85356E+00
   Dimensionless distance   yplus :  0.11927E+00 0.58964E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3616
   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    0.54230E-01     601   0.63488E+00   0.18120E-02 
c  VelocityY    0.54230E-01     601   0.63488E+00   0.00000E+00 
c  VelocityZ    0.54230E-01     601   0.63488E+00   0.00000E+00 
c  Pressure     0.71334E-01     697   0.99142E-02   0.12572E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9982          2.4079        -0.07509       -0.076353
v  Velocity[Y]                 -1.3503          4.4339         0.29356          0.2406
v  Velocity[Z]                 -2.6992          1.8711         0.11488     -0.00059361
v  ǁVelocityǁ                0.0057237          5.0475          0.6457         0.61025
v  Pressure                    -131.43          4283.1          3316.5          2553.4
v  turbulent_viscosity       6.796e-05           0.272        0.017267        0.016119
v  CourantNb                    0.2225            2078          135.57          95.543
v  FourierNb                    6.5249          3309.9          79.896          43.952
v  total_pressure           4.9987e+05      5.0428e+05      5.0332e+05      5.0255e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.5242          3854.2          215.47          139.49


 TIME FOR THE TIME STEP               25:        0.15477E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.328819514E-16
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 0.24592E+01
   Friction velocity        uet   :  0.12093E-01 0.86017E+00
   Friction velocity        uk    :  0.12093E-01 0.86017E+00
   Dimensionless distance   yplus :  0.15039E+00 0.59177E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3585
   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    0.57222E-01     607   0.66781E+00   0.17798E-02 
c  VelocityY    0.57222E-01     607   0.66781E+00   0.00000E+00 
c  VelocityZ    0.57222E-01     607   0.66781E+00   0.00000E+00 
c  Pressure     0.74638E-01     696   0.97415E-02   0.12540E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.2502          2.4858       -0.074724       -0.076489
v  Velocity[Y]                 -1.3642          4.8594           0.295         0.24136
v  Velocity[Z]                 -2.8328          2.1287         0.11461     -0.00065983
v  ǁVelocityǁ                 0.005525          5.2824         0.65063         0.61586
v  Pressure                    -147.11          4391.3          3395.4          2607.7
v  turbulent_viscosity      6.4896e-05         0.29208        0.017598        0.016382
v  CourantNb                   0.12243          2209.2          136.77          96.569
v  FourierNb                    6.6009          3320.8          80.384          44.204
v  total_pressure           4.9985e+05      5.0439e+05       5.034e+05      5.0261e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.132            4009          217.15          140.77


 TIME FOR THE TIME STEP               26:        0.15668E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.444697591E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282906E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.00000E+00 0.25150E+01
   Friction velocity        uet   :  0.13370E-01 0.86895E+00
   Friction velocity        uk    :  0.13370E-01 0.86895E+00
   Dimensionless distance   yplus :  0.15021E+00 0.60149E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3561
   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    0.60020E-01     609   0.70366E+00   0.20762E-02 
c  VelocityY    0.60020E-01     609   0.70366E+00   0.00000E+00 
c  VelocityZ    0.60020E-01     609   0.70366E+00   0.00000E+00 
c  Pressure     0.77525E-01     696   0.94817E-02   0.12428E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.2895          2.6173       -0.074552       -0.076617
v  Velocity[Y]                 -1.4272          4.8435         0.29634         0.24215
v  Velocity[Z]                 -3.0513          2.1802         0.11431     -0.00077539
v  ǁVelocityǁ                0.0059571          5.6125          0.6557         0.62115
v  Pressure                    -162.65          4499.4          3474.5          2662.2
v  turbulent_viscosity      6.4622e-05         0.29445        0.017929        0.016662
v  CourantNb                   0.12993          2337.9          137.97          97.525
v  FourierNb                    6.6673          3376.8          80.858          44.454
v  total_pressure           4.9984e+05       5.045e+05      5.0347e+05      5.0266e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           10.54          4129.7          218.83          141.98


 TIME FOR THE TIME STEP               27:        0.17138E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.229506356E-16
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 0.25208E+01
   Friction velocity        uet   :  0.16007E-01 0.88954E+00
   Friction velocity        uk    :  0.16007E-01 0.88954E+00
   Dimensionless distance   yplus :  0.15745E+00 0.62039E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3540
   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    0.68072E-01     615   0.75934E+00   0.20558E-02 
c  VelocityY    0.68072E-01     615   0.75934E+00   0.00000E+00 
c  VelocityZ    0.68072E-01     615   0.75934E+00   0.00000E+00 
c  Pressure     0.81098E-01     691   0.93952E-02   0.12405E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.5217          2.6701       -0.074357       -0.076707
v  Velocity[Y]                 -1.4376          5.2536         0.29784         0.24285
v  Velocity[Z]                 -3.0267          2.2489         0.11411     -0.00077188
v  ǁVelocityǁ                0.0057054          5.4646         0.66052         0.62617
v  Pressure                    -177.41          4606.6          3552.8          2715.7
v  turbulent_viscosity      6.1068e-05          0.3264        0.018264        0.016887
v  CourantNb                   0.32561          2484.8          139.28          98.507
v  FourierNb                    6.7263            3448          81.365          44.689
v  total_pressure           4.9982e+05      5.0461e+05      5.0355e+05      5.0272e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.047          4359.6          220.65           143.2


 TIME FOR THE TIME STEP               28:        0.15512E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.170827024E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282908E+00
Free inlet               13           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 0.26071E+01
   Friction velocity        uet   :  0.17826E-01 0.90439E+00
   Friction velocity        uk    :  0.17826E-01 0.90439E+00
   Dimensionless distance   yplus :  0.15542E+00 0.61834E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3513
   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    0.64255E-01     624   0.71704E+00   0.23742E-02 
c  VelocityY    0.64255E-01     624   0.71704E+00   0.00000E+00 
c  VelocityZ    0.64255E-01     624   0.71704E+00   0.00000E+00 
c  Pressure     0.84375E-01     690   0.92122E-02   0.12312E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.6254          2.8264       -0.074555       -0.076997
v  Velocity[Y]                  -1.532          5.5742         0.29932         0.24396
v  Velocity[Z]                 -3.1081          2.3532         0.11378     -0.00084887
v  ǁVelocityǁ                0.0057638          6.0001         0.66579         0.63199
v  Pressure                    -191.62          4712.8          3630.4          2768.7
v  turbulent_viscosity      6.2212e-05         0.32715        0.018609        0.017154
v  CourantNb                  0.067721          2622.4          140.58          99.469
v  FourierNb                    6.7875          3500.5          81.843          44.939
v  total_pressure           4.9981e+05      5.0471e+05      5.0363e+05      5.0277e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.8008          4467.2          222.42          144.41


 TIME FOR THE TIME STEP               29:        0.17214E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.418744766E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282909E+00
Free inlet               13           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 0.27133E+01
   Friction velocity        uet   :  0.17349E-01 0.91974E+00
   Friction velocity        uk    :  0.17349E-01 0.91974E+00
   Dimensionless distance   yplus :  0.15416E+00 0.64737E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3486
   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    0.69945E-01     637   0.76812E+00   0.22880E-02 
c  VelocityY    0.69945E-01     637   0.76812E+00   0.00000E+00 
c  VelocityZ    0.69945E-01     637   0.76812E+00   0.00000E+00 
c  Pressure     0.88376E-01     681   0.91554E-02   0.12302E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.8787          2.8868       -0.074518       -0.077076
v  Velocity[Y]                 -1.5303          5.8169         0.30118         0.24487
v  Velocity[Z]                 -3.3044          2.4028         0.11344     -0.00099482
v  ǁVelocityǁ                 0.005207          6.2647         0.67077         0.63649
v  Pressure                    -208.09          4855.1          3709.3          2822.6
v  turbulent_viscosity      5.9866e-05         0.35054        0.018966         0.01741
v  CourantNb                  0.028611          2779.9          141.94          100.53
v  FourierNb                    6.8378          3590.6          82.367          45.202
v  total_pressure           4.9979e+05      5.0486e+05      5.0371e+05      5.0282e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.033          4583.1          224.31          145.74


 TIME FOR THE TIME STEP               30:        0.17285E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.145226876E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282917E+00
Free inlet               13           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 0.29086E+01
   Friction velocity        uet   :  0.16879E-01 0.93465E+00
   Friction velocity        uk    :  0.16879E-01 0.93465E+00
   Dimensionless distance   yplus :  0.14720E+00 0.66948E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3462
   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    0.78163E-01     639   0.82263E+00   0.31640E-02 
c  VelocityY    0.78163E-01     639   0.82263E+00   0.00000E+00 
c  VelocityZ    0.78163E-01     639   0.82263E+00   0.00000E+00 
c  Pressure     0.92213E-01     678   0.90405E-02   0.12241E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -4.0022          3.0479       -0.074929       -0.077414
v  Velocity[Y]                 -1.5988           5.978         0.30249         0.24602
v  Velocity[Z]                 -3.6036          2.5673         0.11318      -0.0011146
v  ǁVelocityǁ                0.0053968          6.6526         0.67584          0.6416
v  Pressure                    -228.04          5010.1          3788.3          2876.5
v  turbulent_viscosity      5.9845e-05         0.35346        0.019356          0.0177
v  CourantNb                  0.012442          2936.1          143.36          101.51
v  FourierNb                     6.918            3659          82.918          45.487
v  total_pressure           4.9977e+05      5.0501e+05      5.0379e+05      5.0288e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.206          4601.6          226.27             147


 TIME FOR THE TIME STEP               31:        0.17694E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.653770304E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282915E+00
Free inlet               13           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 0.30616E+01
   Friction velocity        uet   :  0.11356E-01 0.95688E+00
   Friction velocity        uk    :  0.11356E-01 0.95688E+00
   Dimensionless distance   yplus :  0.10742E+00 0.69154E+01
   ------------------------------------------------------
   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          3 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.92658E-01     657   0.86938E+00   0.33735E-02 
c  VelocityY    0.92658E-01     657   0.86938E+00   0.00000E+00 
c  VelocityZ    0.92658E-01     657   0.86938E+00   0.00000E+00 
c  Pressure     0.96837E-01     675   0.90051E-02   0.12263E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -4.2839          3.1268       -0.074851       -0.077645
v  Velocity[Y]                  -1.579          5.8326         0.30502         0.24731
v  Velocity[Z]                  -3.697           2.667         0.11276      -0.0012478
v  ǁVelocityǁ                0.0061467          6.4716         0.68142         0.64639
v  Pressure                    -245.07          5172.2            3869          2931.6
v  turbulent_viscosity      5.7671e-05         0.39211        0.019696        0.017915
v  CourantNb                 0.0040939          3103.9          144.76          102.55
v  FourierNb                    6.9526          3747.4          83.428          45.724
v  total_pressure           4.9975e+05      5.0517e+05      5.0387e+05      5.0293e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.7776          4697.9          228.18          148.27


 TIME FOR THE TIME STEP               32:        0.17760E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.451539297E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282921E+00
Free inlet               13           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 0.32431E+01
   Friction velocity        uet   :  0.16809E-01 0.97774E+00
   Friction velocity        uk    :  0.16809E-01 0.97774E+00
   Dimensionless distance   yplus :  0.12075E+00 0.72218E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3419
   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    0.88053E-01     672   0.85072E+00   0.45315E-02 
c  VelocityY    0.88053E-01     672   0.85072E+00   0.00000E+00 
c  VelocityZ    0.88053E-01     672   0.85072E+00   0.00000E+00 
c  Pressure     0.10136E+00     675   0.88476E-02   0.12237E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -4.4338          3.2826       -0.075339        -0.07812
v  Velocity[Y]                 -1.6701          6.5196         0.30633         0.24846
v  Velocity[Z]                 -3.7541          2.7551         0.11238      -0.0014335
v  ǁVelocityǁ                0.0062341          7.1969         0.68674         0.65143
v  Pressure                    -259.48          5339.6          3950.6          2987.7
v  turbulent_viscosity      5.7396e-05         0.39406        0.020132        0.018244
v  CourantNb                   0.13505          3497.7           146.4          103.65
v  FourierNb                    6.9979          3859.5          84.044          46.051
v  total_pressure           4.9974e+05      5.0534e+05      5.0395e+05      5.0299e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.4271          4889.2          230.44          149.71


 TIME FOR THE TIME STEP               33:        0.17059E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.194475588E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273282918E+00
Free inlet               13           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 0.33734E+01
   Friction velocity        uet   :  0.17363E-01 0.10014E+01
   Friction velocity        uk    :  0.17363E-01 0.10014E+01
   Dimensionless distance   yplus :  0.17062E+00 0.76578E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3397
   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    0.89234E-01     717   0.84366E+00   0.39567E-02 
c  VelocityY    0.89234E-01     717   0.84366E+00   0.00000E+00 
c  VelocityZ    0.89234E-01     717   0.84366E+00   0.00000E+00 
c  Pressure     0.10611E+00     666   0.88459E-02   0.12218E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -4.7713          3.3918       -0.075806       -0.078618
v  Velocity[Y]                 -1.7937          6.3651         0.30893         0.24983
v  Velocity[Z]                 -3.9735          2.8335         0.11171      -0.0014637
v  ǁVelocityǁ                0.0054438          7.0597         0.69222         0.65565
v  Pressure                    -269.02          5516.2            4036          3046.8
v  turbulent_viscosity      5.5904e-05         0.42286        0.020526        0.018496
v  CourantNb                   0.10299          3673.2          147.95           104.8
v  FourierNb                    7.0407          3962.2          84.648          46.336
v  total_pressure           4.9973e+05      5.0552e+05      5.0404e+05      5.0305e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.9097          5150.8           232.6          151.14


 TIME FOR THE TIME STEP               34:        0.16612E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.588996668E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283075E+00
Free inlet               13           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 0.35989E+01
   Friction velocity        uet   :  0.17677E-01 0.10180E+01
   Friction velocity        uk    :  0.17677E-01 0.10180E+01
   Dimensionless distance   yplus :  0.16409E+00 0.79830E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3389
   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    0.11809E+00     720   0.91538E+00   0.57133E-02 
c  VelocityY    0.11809E+00     720   0.91538E+00   0.00000E+00 
c  VelocityZ    0.11809E+00     720   0.91538E+00   0.00000E+00 
c  Pressure     0.11075E+00     666   0.87489E-02   0.12164E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -5.0629          3.5458        -0.07684       -0.079347
v  Velocity[Y]                 -1.8996          7.2436         0.30987         0.25086
v  Velocity[Z]                 -4.3368          3.0364         0.11139      -0.0015466
v  ǁVelocityǁ                0.0058163          7.9339         0.69788         0.66115
v  Pressure                    -274.99          5699.5          4123.6            3108
v  turbulent_viscosity      5.7297e-05         0.44432        0.020952         0.01879
v  CourantNb                   0.21063          4104.3           149.7          105.92
v  FourierNb                    7.0846          4019.3          85.267          46.657
v  total_pressure           4.9973e+05       5.057e+05      5.0412e+05      5.0311e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.423            5351          234.97          152.58


 TIME FOR THE TIME STEP               35:        0.17962E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.183766577E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283075E+00
Free inlet               13           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 0.37706E+01
   Friction velocity        uet   :  0.15596E-01 0.10405E+01
   Friction velocity        uk    :  0.15596E-01 0.10405E+01
   Dimensionless distance   yplus :  0.16380E+00 0.88270E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3377
   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    0.14052E+00     782   0.93616E+00   0.48801E-02 
c  VelocityY    0.14052E+00     782   0.93616E+00   0.00000E+00 
c  VelocityZ    0.14052E+00     782   0.93616E+00   0.00000E+00 
c  Pressure     0.11671E+00     664   0.87512E-02   0.12221E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -5.3328          3.6739       -0.077368       -0.079642
v  Velocity[Y]                 -2.1509          6.9286         0.31286         0.25207
v  Velocity[Z]                 -4.4455          3.1256         0.11076      -0.0017594
v  ǁVelocityǁ                 0.006779          7.6809         0.70392         0.66525
v  Pressure                    -277.43          5893.7          4215.3          3172.5
v  turbulent_viscosity      5.4029e-05         0.48149        0.021423        0.019089
v  CourantNb                   0.04127          4432.2          151.34          107.16
v  FourierNb                    7.1258          4146.6          85.973          46.989
v  total_pressure           4.9972e+05      5.0589e+05      5.0422e+05      5.0317e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.583          5592.1          237.32          154.15


 TIME FOR THE TIME STEP               36:        0.17948E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.960363309E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283065E+00
Free inlet               13           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 0.40095E+01
   Friction velocity        uet   :  0.10049E-01 0.10639E+01
   Friction velocity        uk    :  0.10049E-01 0.10639E+01
   Dimensionless distance   yplus :  0.10896E+00 0.87769E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3379
   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    0.13226E+00     803   0.92707E+00   0.53628E-02 
c  VelocityY    0.13226E+00     803   0.92707E+00   0.00000E+00 
c  VelocityZ    0.13226E+00     803   0.92707E+00   0.00000E+00 
c  Pressure     0.12285E+00     662   0.86483E-02   0.12251E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -5.6759          3.8304       -0.078507       -0.079992
v  Velocity[Y]                 -2.2647          8.0447         0.31444         0.25321
v  Velocity[Z]                 -4.5356          3.2803         0.11011      -0.0019973
v  ǁVelocityǁ                0.0062572          8.5926         0.70955         0.66963
v  Pressure                    -281.05          6091.9          4307.5          3237.5
v  turbulent_viscosity      5.7729e-05         0.50956          0.0219          0.0194
v  CourantNb                   0.22742          4922.9          153.42          108.46
v  FourierNb                    7.1844          4246.8          86.672          47.319
v  total_pressure           4.9972e+05      5.0609e+05      5.0431e+05      5.0324e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.411            5879           240.1          155.78


 TIME FOR THE TIME STEP               37:        0.20159E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.241419412E-16
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 0.43917E+01
   Friction velocity        uet   :  0.11598E-01 0.10786E+01
   Friction velocity        uk    :  0.11598E-01 0.10786E+01
   Dimensionless distance   yplus :  0.18639E+00 0.95490E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3351
   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    0.13090E+00     886   0.91761E+00   0.37847E-02 
c  VelocityY    0.13090E+00     886   0.91761E+00   0.00000E+00 
c  VelocityZ    0.13090E+00     886   0.91761E+00   0.00000E+00 
c  Pressure     0.12892E+00     661   0.86695E-02   0.12234E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -6.0501          4.0122       -0.078761       -0.080258
v  Velocity[Y]                 -2.5838          7.6255         0.31691         0.25448
v  Velocity[Z]                 -4.7989          3.3907         0.10986      -0.0021795
v  ǁVelocityǁ                0.0055649          8.4222         0.71589         0.67444
v  Pressure                    -285.07          6298.8          4402.2          3304.1
v  turbulent_viscosity      5.5579e-05         0.52749        0.022398        0.019711
v  CourantNb                   0.23974          5164.5           155.2          109.64
v  FourierNb                    7.2277            4405          87.412          47.662
v  total_pressure           4.9971e+05       5.063e+05       5.044e+05       5.033e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.611          6123.8          242.61           157.3


 TIME FOR THE TIME STEP               38:        0.19407E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.686120427E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283054E+00
Free inlet               13           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 0.45085E+01
   Friction velocity        uet   :  0.14534E-01 0.10916E+01
   Friction velocity        uk    :  0.14534E-01 0.10916E+01
   Dimensionless distance   yplus :  0.17819E+00 0.98578E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3330
   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    0.18474E+00     870   0.96112E+00   0.53458E-02 
c  VelocityY    0.18474E+00     870   0.96112E+00   0.00000E+00 
c  VelocityZ    0.18474E+00     870   0.96112E+00   0.00000E+00 
c  Pressure     0.13535E+00     661   0.86403E-02   0.12222E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -6.4734          4.1472        -0.07975       -0.080453
v  Velocity[Y]                 -2.7166          8.8084         0.31854         0.25549
v  Velocity[Z]                 -5.2119          3.4822         0.10929      -0.0020852
v  ǁVelocityǁ                0.0064915          9.5402         0.72144         0.67889
v  Pressure                    -290.23          6516.2            4499          3371.9
v  turbulent_viscosity      5.6987e-05         0.58038        0.022923         0.02006
v  CourantNb                   0.28554          5704.5          157.35          111.01
v  FourierNb                    7.2709            4451          88.161          48.029
v  total_pressure           4.9971e+05      5.0652e+05       5.045e+05      5.0337e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.249          6563.8          245.52          159.04


 TIME FOR THE TIME STEP               39:        0.21372E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.119330862E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283053E+00
Free inlet               13           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 0.47455E+01
   Friction velocity        uet   :  0.12977E-01 0.11138E+01
   Friction velocity        uk    :  0.12977E-01 0.11138E+01
   Dimensionless distance   yplus :  0.18357E+00 0.10354E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3307
   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    0.15836E+00     993   0.93708E+00   0.59245E-02 
c  VelocityY    0.15836E+00     993   0.93708E+00   0.00000E+00 
c  VelocityZ    0.15836E+00     993   0.93708E+00   0.00000E+00 
c  Pressure     0.14204E+00     660   0.86555E-02   0.12199E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -6.8258          4.3528         -0.0805       -0.080653
v  Velocity[Y]                 -3.0767          8.4166         0.32247         0.25721
v  Velocity[Z]                 -5.3383          3.7183         0.10886      -0.0022619
v  ǁVelocityǁ                0.0065206          9.3069         0.72876         0.68363
v  Pressure                    -293.99          6740.5          4597.5          3440.8
v  turbulent_viscosity      5.3707e-05         0.60476        0.023422        0.020366
v  CourantNb                   0.34058            6018           159.2          112.24
v  FourierNb                    7.3076          4563.9          88.936          48.415
v  total_pressure           4.9971e+05      5.0674e+05       5.046e+05      5.0344e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           9.721          6945.2          248.13          160.66


 TIME FOR THE TIME STEP               40:        0.23549E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.412964561E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283052E+00
Free inlet               13           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 0.53887E+01
   Friction velocity        uet   :  0.13475E-01 0.11188E+01
   Friction velocity        uk    :  0.13475E-01 0.11188E+01
   Dimensionless distance   yplus :  0.19047E+00 0.10960E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3290
   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    0.20348E+00     964   0.96407E+00   0.60945E-02 
c  VelocityY    0.20348E+00     964   0.96407E+00   0.00000E+00 
c  VelocityZ    0.20348E+00     964   0.96407E+00   0.00000E+00 
c  Pressure     0.14853E+00     659   0.85145E-02   0.12129E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -7.2683          4.5526       -0.081684       -0.080972
v  Velocity[Y]                 -3.4146          9.8257         0.32303         0.25827
v  Velocity[Z]                 -5.6135          3.8952         0.10853      -0.0024906
v  ǁVelocityǁ                0.0071139           10.49           0.735          0.6887
v  Pressure                    -298.12          6970.9          4696.6          3509.8
v  turbulent_viscosity      5.8582e-05         0.64983         0.02401        0.020738
v  CourantNb                  0.085361          6623.6          161.78          113.78
v  FourierNb                    7.3495            4677          89.783          48.834
v  total_pressure            4.997e+05      5.0697e+05       5.047e+05      5.0351e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           9.165          7590.4          251.57          162.62


 TIME FOR THE TIME STEP               41:        0.23081E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.645469943E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283063E+00
Free inlet               13           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 0.55655E+01
   Friction velocity        uet   :  0.14788E-01 0.11440E+01
   Friction velocity        uk    :  0.14788E-01 0.11440E+01
   Dimensionless distance   yplus :  0.19997E+00 0.11456E+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          9 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.24303E+00    1044   0.97329E+00   0.77706E-02 
c  VelocityY    0.24303E+00    1044   0.97329E+00   0.00000E+00 
c  VelocityZ    0.24303E+00    1044   0.97329E+00   0.00000E+00 
c  Pressure     0.15665E+00     658   0.85491E-02   0.12156E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -7.7739          4.7245       -0.082642       -0.081406
v  Velocity[Y]                 -3.6662          9.0602         0.32679         0.26005
v  Velocity[Z]                  -6.022          4.0025         0.10753       -0.002713
v  ǁVelocityǁ                0.0069914          10.208         0.74255          0.6935
v  Pressure                    -302.47            7215          4800.1          3581.6
v  turbulent_viscosity      5.6956e-05         0.68644        0.024617        0.021087
v  CourantNb                   0.34253            6991          163.76          115.08
v  FourierNb                    7.3511            4877          90.745          49.261
v  total_pressure            4.997e+05      5.0721e+05       5.048e+05      5.0358e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.0546          8013.8          254.51          164.34


 TIME FOR THE TIME STEP               42:        0.24134E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.357374003E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283081E+00
Free inlet               13           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 0.56941E+01
   Friction velocity        uet   :  0.11635E-01 0.11597E+01
   Friction velocity        uk    :  0.11635E-01 0.11597E+01
   Dimensionless distance   yplus :  0.19435E+00 0.11438E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3287
   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    0.26521E+00    1062   0.97590E+00   0.84101E-02 
c  VelocityY    0.26521E+00    1062   0.97590E+00   0.00000E+00 
c  VelocityZ    0.26521E+00    1062   0.97590E+00   0.00000E+00 
c  Pressure     0.16445E+00     655   0.84664E-02   0.12126E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -8.2719          4.9105       -0.083221       -0.081274
v  Velocity[Y]                 -3.8371          10.811         0.32902         0.26126
v  Velocity[Z]                 -6.2238           4.126          0.1073      -0.0027206
v  ǁVelocityǁ                0.0069794          11.649         0.74889         0.69756
v  Pressure                     -310.8          7466.6          4903.6          3653.4
v  turbulent_viscosity       5.619e-05         0.75162        0.025205        0.021411
v  CourantNb                   0.10878          7731.2          166.49          116.72
v  FourierNb                    7.3902          4971.6          91.606          49.657
v  total_pressure           4.9969e+05      5.0747e+05       5.049e+05      5.0365e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.1318          8794.1           258.1          166.38


 TIME FOR THE TIME STEP               43:        0.24363E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.350489131E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283094E+00
Free inlet               13           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 0.64528E+01
   Friction velocity        uet   :  0.52415E-02 0.11703E+01
   Friction velocity        uk    :  0.52415E-02 0.11703E+01
   Dimensionless distance   yplus :  0.45644E-01 0.12363E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3277
   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    0.23907E+00    1151   0.96555E+00   0.72557E-02 
c  VelocityY    0.23907E+00    1151   0.96555E+00   0.00000E+00 
c  VelocityZ    0.23907E+00    1151   0.96555E+00   0.00000E+00 
c  Pressure     0.17359E+00     655   0.84749E-02   0.12165E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -8.7893          5.1707        -0.08409       -0.081707
v  Velocity[Y]                 -4.3053          10.142         0.33264         0.26278
v  Velocity[Z]                 -6.5437          4.1754         0.10671      -0.0031263
v  ǁVelocityǁ                0.0048401          11.291         0.75737         0.70343
v  Pressure                    -320.12          7729.8          5012.1          3728.5
v  turbulent_viscosity      5.4039e-05         0.77559        0.025803        0.021736
v  CourantNb                   0.50152          8062.6          168.79          118.06
v  FourierNb                    7.3665          5040.2          92.529          50.057
v  total_pressure           4.9968e+05      5.0773e+05      5.0501e+05      5.0373e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.1186            9199          261.32          168.12


 TIME FOR THE TIME STEP               44:        0.22609E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.681006549E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283094E+00
Free inlet               13           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 0.63869E+01
   Friction velocity        uet   :  0.14881E-01 0.11754E+01
   Friction velocity        uk    :  0.14881E-01 0.11754E+01
   Dimensionless distance   yplus :  0.15355E+00 0.12406E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3264
   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    0.39518E+00    1117   0.98572E+00   0.95156E-02 
c  VelocityY    0.39518E+00    1117   0.98572E+00   0.00000E+00 
c  VelocityZ    0.39518E+00    1117   0.98572E+00   0.00000E+00 
c  Pressure     0.18083E+00     645   0.84489E-02   0.12035E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -9.4259          5.3916       -0.085716       -0.081919
v  Velocity[Y]                 -4.4915          10.588         0.33433         0.26398
v  Velocity[Z]                 -7.0618          4.4216         0.10621      -0.0032486
v  ǁVelocityǁ                0.0034087          12.903          0.7646         0.70848
v  Pressure                    -331.34          8005.8          5120.1          3802.8
v  turbulent_viscosity      5.7616e-05         0.84357        0.026462        0.022107
v  CourantNb                  0.058311          8875.6          171.78          119.92
v  FourierNb                    7.3468          5127.3          93.496          50.502
v  total_pressure           4.9967e+05      5.0801e+05      5.0512e+05       5.038e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8.9872           10052          265.27          170.42


 TIME FOR THE TIME STEP               45:        0.22199E+01

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.606570749E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283367E+00
Free inlet               13           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 0.68007E+01
   Friction velocity        uet   :  0.10459E-01 0.11914E+01
   Friction velocity        uk    :  0.10459E-01 0.11914E+01
   Dimensionless distance   yplus :  0.13438E+00 0.13170E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3245
   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    0.31171E+00    1246   0.97298E+00   0.90444E-02 
c  VelocityY    0.31171E+00    1246   0.97298E+00   0.00000E+00 
c  VelocityZ    0.31171E+00    1246   0.97298E+00   0.00000E+00 
c  Pressure     0.19213E+00     645   0.84278E-02   0.12125E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -9.9997          5.7093       -0.086116       -0.082278
v  Velocity[Y]                 -5.0285          11.166         0.33908         0.26573
v  Velocity[Z]                 -7.2899          4.6658         0.10544      -0.0034452
v  ǁVelocityǁ                0.0030497          12.577         0.77408          0.7136
v  Pressure                    -341.71          8293.5          5234.9          3881.9
v  turbulent_viscosity      5.7094e-05         0.88774        0.027215        0.022524
v  CourantNb                   0.18107          9281.2          174.36          121.49
v  FourierNb                    7.3117          5296.5          94.682           51.04
v  total_pressure           4.9966e+05      5.0829e+05      5.0523e+05      5.0388e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.0598           10543          269.04          172.53


 TIME FOR THE TIME STEP               46:        0.23816E+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        -0.397274334E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283398E+00
Free inlet               13           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 0.72894E+01
   Friction velocity        uet   :  0.13389E-01 0.12147E+01
   Friction velocity        uk    :  0.13389E-01 0.12147E+01
   Dimensionless distance   yplus :  0.17223E+00 0.13425E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3228
   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    0.41848E+00    1213   0.98727E+00   0.10152E-01 
c  VelocityY    0.41848E+00    1213   0.98727E+00   0.00000E+00 
c  VelocityZ    0.41848E+00    1213   0.98727E+00   0.00000E+00 
c  Pressure     0.20103E+00     645   0.83803E-02   0.12042E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -10.677          5.8373       -0.087942       -0.082774
v  Velocity[Y]                 -5.2202          11.773          0.3411         0.26751
v  Velocity[Z]                 -7.7439          4.8636         0.10587      -0.0036844
v  ǁVelocityǁ                0.0056956          14.262         0.78289         0.71934
v  Pressure                    -352.38          8592.6          5352.1          3962.7
v  turbulent_viscosity      6.4741e-05         0.95956         0.02788        0.022879
v  CourantNb                  0.050599           10181          177.82          123.48
v  FourierNb                    7.2306          5430.9          95.684          51.495
v  total_pressure           4.9965e+05      5.0859e+05      5.0535e+05      5.0396e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.0704           11486          273.51          174.97


 TIME FOR THE TIME STEP               47:        0.26913E+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         0.261102538E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283410E+00
Free inlet               13           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 0.79838E+01
   Friction velocity        uet   :  0.11069E-01 0.12268E+01
   Friction velocity        uk    :  0.11069E-01 0.12268E+01
   Dimensionless distance   yplus :  0.14554E+00 0.14456E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3222
   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    0.49345E+00    1301   0.98903E+00   0.13070E-01 
c  VelocityY    0.49345E+00    1301   0.98903E+00   0.00000E+00 
c  VelocityZ    0.49345E+00    1301   0.98903E+00   0.00000E+00 
c  Pressure     0.21150E+00     645   0.84335E-02   0.12014E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -11.358          6.2032       -0.089079       -0.083121
v  Velocity[Y]                 -5.8712          12.179         0.34643         0.26926
v  Velocity[Z]                 -8.4185          5.1354         0.10504      -0.0040392
v  ǁVelocityǁ                0.0072945           14.08         0.79238          0.7251
v  Pressure                     -363.4          8913.7          5476.5          4048.1
v  turbulent_viscosity      6.4305e-05          1.0104        0.028688         0.02331
v  CourantNb                   0.23346           10587          180.72          125.16
v  FourierNb                    7.3821          5506.7          96.951          52.042
v  total_pressure           4.9964e+05      5.0891e+05      5.0548e+05      5.0405e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.408           11993          277.67           177.2


 TIME FOR THE TIME STEP               48:        0.24538E+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        -0.329158989E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283452E+00
Free inlet               13           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 0.82233E+01
   Friction velocity        uet   :  0.16035E-01 0.12463E+01
   Friction velocity        uk    :  0.16035E-01 0.12463E+01
   Dimensionless distance   yplus :  0.18126E+00 0.13955E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3199
   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    0.55459E+00    1321   0.98961E+00   0.15111E-01 
c  VelocityY    0.55459E+00    1321   0.98961E+00   0.00000E+00 
c  VelocityZ    0.55459E+00    1321   0.98961E+00   0.00000E+00 
c  Pressure     0.22310E+00     642   0.83550E-02   0.12011E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -12.07          6.4452       -0.091445       -0.083572
v  Velocity[Y]                 -6.0593          13.457          0.3492         0.27127
v  Velocity[Z]                 -8.7131          5.3656         0.10449      -0.0043251
v  ǁVelocityǁ                0.0059076          16.002         0.80234         0.73159
v  Pressure                    -373.07          9243.3          5599.5          4132.3
v  turbulent_viscosity      7.8662e-05          1.0863        0.029373        0.023689
v  CourantNb                    0.1908           11697          184.31          127.34
v  FourierNb                    7.5507          5607.1           97.98          52.514
v  total_pressure           4.9963e+05      5.0924e+05       5.056e+05      5.0413e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.613           13162          282.29          179.85


 TIME FOR THE TIME STEP               49:        0.28227E+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        -0.101391194E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283424E+00
Free inlet               13           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 0.91872E+01
   Friction velocity        uet   :  0.14510E-01 0.12450E+01
   Friction velocity        uk    :  0.14510E-01 0.12450E+01
   Dimensionless distance   yplus :  0.20121E+00 0.15738E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3184
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for          9 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:    0.80239E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.52778E+00    1415   0.99004E+00   0.13102E-01 
c  VelocityY    0.52778E+00    1415   0.99004E+00   0.00000E+00 
c  VelocityZ    0.52778E+00    1415   0.99004E+00   0.00000E+00 
c  Pressure     0.23647E+00     643   0.83438E-02   0.12065E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -12.869          6.6964       -0.093019       -0.084278
v  Velocity[Y]                 -6.7964          13.656         0.35349         0.27308
v  Velocity[Z]                   -9.16          5.6099         0.10382      -0.0046635
v  ǁVelocityǁ                0.0080604          15.794         0.81562          0.7404
v  Pressure                    -381.25          9586.6          5731.4          4222.5
v  turbulent_viscosity      7.9177e-05          1.1306        0.030374        0.024275
v  CourantNb                   0.11503           12083          187.67          129.24
v  FourierNb                    7.5689          6613.5           99.56          53.225
v  total_pressure           4.9962e+05      5.0959e+05      5.0573e+05      5.0422e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.332           13654          287.23          182.47


 TIME FOR THE TIME STEP               50:        0.30332E+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        -0.923367821E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283478E+00
Free inlet               13           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 0.92892E+01
   Friction velocity        uet   :  0.22442E-01 0.12396E+01
   Friction velocity        uk    :  0.22442E-01 0.12396E+01
   Dimensionless distance   yplus :  0.23329E+00 0.15847E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3154
   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    0.82446E+00    1375   0.99290E+00   0.18863E-01 
c  VelocityY    0.82446E+00    1375   0.99290E+00   0.00000E+00 
c  VelocityZ    0.82446E+00    1375   0.99290E+00   0.00000E+00 
c  Pressure     0.24715E+00     642   0.83118E-02   0.11949E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -13.932          7.0785       -0.094531       -0.084577
v  Velocity[Y]                  -7.096          14.189         0.35719         0.27477
v  Velocity[Z]                 -10.005           6.015         0.10453      -0.0050549
v  ǁVelocityǁ                0.0080177          17.644         0.82305         0.74427
v  Pressure                    -389.16            9956          5869.4          4317.2
v  turbulent_viscosity      7.8834e-05          1.2399        0.031288        0.024732
v  CourantNb                  0.027642           13352          192.05          131.91
v  FourierNb                    7.4471          9549.9          101.01          53.867
v  total_pressure           4.9961e+05      5.0996e+05      5.0587e+05      5.0432e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.309           14991          293.07          185.78


 TIME FOR THE TIME STEP               51:        0.26102E+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        -0.226499456E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283518E+00
Free inlet               13           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 0.10091E+02
   Friction velocity        uet   :  0.12790E-01 0.12946E+01
   Friction velocity        uk    :  0.12790E-01 0.12946E+01
   Dimensionless distance   yplus :  0.17609E+00 0.16484E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3133
   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    0.63952E+00    1544   0.99259E+00   0.22145E-01 
c  VelocityY    0.63952E+00    1544   0.99259E+00   0.00000E+00 
c  VelocityZ    0.63952E+00    1544   0.99259E+00   0.00000E+00 
c  Pressure     0.26408E+00     641   0.83368E-02   0.12089E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -14.55          7.5085       -0.095768       -0.084946
v  Velocity[Y]                 -7.9235          15.232         0.36481         0.27738
v  Velocity[Z]                 -10.307          6.1779         0.10264      -0.0052784
v  ǁVelocityǁ                0.0079755          17.738          0.8407         0.75511
v  Pressure                    -397.84           10340          6014.8          4417.2
v  turbulent_viscosity      8.0557e-05           1.313         0.03227        0.025227
v  CourantNb                   0.13698           13888          195.27           133.7
v  FourierNb                    7.5699           14199          102.62          54.509
v  total_pressure            4.996e+05      5.1034e+05      5.0601e+05      5.0442e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.859           15631          297.88          188.21


 TIME FOR THE TIME STEP               52:        0.31993E+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        -0.180398960E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283526E+00
Free inlet               13           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 0.10557E+02
   Friction velocity        uet   :  0.17089E-01 0.14745E+01
   Friction velocity        uk    :  0.17089E-01 0.14745E+01
   Dimensionless distance   yplus :  0.18087E+00 0.17572E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3111
   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    0.87925E+00    1514   0.99392E+00   0.18625E-01 
c  VelocityY    0.87925E+00    1514   0.99392E+00   0.00000E+00 
c  VelocityZ    0.87925E+00    1514   0.99392E+00   0.00000E+00 
c  Pressure     0.27750E+00     638   0.82619E-02   0.12021E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -15.628          7.6768         -0.1003       -0.085922
v  Velocity[Y]                 -8.1998          16.073         0.36472         0.27896
v  Velocity[Z]                 -10.969          6.6264           0.104       -0.005686
v  ǁVelocityǁ                0.0071184          19.632         0.84959         0.76091
v  Pressure                    -406.87           10741          6161.4          4517.4
v  turbulent_viscosity      7.9734e-05          1.3809        0.033223        0.025782
v  CourantNb                   0.38521           15162          200.83          136.87
v  FourierNb                     7.569           12504          104.05          55.196
v  total_pressure           4.9959e+05      5.1074e+05      5.0616e+05      5.0452e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.5712           16988          304.89          192.07


 TIME FOR THE TIME STEP               53:        0.28765E+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        -0.662577494E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283526E+00
Free inlet               13           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 0.11383E+02
   Friction velocity        uet   :  0.16145E-01 0.16602E+01
   Friction velocity        uk    :  0.16145E-01 0.16602E+01
   Dimensionless distance   yplus :  0.18415E+00 0.18465E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3103
   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    0.10574E+01    1617   0.99443E+00   0.27522E-01 
c  VelocityY    0.10574E+01    1617   0.99443E+00   0.00000E+00 
c  VelocityZ    0.10574E+01    1617   0.99443E+00   0.00000E+00 
c  Pressure     0.29376E+00     641   0.83635E-02   0.12045E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -16.782           8.111        -0.10088       -0.086707
v  Velocity[Y]                  -9.195          17.293         0.37237         0.28099
v  Velocity[Z]                 -11.833          6.9748         0.10189      -0.0063122
v  ǁVelocityǁ                0.0073651          20.272         0.86585         0.77183
v  Pressure                    -415.47           11181          6319.9            4626
v  turbulent_viscosity      8.1127e-05          1.4821        0.034449        0.026397
v  CourantNb                  0.068825           15775          204.18          138.85
v  FourierNb                    7.5755          9762.9          105.93          56.003
v  total_pressure           4.9958e+05      5.1118e+05      5.0632e+05      5.0463e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           10.01           17716           310.1          194.85


 TIME FOR THE TIME STEP               54:        0.33221E+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        -0.663689630E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283555E+00
Free inlet               13           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 0.12273E+02
   Friction velocity        uet   :  0.20627E-01 0.16197E+01
   Friction velocity        uk    :  0.20627E-01 0.16197E+01
   Dimensionless distance   yplus :  0.21079E+00 0.17982E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3070
   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    0.11159E+01    1613   0.99214E+00   0.30336E-01 
c  VelocityY    0.11159E+01    1613   0.99214E+00   0.00000E+00 
c  VelocityZ    0.11159E+01    1613   0.99214E+00   0.00000E+00 
c  Pressure     0.30994E+00     637   0.82254E-02   0.12023E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -17.96          8.6048        -0.10229       -0.086957
v  Velocity[Y]                 -9.5036          18.238         0.37527         0.28364
v  Velocity[Z]                 -12.286          7.5182          0.1018      -0.0059483
v  ǁVelocityǁ                0.0087025          21.844         0.87769         0.77938
v  Pressure                    -436.28           11653          6477.6          4733.8
v  turbulent_viscosity      7.9467e-05          1.6109        0.035449        0.026965
v  CourantNb                   0.41947           17286          209.79          142.24
v  FourierNb                     7.223          9372.1          107.38          56.682
v  total_pressure           4.9956e+05      5.1165e+05      5.0648e+05      5.0473e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.9353           19334          317.17          198.92


 TIME FOR THE TIME STEP               55:        0.30532E+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        -0.560450202E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283531E+00
Free inlet               13           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 0.13203E+02
   Friction velocity        uet   :  0.14188E-01 0.16232E+01
   Friction velocity        uk    :  0.14188E-01 0.16232E+01
   Dimensionless distance   yplus :  0.20785E+00 0.20324E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3035
   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    0.10820E+01    1800   0.99478E+00   0.29196E-01 
c  VelocityY    0.10820E+01    1800   0.99478E+00   0.00000E+00 
c  VelocityZ    0.10820E+01    1800   0.99478E+00   0.00000E+00 
c  Pressure     0.32910E+00     636   0.82624E-02   0.12073E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -18.901          8.9538          -0.105       -0.087915
v  Velocity[Y]                 -10.675          19.188         0.38291         0.28584
v  Velocity[Z]                 -13.008          7.7609         0.10012       -0.006603
v  ǁVelocityǁ                 0.011713           22.58         0.89817         0.79283
v  Pressure                    -490.03           12163          6647.6          4849.9
v  turbulent_viscosity      7.8242e-05          1.6738        0.036826        0.027719
v  CourantNb                   0.46155           17907          213.99          144.61
v  FourierNb                    7.2853          9811.2          109.52          57.619
v  total_pressure           4.9951e+05      5.1216e+05      5.0665e+05      5.0485e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.577           20515          323.51          202.23


 TIME FOR THE TIME STEP               56:        0.32530E+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        -0.457081676E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283554E+00
Free inlet               13           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 0.13913E+02
   Friction velocity        uet   :  0.22875E-01 0.16461E+01
   Friction velocity        uk    :  0.22875E-01 0.16461E+01
   Dimensionless distance   yplus :  0.22377E+00 0.20403E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       3001
   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    0.17624E+01    1668   0.99594E+00   0.41006E-01 
c  VelocityY    0.17624E+01    1668   0.99594E+00   0.00000E+00 
c  VelocityZ    0.17624E+01    1668   0.99594E+00   0.00000E+00 
c  Pressure     0.34538E+00     636   0.82092E-02   0.11969E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -20.489          9.2396        -0.10726       -0.088748
v  Velocity[Y]                 -10.977          20.072         0.38422         0.28824
v  Velocity[Z]                 -14.295          8.5624          0.1022      -0.0070882
v  ǁVelocityǁ                  0.00968          24.552         0.90929         0.79949
v  Pressure                     -544.2           12695          6826.3          4972.5
v  turbulent_viscosity      7.9646e-05          1.8032        0.037918        0.028302
v  CourantNb                   0.49259           19620          220.74          148.66
v  FourierNb                    7.3127           11311          111.21          58.393
v  total_pressure           4.9946e+05       5.127e+05      5.0683e+05      5.0497e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.204           21906          331.95          207.05


 TIME FOR THE TIME STEP               57:        0.33909E+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        -0.128967374E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283612E+00
Free inlet               13           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 0.15193E+02
   Friction velocity        uet   :  0.23937E-01 0.17634E+01
   Friction velocity        uk    :  0.23937E-01 0.17634E+01
   Dimensionless distance   yplus :  0.24728E+00 0.21209E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2992
   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    0.13662E+01    1900   0.99584E+00   0.43772E-01 
c  VelocityY    0.13662E+01    1900   0.99584E+00   0.00000E+00 
c  VelocityZ    0.13662E+01    1900   0.99584E+00   0.00000E+00 
c  Pressure     0.36851E+00     635   0.82341E-02   0.12058E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -21.551          9.7896        -0.11097       -0.089396
v  Velocity[Y]                 -12.298          21.846         0.39638         0.29144
v  Velocity[Z]                 -14.622          8.7378        0.097863      -0.0076712
v  ǁVelocityǁ                0.0050919          25.734          0.9336         0.81251
v  Pressure                    -601.45           13269          7012.9          5099.9
v  turbulent_viscosity      8.2881e-05          1.8911        0.039373         0.02903
v  CourantNb                   0.74991           20342          225.22           151.2
v  FourierNb                    7.3279           11896          113.55          59.375
v  total_pressure            4.994e+05      5.1327e+05      5.0701e+05       5.051e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.448           24496          338.78          210.58


 TIME FOR THE TIME STEP               58:        0.37612E+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        -0.119528508E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283603E+00
Free inlet               13           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 0.15975E+02
   Friction velocity        uet   :  0.23825E-01 0.18343E+01
   Friction velocity        uk    :  0.23825E-01 0.18343E+01
   Dimensionless distance   yplus :  0.26183E+00 0.21838E+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          9 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.19234E+01    1860   0.99652E+00   0.36829E-01 
c  VelocityY    0.19234E+01    1860   0.99652E+00   0.00000E+00 
c  VelocityZ    0.19234E+01    1860   0.99652E+00   0.00000E+00 
c  Pressure     0.38694E+00     632   0.81259E-02   0.11947E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -23.157          10.289        -0.11311       -0.090321
v  Velocity[Y]                 -12.676          22.466         0.39628         0.29396
v  Velocity[Z]                 -15.518          9.3779         0.10064       -0.007888
v  ǁVelocityǁ                0.0022643           27.53         0.94158         0.81996
v  Pressure                    -657.76           13867          7208.7          5234.4
v  turbulent_viscosity      7.8244e-05           2.056        0.040592          0.0297
v  CourantNb                   0.29864           22140          233.21          155.52
v  FourierNb                    7.3982           12720          115.45          60.227
v  total_pressure           4.9934e+05      5.1387e+05      5.0721e+05      5.0523e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.154           26042          348.66          215.75


 TIME FOR THE TIME STEP               59:        0.36675E+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        -0.473353245E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283667E+00
Free inlet               13           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 0.17237E+02
   Friction velocity        uet   :  0.18772E-01 0.19473E+01
   Friction velocity        uk    :  0.18772E-01 0.19473E+01
   Dimensionless distance   yplus :  0.27029E+00 0.24122E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2949
   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    0.21532E+01    1982   0.99596E+00   0.54269E-01 
c  VelocityY    0.21532E+01    1982   0.99596E+00   0.00000E+00 
c  VelocityZ    0.21532E+01    1982   0.99596E+00   0.00000E+00 
c  Pressure     0.41101E+00     632   0.82129E-02   0.11984E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -24.772          10.812        -0.11459       -0.091989
v  Velocity[Y]                  -14.25          24.559         0.40696         0.29639
v  Velocity[Z]                 -16.848          10.009        0.097165      -0.0091122
v  ǁVelocityǁ                0.0082989          29.632         0.97006         0.83771
v  Pressure                     -888.2           14517          7417.1            5377
v  turbulent_viscosity      7.8534e-05          2.1583        0.042343        0.030689
v  CourantNb                   0.17099           23003          236.96          157.95
v  FourierNb                    7.3988           14442          118.17          61.447
v  total_pressure           4.9911e+05      5.1452e+05      5.0742e+05      5.0538e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.841           29196          355.13           219.4


 TIME FOR THE TIME STEP               60:        0.38877E+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        -0.829704109E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273283694E+00
Free inlet               13           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 0.18527E+02
   Friction velocity        uet   :  0.19299E-01 0.20615E+01
   Friction velocity        uk    :  0.19299E-01 0.20615E+01
   Dimensionless distance   yplus :  0.24470E+00 0.23733E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2911
   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    0.24093E+01    1957   0.99689E+00   0.61276E-01 
c  VelocityY    0.24093E+01    1957   0.99689E+00   0.00000E+00 
c  VelocityZ    0.24093E+01    1957   0.99689E+00   0.00000E+00 
c  Pressure     0.43408E+00     622   0.80887E-02   0.11958E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -26.442           11.16        -0.11749       -0.092141
v  Velocity[Y]                 -14.592          25.475         0.41106         0.30004
v  Velocity[Z]                 -17.569          10.566        0.096707      -0.0090723
v  ǁVelocityǁ                0.0066469          31.306         0.98476         0.84591
v  Pressure                    -1211.2           15188          7632.4          5524.4
v  turbulent_viscosity      8.5499e-05          2.3618         0.04368        0.031419
v  CourantNb                  0.093301           25242          246.02          163.18
v  FourierNb                    7.3247           15474          120.16          62.354
v  total_pressure           4.9879e+05      5.1519e+05      5.0763e+05      5.0552e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.259           31248          366.18          225.54


 TIME FOR THE TIME STEP               61:        0.38187E+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        -0.776315953E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284328E+00
Free inlet               13           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 0.19820E+02
   Friction velocity        uet   :  0.23760E-01 0.21745E+01
   Friction velocity        uk    :  0.23760E-01 0.21745E+01
   Dimensionless distance   yplus :  0.22670E+00 0.26299E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2884
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.22640E+01    2165   0.99651E+00   0.54426E-01 
c  VelocityY    0.22640E+01    2165   0.99651E+00   0.00000E+00 
c  VelocityZ    0.22640E+01    2165   0.99651E+00   0.00000E+00 
c  Pressure     0.46242E+00     619   0.81565E-02   0.12030E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -27.95          11.769        -0.12358       -0.094121
v  Velocity[Y]                 -16.329          27.694         0.42181         0.30297
v  Velocity[Z]                 -18.572          11.074        0.096011      -0.0096705
v  ǁVelocityǁ                0.0041441          33.485          1.0146         0.86614
v  Pressure                    -1571.4           15915          7860.3          5679.9
v  turbulent_viscosity      7.6763e-05          2.4028         0.04563        0.032432
v  CourantNb                  0.081291           26077          251.74          166.35
v  FourierNb                    7.3172           17687          123.36          63.709
v  total_pressure           4.9843e+05      5.1591e+05      5.0786e+05      5.0568e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.849           34814          375.09          230.06


 TIME FOR THE TIME STEP               62:        0.38044E+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         0.462535212E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284191E+00
Free inlet               13           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 0.20999E+02
   Friction velocity        uet   :  0.78705E-02 0.22766E+01
   Friction velocity        uk    :  0.78705E-02 0.22766E+01
   Dimensionless distance   yplus :  0.69928E-01 0.26154E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2847
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.37612E+01    1946   0.99707E+00   0.81720E-01 
c  VelocityY    0.37612E+01    1946   0.99707E+00   0.00000E+00 
c  VelocityZ    0.37612E+01    1946   0.99707E+00   0.00000E+00 
c  Pressure     0.48479E+00     623   0.81180E-02   0.11914E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -30.187          12.462        -0.12209       -0.095591
v  Velocity[Y]                 -16.849          29.074         0.42127           0.306
v  Velocity[Z]                 -20.389          12.047        0.097969       -0.010438
v  ǁVelocityǁ                0.0042943          35.819          1.0267         0.87423
v  Pressure                      -1914           16674          8105.1          5847.7
v  turbulent_viscosity      8.2478e-05          2.6832        0.047209         0.03334
v  CourantNb                   0.89282           28483          261.41          172.05
v  FourierNb                    7.2302           20320          125.72          64.789
v  total_pressure           4.9809e+05      5.1667e+05      5.0811e+05      5.0585e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.623           37541          387.13          236.84


 TIME FOR THE TIME STEP               63:        0.38858E+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        -0.637725903E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284512E+00
Free inlet               13           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 0.22799E+02
   Friction velocity        uet   :  0.22658E-01 0.24307E+01
   Friction velocity        uk    :  0.22658E-01 0.24307E+01
   Dimensionless distance   yplus :  0.16522E+00 0.27359E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2832
   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    0.27473E+01    2185   0.99725E+00   0.84917E-01 
c  VelocityY    0.27473E+01    2185   0.99725E+00   0.00000E+00 
c  VelocityZ    0.27473E+01    2185   0.99725E+00   0.00000E+00 
c  Pressure     0.51931E+00     611   0.81116E-02   0.12048E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -31.861          13.029        -0.12989       -0.095693
v  Velocity[Y]                 -18.752           31.57         0.44106         0.31106
v  Velocity[Z]                 -20.841          12.523        0.091809       -0.010481
v  ǁVelocityǁ                0.0071477          38.227           1.062         0.89273
v  Pressure                    -2321.6           17494          8358.1          6020.9
v  turbulent_viscosity      7.9193e-05          2.8037        0.049227        0.034327
v  CourantNb                   0.75318           29546          266.95          175.41
v  FourierNb                     7.151           21593          128.93          66.106
v  total_pressure           4.9768e+05      5.1749e+05      5.0836e+05      5.0602e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.786           41554          395.88          241.52


 TIME FOR THE TIME STEP               64:        0.42222E+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        -0.606613564E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284399E+00
Free inlet               13           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 0.24111E+02
   Friction velocity        uet   :  0.21330E-01 0.25418E+01
   Friction velocity        uk    :  0.21330E-01 0.25418E+01
   Dimensionless distance   yplus :  0.16635E+00 0.29356E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2828
   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    0.40255E+01    2108   0.99751E+00   0.75092E-01 
c  VelocityY    0.40255E+01    2108   0.99751E+00   0.00000E+00 
c  VelocityZ    0.40255E+01    2108   0.99751E+00   0.00000E+00 
c  Pressure     0.54569E+00     621   0.80481E-02   0.11955E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -34.222          13.523         -0.1306       -0.096917
v  Velocity[Y]                 -19.218          32.763         0.43987         0.31406
v  Velocity[Z]                 -22.384          13.394        0.091752        -0.01162
v  ǁVelocityǁ                0.0075724          40.593           1.078         0.90689
v  Pressure                    -2727.9           18352          8633.8          6210.2
v  turbulent_viscosity      8.6993e-05          3.0474        0.051004        0.035309
v  CourantNb                   0.29384           32069          278.34           181.3
v  FourierNb                    7.1307           23161          131.71          67.363
v  total_pressure           4.9727e+05      5.1835e+05      5.0863e+05      5.0621e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.859           45255          410.05          248.67


 TIME FOR THE TIME STEP               65:        0.36178E+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        -0.440085282E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284585E+00
Free inlet               13           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 0.25974E+02
   Friction velocity        uet   :  0.13332E-01 0.26978E+01
   Friction velocity        uk    :  0.13332E-01 0.26978E+01
   Dimensionless distance   yplus :  0.10398E+00 0.30316E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2794
   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    0.44784E+01    2182   0.99706E+00   0.12056E+00 
c  VelocityY    0.44784E+01    2182   0.99706E+00   0.00000E+00 
c  VelocityZ    0.44784E+01    2182   0.99706E+00   0.00000E+00 
c  Pressure     0.58106E+00     623   0.81217E-02   0.12010E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -36.314          14.213        -0.14052       -0.098957
v  Velocity[Y]                 -21.607           35.77         0.45248         0.31679
v  Velocity[Z]                 -24.021          14.447        0.089079       -0.012872
v  ǁVelocityǁ                0.0097694          43.723          1.1189         0.92956
v  Pressure                    -3138.4           19285          8930.8          6413.5
v  turbulent_viscosity      8.0595e-05          3.1409        0.053304        0.036527
v  CourantNb                 0.0039925           33377          284.91          185.74
v  FourierNb                    7.1674           28394          135.43          68.922
v  total_pressure           4.9686e+05      5.1928e+05      5.0893e+05      5.0641e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.638           50120          420.34          254.66


 TIME FOR THE TIME STEP               66:        0.43885E+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        -0.767941759E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284802E+00
Free inlet               13           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 0.27720E+02
   Friction velocity        uet   :  0.16910E-01 0.28425E+01
   Friction velocity        uk    :  0.16910E-01 0.28425E+01
   Dimensionless distance   yplus :  0.11313E+00 0.30388E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2775
   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    0.52372E+01    2165   0.99787E+00   0.15080E+00 
c  VelocityY    0.52372E+01    2165   0.99787E+00   0.00000E+00 
c  VelocityZ    0.52372E+01    2165   0.99787E+00   0.00000E+00 
c  Pressure     0.61275E+00     610   0.79886E-02   0.11952E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -38.894          14.937        -0.14034       -0.099366
v  Velocity[Y]                 -22.131          37.218         0.45876         0.32331
v  Velocity[Z]                 -25.044          15.065        0.088903         -0.0131
v  ǁVelocityǁ                0.0063442          46.236          1.1437         0.94557
v  Pressure                      -3617           20242          9226.2          6615.6
v  turbulent_viscosity       8.486e-05          3.4989        0.055197        0.037552
v  CourantNb                   0.38776           36426          298.21          192.93
v  FourierNb                    7.1999           30162          138.29          70.199
v  total_pressure           4.9638e+05      5.2024e+05      5.0923e+05      5.0662e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.357           54248           436.5          263.13


 TIME FOR THE TIME STEP               67:        0.39068E+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        -0.830239047E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284489E+00
Free inlet               13           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 0.29697E+02
   Friction velocity        uet   :  0.16615E-01 0.30044E+01
   Friction velocity        uk    :  0.16615E-01 0.30044E+01
   Dimensionless distance   yplus :  0.18248E+00 0.34843E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2717
   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    0.47322E+01    2363   0.99751E+00   0.11392E+00 
c  VelocityY    0.47322E+01    2363   0.99751E+00   0.00000E+00 
c  VelocityZ    0.47322E+01    2363   0.99751E+00   0.00000E+00 
c  Pressure     0.65362E+00     620   0.80530E-02   0.12021E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -41.589          15.763        -0.14912         -0.1014
v  Velocity[Y]                 -24.636          40.416         0.47535         0.32624
v  Velocity[Z]                  -26.18          16.113        0.085296       -0.013968
v  ǁVelocityǁ                0.0085111           49.92          1.1751         0.96465
v  Pressure                    -4112.4           21317          9565.3          6848.7
v  turbulent_viscosity      8.2236e-05          3.7238        0.058412         0.03934
v  CourantNb                   0.55728           37653          306.82          197.67
v  FourierNb                    7.2972           34431           143.5          72.459
v  total_pressure           4.9589e+05      5.2132e+05      5.0957e+05      5.0685e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.191           60320          450.32          270.13


 TIME FOR THE TIME STEP               68:        0.40697E+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        -0.127849615E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284684E+00
Free inlet               13           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 0.31889E+02
   Friction velocity        uet   :  0.19612E-01 0.31822E+01
   Friction velocity        uk    :  0.19612E-01 0.31822E+01
   Dimensionless distance   yplus :  0.11900E+00 0.33948E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2706
   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    0.66354E+01    2235   0.99723E+00   0.16074E+00 
c  VelocityY    0.66354E+01    2235   0.99723E+00   0.00000E+00 
c  VelocityZ    0.66354E+01    2235   0.99723E+00   0.00000E+00 
c  Pressure     0.68742E+00     619   0.79844E-02   0.11932E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -44.716          16.321        -0.14223         -0.1017
v  Velocity[Y]                  -25.43          42.147         0.48194         0.33034
v  Velocity[Z]                 -27.995          17.031        0.087816       -0.013962
v  ǁVelocityǁ                0.0087616           53.07          1.2019         0.98402
v  Pressure                    -4642.4           22430          9918.7          7090.7
v  turbulent_viscosity      8.2905e-05          4.0523        0.060046        0.040174
v  CourantNb                   0.34516           41660          318.59          204.38
v  FourierNb                    7.3523           33772          145.96          73.576
v  total_pressure           4.9536e+05      5.2243e+05      5.0992e+05      5.0709e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.639           65543          464.55          277.96


 TIME FOR THE TIME STEP               69:        0.46437E+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        -0.322259720E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284712E+00
Free inlet               13           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 0.34324E+02
   Friction velocity        uet   :  0.29902E-01 0.33774E+01
   Friction velocity        uk    :  0.29902E-01 0.33774E+01
   Dimensionless distance   yplus :  0.22336E+00 0.36823E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2635
   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    0.60323E+01    2298   0.99733E+00   0.17498E+00 
c  VelocityY    0.60323E+01    2298   0.99733E+00   0.00000E+00 
c  VelocityZ    0.60323E+01    2298   0.99733E+00   0.00000E+00 
c  Pressure     0.73531E+00     617   0.80573E-02   0.12037E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -46.811          17.312        -0.16271        -0.10477
v  Velocity[Y]                 -28.332          45.605         0.49974         0.33546
v  Velocity[Z]                 -29.505          17.763        0.085565       -0.015091
v  ǁVelocityǁ                0.0091848          56.401           1.266          1.0203
v  Pressure                    -5222.3           23615           10285          7340.8
v  turbulent_viscosity      8.4253e-05          4.5133        0.063408        0.042053
v  CourantNb                   0.13934           45588          328.61           210.2
v  FourierNb                    7.4007           41482           151.4          75.897
v  total_pressure           4.9478e+05      5.2361e+05      5.1029e+05      5.0734e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.8947           72218             480           286.1


 TIME FOR THE TIME STEP               70:        0.45071E+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        -0.133254552E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284613E+00
Free inlet               13           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 0.36036E+02
   Friction velocity        uet   :  0.18135E-01 0.35134E+01
   Friction velocity        uk    :  0.18135E-01 0.35134E+01
   Dimensionless distance   yplus :  0.20685E+00 0.37789E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2594
   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    0.84370E+01    2251   0.99776E+00   0.21588E+00 
c  VelocityY    0.84370E+01    2251   0.99776E+00   0.00000E+00 
c  VelocityZ    0.84370E+01    2251   0.99776E+00   0.00000E+00 
c  Pressure     0.77546E+00     608   0.79425E-02   0.11972E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -50.742          18.214        -0.15504        -0.10531
v  Velocity[Y]                 -29.209           47.66         0.49371         0.34152
v  Velocity[Z]                 -31.511          19.432        0.086699       -0.016267
v  ǁVelocityǁ                 0.010963          60.437          1.2751          1.0274
v  Pressure                    -5829.1           24848           10663          7597.8
v  turbulent_viscosity      8.6679e-05          4.9063        0.066147        0.043526
v  CourantNb                  0.035322           50747           347.3          220.01
v  FourierNb                    7.4628           40773          155.61          77.779
v  total_pressure           4.9417e+05      5.2485e+05      5.1066e+05       5.076e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.083           78371          502.91          297.79


 TIME FOR THE TIME STEP               71:        0.39613E+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        -0.323986860E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284633E+00
Free inlet               13           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 0.39236E+02
   Friction velocity        uet   :  0.18653E-01 0.37649E+01
   Friction velocity        uk    :  0.18653E-01 0.37649E+01
   Dimensionless distance   yplus :  0.21264E+00 0.41313E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2587
   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    0.77740E+01    2451   0.99823E+00   0.24474E+00 
c  VelocityY    0.77740E+01    2451   0.99823E+00   0.00000E+00 
c  VelocityZ    0.77740E+01    2451   0.99823E+00   0.00000E+00 
c  Pressure     0.82749E+00     618   0.80367E-02   0.12043E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -54.083          19.263        -0.16905        -0.10895
v  Velocity[Y]                 -32.384          51.689         0.52134         0.34507
v  Velocity[Z]                 -32.941          20.518         0.07867       -0.016509
v  ǁVelocityǁ                0.0086276          64.982          1.3307          1.0652
v  Pressure                    -6474.2           26225           11086          7886.4
v  turbulent_viscosity      8.9127e-05          5.4788         0.06978        0.045427
v  CourantNb                   0.20337           55670          354.14          224.35
v  FourierNb                    7.6769           46695          161.52          80.202
v  total_pressure           4.9353e+05      5.2622e+05      5.1109e+05      5.0789e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.708           87101          515.66          304.55


 TIME FOR THE TIME STEP               72:        0.42462E+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        -0.239147848E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284867E+00
Free inlet               13           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 0.41928E+02
   Friction velocity        uet   :  0.10888E-01 0.39741E+01
   Friction velocity        uk    :  0.10888E-01 0.39741E+01
   Dimensionless distance   yplus :  0.68937E-01 0.42397E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2553
   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    0.10953E+02    2258   0.99662E+00   0.24141E+00 
c  VelocityY    0.10953E+02    2258   0.99662E+00   0.00000E+00 
c  VelocityZ    0.10953E+02    2258   0.99662E+00   0.00000E+00 
c  Pressure     0.87033E+00     605   0.79195E-02   0.11954E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -57.756          19.857         -0.1602         -0.1094
v  Velocity[Y]                 -33.255          53.925         0.52552         0.35332
v  Velocity[Z]                 -35.416          21.453        0.078971       -0.017442
v  ǁVelocityǁ                 0.014735          68.615          1.3635          1.0861
v  Pressure                    -7166.9           27609           11515          8178.1
v  turbulent_viscosity      8.3777e-05          5.9334        0.072297        0.046929
v  CourantNb                   0.24555           64177          371.92          234.55
v  FourierNb                    7.6784           53047          165.27          82.006
v  total_pressure           4.9283e+05      5.2761e+05      5.1151e+05      5.0818e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.973           93820          537.19          316.55


 TIME FOR THE TIME STEP               73:        0.42987E+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        -0.462138000E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273284887E+00
Free inlet               13           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 0.44781E+02
   Friction velocity        uet   :  0.26721E-01 0.41937E+01
   Friction velocity        uk    :  0.26721E-01 0.41937E+01
   Dimensionless distance   yplus :  0.31029E+00 0.44739E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2504
   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    0.99516E+01    2574   0.99799E+00   0.50100E+00 
c  VelocityY    0.99516E+01    2574   0.99799E+00   0.00000E+00 
c  VelocityZ    0.99516E+01    2574   0.99799E+00   0.00000E+00 
c  Pressure     0.93417E+00     618   0.80447E-02   0.12096E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -60.802          21.945        -0.18181        -0.11366
v  Velocity[Y]                 -37.103          58.473         0.54967          0.3578
v  Velocity[Z]                 -37.893          23.186        0.069903       -0.017536
v  ǁVelocityǁ                0.0064592          73.417          1.4487           1.146
v  Pressure                      -7897           29143           11987          8500.3
v  turbulent_viscosity      9.3411e-05          6.6096        0.076567        0.049326
v  CourantNb                  0.047858           70107          384.12          241.46
v  FourierNb                    7.0265           60401          172.19          84.876
v  total_pressure            4.921e+05      5.2914e+05      5.1199e+05       5.085e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.016      1.0337e+05          556.31          326.34


 TIME FOR THE TIME STEP               74:        0.49115E+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        -0.364364047E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285215E+00
Free inlet               13           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 0.47410E+02
   Friction velocity        uet   :  0.21999E-01 0.43996E+01
   Friction velocity        uk    :  0.21999E-01 0.43996E+01
   Dimensionless distance   yplus :  0.24137E+00 0.46877E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2416
   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    0.14042E+02    2329   0.99807E+00   0.51045E+00 
c  VelocityY    0.14042E+02    2329   0.99807E+00   0.00000E+00 
c  VelocityZ    0.14042E+02    2329   0.99807E+00   0.00000E+00 
c  Pressure     0.98511E+00     616   0.79174E-02   0.12028E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -65.637           22.88        -0.18672        -0.11524
v  Velocity[Y]                 -38.276           60.91         0.54575         0.36474
v  Velocity[Z]                 -40.254          24.894        0.078153       -0.018827
v  ǁVelocityǁ                 0.010739          78.325          1.4695          1.1476
v  Pressure                    -8650.2           30720           12471            8830
v  turbulent_viscosity      9.1913e-05          7.1505        0.079799        0.051135
v  CourantNb                   0.10985           78562          408.32          255.55
v  FourierNb                    7.1075           59040          177.19          87.173
v  total_pressure           4.9135e+05      5.3072e+05      5.1247e+05      5.0883e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.376       1.131e+05          585.51          342.72


 TIME FOR THE TIME STEP               75:        0.38595E+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        -0.183002582E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285173E+00
Free inlet               13           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 0.51295E+02
   Friction velocity        uet   :  0.78274E-02 0.48221E+01
   Friction velocity        uk    :  0.78274E-02 0.48221E+01
   Dimensionless distance   yplus :  0.12734E+00 0.50006E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2372
   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    0.12955E+02    2467   0.99776E+00   0.50864E+00 
c  VelocityY    0.12955E+02    2467   0.99776E+00   0.00000E+00 
c  VelocityZ    0.12955E+02    2467   0.99776E+00   0.00000E+00 
c  Pressure     0.10516E+01     604   0.79802E-02   0.12101E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -70.886          25.033        -0.21034        -0.11955
v  Velocity[Y]                   -42.5          66.581         0.56876         0.37183
v  Velocity[Z]                  -41.95          26.012        0.061015       -0.019181
v  ǁVelocityǁ                0.0033006          85.028          1.5378          1.2111
v  Pressure                    -9502.4           32448           12976          9174.8
v  turbulent_viscosity       9.589e-05          7.9988        0.084877        0.053895
v  CourantNb                   0.30167           85579          420.38          260.86
v  FourierNb                    7.1433           73244          185.62          90.589
v  total_pressure            4.905e+05      5.3245e+05      5.1298e+05      5.0917e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.7003      1.2478e+05             606          351.45


 TIME FOR THE TIME STEP               76:        0.46656E+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        -0.288225939E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285175E+00
Free inlet               13           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 0.55819E+02
   Friction velocity        uet   :  0.16534E-01 0.51753E+01
   Friction velocity        uk    :  0.16534E-01 0.51753E+01
   Dimensionless distance   yplus :  0.16546E+00 0.53338E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2327
   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    0.18241E+02    2318   0.99897E+00   0.46044E+00 
c  VelocityY    0.18241E+02    2318   0.99897E+00   0.00000E+00 
c  VelocityZ    0.18241E+02    2318   0.99897E+00   0.00000E+00 
c  Pressure     0.11093E+01     609   0.78928E-02   0.12033E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -75.063          26.094        -0.19143        -0.11739
v  Velocity[Y]                 -43.799          69.041         0.57579         0.37952
v  Velocity[Z]                 -45.276          28.363        0.053387       -0.021394
v  ǁVelocityǁ                 0.007773          89.551           1.564           1.217
v  Pressure                     -10362           34247           13530          9553.1
v  turbulent_viscosity      8.8448e-05          8.6862        0.088059        0.056101
v  CourantNb                  0.054369           95345          439.71          274.05
v  FourierNb                     7.318           71561          189.89          92.913
v  total_pressure           4.8964e+05      5.3425e+05      5.1353e+05      5.0955e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.069      1.3748e+05           629.6          366.96


 TIME FOR THE TIME STEP               77:        0.38469E+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        -0.228448459E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285583E+00
Free inlet               13           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 0.62125E+02
   Friction velocity        uet   :  0.12565E-01 0.56504E+01
   Friction velocity        uk    :  0.12565E-01 0.56504E+01
   Dimensionless distance   yplus :  0.10748E+00 0.56097E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2265
   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    0.16658E+02    2515   0.99793E+00   0.62439E+00 
c  VelocityY    0.16658E+02    2515   0.99793E+00   0.00000E+00 
c  VelocityZ    0.16658E+02    2515   0.99793E+00   0.00000E+00 
c  Pressure     0.11886E+01     614   0.80292E-02   0.12153E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -79.403          28.554         -0.2317        -0.12661
v  Velocity[Y]                 -48.451          75.527         0.62473         0.38516
v  Velocity[Z]                 -47.364          29.987        0.065312        -0.02085
v  ǁVelocityǁ                0.0052353           95.79          1.6797          1.2998
v  Pressure                     -11316           36227           14136          9968.9
v  turbulent_viscosity      0.00012087          9.6648         0.09289        0.058545
v  CourantNb                    0.1026      1.0436e+05          454.47          281.11
v  FourierNb                    7.2026           81573          198.15          96.189
v  total_pressure           4.8868e+05      5.3623e+05      5.1414e+05      5.0997e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          9.4145      1.5383e+05          652.62           377.3


 TIME FOR THE TIME STEP               78:        0.41475E+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        -0.284874286E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285634E+00
Free inlet               13           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 0.67633E+02
   Friction velocity        uet   :  0.13734E-01 0.60596E+01
   Friction velocity        uk    :  0.13734E-01 0.60596E+01
   Dimensionless distance   yplus :  0.22037E+00 0.58912E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2184
   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    0.23343E+02    2334   0.99783E+00   0.80394E+00 
c  VelocityY    0.23343E+02    2334   0.99783E+00   0.00000E+00 
c  VelocityZ    0.23343E+02    2334   0.99783E+00   0.00000E+00 
c  Pressure     0.12502E+01     605   0.78716E-02   0.12048E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -84.694          29.479        -0.20881        -0.12462
v  Velocity[Y]                 -49.824          78.306         0.60154          0.3968
v  Velocity[Z]                 -50.788          30.971        0.061202       -0.024713
v  ǁVelocityǁ                 0.015267          101.02          1.7032          1.3034
v  Pressure                     -12309           38224           14747           10386
v  turbulent_viscosity      9.0589e-05          10.498        0.097867        0.061735
v  CourantNb                   0.28844      1.1597e+05          485.96          298.85
v  FourierNb                    7.2448           86087           205.6          99.732
v  total_pressure           4.8769e+05      5.3822e+05      5.1475e+05      5.1039e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.084      1.6578e+05          691.56          398.58


 TIME FOR THE TIME STEP               79:        0.44874E+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        -0.176880881E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285676E+00
Free inlet               13           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 0.75501E+02
   Friction velocity        uet   :  0.24548E-01 0.66360E+01
   Friction velocity        uk    :  0.24548E-01 0.66360E+01
   Dimensionless distance   yplus :  0.29082E+00 0.62096E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2139
   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    0.21207E+02    3024   0.99851E+00   0.93169E+00 
c  VelocityY    0.21207E+02    3024   0.99851E+00   0.00000E+00 
c  VelocityZ    0.21207E+02    3024   0.99851E+00   0.00000E+00 
c  Pressure     0.13391E+01     614   0.79523E-02   0.12158E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -89.81          32.798        -0.24164        -0.13049
v  Velocity[Y]                 -55.354          84.773         0.64748         0.40406
v  Velocity[Z]                 -52.938          33.973        0.049782       -0.023392
v  ǁVelocityǁ                 0.016264          108.61          1.8128           1.391
v  Pressure                     -13530           40440           15420           10849
v  turbulent_viscosity      0.00010119          11.704         0.10431        0.065056
v  CourantNb                   0.22882      1.2698e+05          500.23          305.84
v  FourierNb                    7.2274           99075          216.52          104.04
v  total_pressure           4.8647e+05      5.4044e+05      5.1542e+05      5.1085e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.414      1.8345e+05          716.74          409.88


 TIME FOR THE TIME STEP               80:        0.49020E+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        -0.335447072E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273285972E+00
Free inlet               13           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 0.82602E+02
   Friction velocity        uet   :  0.24610E-01 0.71487E+01
   Friction velocity        uk    :  0.24610E-01 0.71487E+01
   Dimensionless distance   yplus :  0.26555E+00 0.65502E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       2062
   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    0.31142E+02    2422   0.99671E+00   0.10539E+01 
c  VelocityY    0.31142E+02    2422   0.99671E+00   0.00000E+00 
c  VelocityZ    0.31142E+02    2422   0.99671E+00   0.00000E+00 
c  Pressure     0.14129E+01     614   0.79242E-02   0.12092E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -97.326          33.748        -0.21043        -0.12999
v  Velocity[Y]                 -56.898          90.632           0.638         0.41202
v  Velocity[Z]                 -57.389          35.729         0.05007       -0.026579
v  ǁVelocityǁ                 0.013304           115.9          1.8442          1.4058
v  Pressure                     -14820           42737           16142           11341
v  turbulent_viscosity      8.1688e-05          12.722         0.10854        0.067703
v  CourantNb                   0.80356      1.4122e+05          530.57          324.53
v  FourierNb                    7.2798      1.0424e+05          222.74          107.03
v  total_pressure           4.8518e+05      5.4274e+05      5.1614e+05      5.1134e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.761      2.0133e+05          753.31          431.56


 TIME FOR THE TIME STEP               81:        0.39743E+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        -0.330620921E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273286141E+00
Free inlet               13           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 0.91746E+02
   Friction velocity        uet   :  0.25155E-01 0.78000E+01
   Friction velocity        uk    :  0.25155E-01 0.78000E+01
   Dimensionless distance   yplus :  0.27569E+00 0.70539E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1984
   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    0.26822E+02    3166   0.99727E+00   0.19588E+01 
c  VelocityY    0.26822E+02    3166   0.99727E+00   0.00000E+00 
c  VelocityZ    0.26822E+02    3166   0.99727E+00   0.00000E+00 
c  Pressure     0.15188E+01     613   0.79571E-02   0.12245E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -103.48           37.18        -0.25644        -0.13743
v  Velocity[Y]                 -63.647          99.106         0.68726         0.42232
v  Velocity[Z]                 -60.913          37.884        0.029092       -0.024143
v  ǁVelocityǁ                0.0056544          124.88          2.0085          1.5468
v  Pressure                     -16235           45227           16874           11841
v  turbulent_viscosity      0.00012252          14.152         0.11579        0.071701
v  CourantNb                   0.16119      1.5435e+05          548.36          334.21
v  FourierNb                    7.2169      1.1917e+05          234.62          111.94
v  total_pressure           4.8377e+05      5.4523e+05      5.1687e+05      5.1184e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.398      2.2292e+05          782.98          446.15


 TIME FOR THE TIME STEP               82:        0.60201E+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         0.359564096E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273286240E+00
Free inlet               13           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 0.10054E+03
   Friction velocity        uet   :  0.16957E-01 0.84174E+01
   Friction velocity        uk    :  0.16957E-01 0.84174E+01
   Dimensionless distance   yplus :  0.18980E+00 0.76123E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1896
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.39240E+02    2448   0.99834E+00   0.19978E+01 
c  VelocityY    0.39240E+02    2448   0.99834E+00   0.00000E+00 
c  VelocityZ    0.39240E+02    2448   0.99834E+00   0.00000E+00 
c  Pressure     0.15969E+01     605   0.78385E-02   0.12125E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -110.31           38.35        -0.25926        -0.13327
v  Velocity[Y]                 -65.065           109.8         0.67001         0.43365
v  Velocity[Z]                 -64.432          41.051        0.035384       -0.030387
v  ǁVelocityǁ                0.0094677          131.76          2.0402           1.522
v  Pressure                     -17709           47817           17643           12366
v  turbulent_viscosity      9.2331e-05          15.435         0.12069        0.075164
v  CourantNb                   0.52083      1.7134e+05          589.11          360.47
v  FourierNb                    7.3373      1.2625e+05          241.59          115.56
v  total_pressure           4.8229e+05      5.4782e+05      5.1764e+05      5.1237e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.164      2.4341e+05           830.7          476.03


 TIME FOR THE TIME STEP               83:        0.47065E+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        -0.119099276E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273286475E+00
Free inlet               13           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 0.11197E+03
   Friction velocity        uet   :  0.32174E-01 0.92098E+01
   Friction velocity        uk    :  0.32174E-01 0.92098E+01
   Dimensionless distance   yplus :  0.25534E+00 0.83289E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1880
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.34729E+02    3022   0.99700E+00   0.20303E+01 
c  VelocityY    0.34729E+02    3022   0.99700E+00   0.00000E+00 
c  VelocityZ    0.34729E+02    3022   0.99700E+00   0.00000E+00 
c  Pressure     0.17138E+01     604   0.79565E-02   0.12252E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -118.66          42.722          -0.305        -0.14929
v  Velocity[Y]                 -72.582          119.33         0.71337         0.43756
v  Velocity[Z]                 -67.176          44.044       0.0017931       -0.029921
v  ǁVelocityǁ                0.0020146             143          2.1973          1.6659
v  Pressure                     -19332           50650           18484           12940
v  turbulent_viscosity       0.0001183          17.091         0.12977        0.079466
v  CourantNb                 0.0031037      1.8661e+05           611.3          367.09
v  FourierNb                    7.1899      1.4419e+05          257.34          121.48
v  total_pressure           4.8067e+05      5.5065e+05      5.1848e+05      5.1294e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.972      2.6855e+05          868.64          488.57


 TIME FOR THE TIME STEP               84:        0.48941E+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         0.100097284E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273288913E+00
Free inlet               13           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 0.12195E+03
   Friction velocity        uet   :  0.25934E-01 0.98922E+01
   Friction velocity        uk    :  0.25934E-01 0.98922E+01
   Dimensionless distance   yplus :  0.26739E+00 0.89460E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1807
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.50182E+02    2524   0.99794E+00   0.20137E+01 
c  VelocityY    0.50182E+02    2524   0.99794E+00   0.00000E+00 
c  VelocityZ    0.50182E+02    2524   0.99794E+00   0.00000E+00 
c  Pressure     0.18033E+01     613   0.78480E-02   0.12144E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -125.22          43.702        -0.24149         -0.1394
v  Velocity[Y]                 -74.133          131.91         0.69455         0.45013
v  Velocity[Z]                 -73.452          45.183     -0.00062218       -0.036186
v  ǁVelocityǁ                 0.013031          149.46          2.2224          1.6517
v  Pressure                     -21023           53575           19383           13554
v  turbulent_viscosity      8.6321e-05          18.597         0.13525        0.083488
v  CourantNb                   0.26199      2.0813e+05          652.57          394.21
v  FourierNb                    7.3529      1.5207e+05          264.94          125.59
v  total_pressure           4.7898e+05      5.5358e+05      5.1938e+05      5.1355e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.747       2.948e+05          917.51           519.8


 TIME FOR THE TIME STEP               85:        0.41021E+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         0.156492666E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273286986E+00
Free inlet               13           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 0.13556E+03
   Friction velocity        uet   :  0.33784E-01 0.10811E+02
   Friction velocity        uk    :  0.33784E-01 0.10811E+02
   Dimensionless distance   yplus :  0.24518E+00 0.97769E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1704
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.45825E+02    3200   0.99642E+00   0.22269E+01 
c  VelocityY    0.45825E+02    3200   0.99642E+00   0.00000E+00 
c  VelocityZ    0.45825E+02    3200   0.99642E+00   0.00000E+00 
c  Pressure     0.19413E+01     604   0.79517E-02   0.12309E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -134.95           48.18        -0.32514        -0.15599
v  Velocity[Y]                  -82.56          139.34         0.76818         0.46068
v  Velocity[Z]                 -76.278          49.992      -0.0065726       -0.031083
v  ǁVelocityǁ                 0.023269          162.58          2.3623          1.7812
v  Pressure                     -22894           56774           20335           14208
v  turbulent_viscosity      0.00017825          20.671         0.14427        0.087801
v  CourantNb                   0.57639      2.2642e+05          672.52          402.05
v  FourierNb                    7.8011      1.7367e+05          280.63          131.64
v  total_pressure           4.7711e+05      5.5677e+05      5.2034e+05      5.1421e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           13.77      3.2551e+05          953.14          533.69


 TIME FOR THE TIME STEP               86:        0.59430E+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        -0.413395171E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273289812E+00
Free inlet               13           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 0.14339E+03
   Friction velocity        uet   :  0.26113E-01 0.11333E+02
   Friction velocity        uk    :  0.26113E-01 0.11333E+02
   Dimensionless distance   yplus :  0.27064E+00 0.10249E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1629
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.65113E+02    2547   0.99723E+00   0.28223E+01 
c  VelocityY    0.65113E+02    2547   0.99723E+00   0.00000E+00 
c  VelocityZ    0.65113E+02    2547   0.99723E+00   0.00000E+00 
c  Pressure     0.20425E+01     614   0.78526E-02   0.12195E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -142.88          49.615        -0.27994        -0.15032
v  Velocity[Y]                 -84.566          159.24         0.75726         0.46932
v  Velocity[Z]                 -82.576          52.092       0.0080521       -0.037524
v  ǁVelocityǁ                 0.013334          170.59          2.4458          1.7983
v  Pressure                     -24821           60105           21383           14925
v  turbulent_viscosity      0.00011499          22.126          0.1499        0.092065
v  CourantNb                   0.22234      2.5242e+05          711.56          427.56
v  FourierNb                    7.4083      1.7944e+05          288.32          135.84
v  total_pressure           4.7518e+05       5.601e+05      5.2138e+05      5.1493e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          16.271      3.6132e+05          999.88           563.4


 TIME FOR THE TIME STEP               87:        0.42508E+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         0.172710551E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273287675E+00
Free inlet               13           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 0.16469E+03
   Friction velocity        uet   :  0.19935E-01 0.12737E+02
   Friction velocity        uk    :  0.19935E-01 0.12737E+02
   Dimensionless distance   yplus :  0.34445E+00 0.11519E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1597
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.57341E+02    3364   0.99458E+00   0.39841E+01 
c  VelocityY    0.57341E+02    3364   0.99458E+00   0.00000E+00 
c  VelocityZ    0.57341E+02    3364   0.99458E+00   0.00000E+00 
c  Pressure     0.21975E+01     593   0.79032E-02   0.12349E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -153.11          55.178        -0.35224        -0.16832
v  Velocity[Y]                 -94.276          166.42         0.84571         0.48465
v  Velocity[Z]                  -85.22          55.261       -0.014695        -0.03586
v  ǁVelocityǁ                 0.013575          184.63          2.6931          2.0175
v  Pressure                     -26984           63676           22408           15623
v  turbulent_viscosity       0.0001728          25.103         0.16324        0.098639
v  CourantNb                    0.1436      2.7564e+05          746.93          442.86
v  FourierNb                    7.2566      2.1067e+05          311.65          144.58
v  total_pressure           4.7302e+05      5.6368e+05      5.2241e+05      5.1562e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          16.583      3.9811e+05          1058.6          587.44


 TIME FOR THE TIME STEP               88:        0.52444E+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         0.100658365E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273289777E+00
Free inlet               13           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 0.17250E+03
   Friction velocity        uet   :  0.26044E-01 0.13246E+02
   Friction velocity        uk    :  0.26044E-01 0.13246E+02
   Dimensionless distance   yplus :  0.31048E+00 0.11979E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1452
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.84496E+02    2628   0.99663E+00   0.54375E+01 
c  VelocityY    0.84496E+02    2628   0.99663E+00   0.00000E+00 
c  VelocityZ    0.84496E+02    2628   0.99663E+00   0.00000E+00 
c  Pressure     0.23073E+01     621   0.78256E-02   0.12202E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -163.73          56.999        -0.31372         -0.1544
v  Velocity[Y]                 -95.886           185.5         0.84813         0.49243
v  Velocity[Z]                  -91.22          60.552       -0.026587        -0.04622
v  ǁVelocityǁ                 0.021493          194.96          2.7228          1.9662
v  Pressure                     -29125           67538           23598           16439
v  turbulent_viscosity      7.6702e-05          26.574         0.16953          0.1039
v  CourantNb                    0.3848      3.0735e+05          809.55          482.23
v  FourierNb                    7.7102      2.3292e+05          319.77          149.52
v  total_pressure           4.7088e+05      5.6754e+05       5.236e+05      5.1644e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          18.804      4.3352e+05          1129.3          631.75


 TIME FOR THE TIME STEP               89:        0.44013E+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        -0.225120340E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273288914E+00
Free inlet               13           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 0.19302E+03
   Friction velocity        uet   :  0.24627E-01 0.14568E+02
   Friction velocity        uk    :  0.24627E-01 0.14568E+02
   Dimensionless distance   yplus :  0.32343E+00 0.13175E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1456
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.73875E+02    3516   0.99323E+00   0.56487E+01 
c  VelocityY    0.73875E+02    3516   0.99323E+00   0.00000E+00 
c  VelocityZ    0.73875E+02    3516   0.99323E+00   0.00000E+00 
c  Pressure     0.24878E+01     605   0.78698E-02   0.12377E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -174.57          62.387         -0.3993        -0.17623
v  Velocity[Y]                 -107.71          200.15          0.8591         0.50553
v  Velocity[Z]                 -95.339          64.534       -0.059335       -0.041292
v  ǁVelocityǁ                 0.012286          210.65          2.9217          2.1517
v  Pressure                     -31534           71689           24829           17284
v  turbulent_viscosity      0.00030167          29.915          0.1826         0.10939
v  CourantNb                   0.51384      3.3338e+05          837.54          490.49
v  FourierNb                    7.3142      2.6773e+05           343.7          157.96
v  total_pressure           4.6847e+05      5.7169e+05      5.2483e+05      5.1728e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          14.275      4.8279e+05          1181.2          648.45


 TIME FOR THE TIME STEP               90:        0.59619E+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        -0.804910535E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273291604E+00
Free inlet               13           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 0.20858E+03
   Friction velocity        uet   :  0.28407E-01 0.15558E+02
   Friction velocity        uk    :  0.28407E-01 0.15558E+02
   Dimensionless distance   yplus :  0.30926E+00 0.14070E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1365
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10883E+03    2675   0.99614E+00   0.57348E+01 
c  VelocityY    0.10883E+03    2675   0.99614E+00   0.00000E+00 
c  VelocityZ    0.10883E+03    2675   0.99614E+00   0.00000E+00 
c  Pressure     0.26171E+01     594   0.77889E-02   0.12258E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -184.71          64.138        -0.28069        -0.17316
v  Velocity[Y]                 -109.15          221.83         0.80922         0.52992
v  Velocity[Z]                 -103.92          72.254       -0.029551       -0.046543
v  ǁVelocityǁ                 0.033216          223.02          2.9478          2.1613
v  Pressure                     -34139           75864           26060           18121
v  turbulent_viscosity      0.00014274          32.235         0.18902         0.11423
v  CourantNb                   0.57225      3.7086e+05          893.36          526.65
v  FourierNb                    7.5329      2.5996e+05          352.41           162.8
v  total_pressure           4.6586e+05      5.7586e+05      5.2606e+05      5.1812e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          17.433      5.2297e+05          1245.8          689.45


 TIME FOR THE TIME STEP               91:        0.50218E+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        -0.269906380E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273291538E+00
Free inlet               13           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 0.23233E+03
   Friction velocity        uet   :  0.23192E-01 0.17052E+02
   Friction velocity        uk    :  0.23192E-01 0.17052E+02
   Dimensionless distance   yplus :  0.15985E+00 0.15421E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1375
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.99415E+02    3691   0.99372E+00   0.84086E+01 
c  VelocityY    0.99415E+02    3691   0.99372E+00   0.00000E+00 
c  VelocityZ    0.99415E+02    3691   0.99372E+00   0.00000E+00 
c  Pressure     0.28179E+01     604   0.78758E-02   0.12411E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -197.35          72.334        -0.44799        -0.18873
v  Velocity[Y]                 -122.87          240.35         0.92689            0.54
v  Velocity[Z]                  -109.8          76.334         -0.1109       -0.038175
v  ǁVelocityǁ                 0.016888          241.17          3.2496          2.3831
v  Pressure                     -36914           80508           27404           19041
v  turbulent_viscosity      0.00054275          35.847         0.20439         0.12254
v  CourantNb                   0.19105      4.0285e+05          913.27          538.41
v  FourierNb                    7.4693      3.2171e+05          378.21          173.32
v  total_pressure           4.6309e+05      5.8051e+05       5.274e+05      5.1904e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          13.676      5.8076e+05          1291.5          711.73


 TIME FOR THE TIME STEP               92:        0.60605E+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        -0.492247877E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273292848E+00
Free inlet               13           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 0.25191E+03
   Friction velocity        uet   :  0.23042E-01 0.18269E+02
   Friction velocity        uk    :  0.23042E-01 0.18269E+02
   Dimensionless distance   yplus :  0.36100E+00 0.16522E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1175
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.13743E+03    2752   0.99578E+00   0.11917E+02 
c  VelocityY    0.13743E+03    2752   0.99578E+00   0.00000E+00 
c  VelocityZ    0.13743E+03    2752   0.99578E+00   0.00000E+00 
c  Pressure     0.29688E+01     593   0.78646E-02   0.12309E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -211.22           74.12        -0.48858         -0.1796
v  Velocity[Y]                 -124.95          264.14         0.93103         0.55808
v  Velocity[Z]                 -116.62          87.813        -0.11018       -0.056298
v  ǁVelocityǁ                 0.014872          265.64          3.6623          2.5051
v  Pressure                     -39870           85297           28775           19964
v  turbulent_viscosity      0.00017978          38.795         0.21417         0.12871
v  CourantNb                   0.33606       4.502e+05          996.42          584.77
v  FourierNb                    7.7594      3.1211e+05          393.03          180.19
v  total_pressure           4.6013e+05       5.853e+05      5.2877e+05      5.1996e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.318      6.3117e+05          1389.4          764.96


 TIME FOR THE TIME STEP               93:        0.44334E+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        -0.604164090E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273292112E+00
Free inlet               13           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 0.27817E+03
   Friction velocity        uet   :  0.34090E-01 0.19883E+02
   Friction velocity        uk    :  0.34090E-01 0.19883E+02
   Dimensionless distance   yplus :  0.33471E+00 0.17982E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1042
   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    0.12437E+03    3610   0.99316E+00   0.81049E+01 
c  VelocityY    0.12437E+03    3610   0.99316E+00   0.00000E+00 
c  VelocityZ    0.12437E+03    3610   0.99316E+00   0.00000E+00 
c  Pressure     0.31918E+01     613   0.78427E-02   0.12444E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -225.43          80.639        -0.50022        -0.20092
v  Velocity[Y]                 -139.49          287.41         0.95263          0.5717
v  Velocity[Z]                 -123.12          92.078        -0.16639       -0.054974
v  ǁVelocityǁ                0.0060373          288.46          3.3994          2.4017
v  Pressure                     -42996           90614           30288           21000
v  turbulent_viscosity      0.00054702          42.966         0.23954         0.14158
v  CourantNb                    1.5915      4.8758e+05          1118.7           630.5
v  FourierNb                    8.2888      3.5553e+05          436.34          196.76
v  total_pressure             4.57e+05      5.9061e+05      5.3029e+05        5.21e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          18.412      7.0144e+05          1555.1          827.26


 TIME FOR THE TIME STEP               94:        0.65817E+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         0.551766487E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273290053E+00
Free inlet               13           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 0.30305E+03
   Friction velocity        uet   :  0.17293E-01 0.21395E+02
   Friction velocity        uk    :  0.17293E-01 0.21395E+02
   Dimensionless distance   yplus :  0.14780E+00 0.19348E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1054
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.17888E+03    3092   0.99481E+00   0.10629E+02 
c  VelocityY    0.17888E+03    3092   0.99481E+00   0.00000E+00 
c  VelocityZ    0.17888E+03    3092   0.99481E+00   0.00000E+00 
c  Pressure     0.33679E+01     604   0.78039E-02   0.12357E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -240.89          82.645        -0.38647        -0.19819
v  Velocity[Y]                 -145.11             318         0.70045         0.59467
v  Velocity[Z]                 -130.34          103.89        -0.10848       -0.069322
v  ǁVelocityǁ                 0.018745          319.69          3.8887          2.7122
v  Pressure                     -46374           96010           31901           22083
v  turbulent_viscosity      0.00012128          46.772         0.23704         0.14079
v  CourantNb                   0.91031      5.4447e+05          1079.1          619.73
v  FourierNb                    7.6093      3.7558e+05          430.53          195.43
v  total_pressure           4.5363e+05      5.9601e+05       5.319e+05      5.2208e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          16.888      7.7065e+05          1509.7          815.17


 TIME FOR THE TIME STEP               95:        0.57364E+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        -0.616120695E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273294654E+00
Free inlet               13           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 0.33663E+03
   Friction velocity        uet   :  0.32089E-01 0.23411E+02
   Friction velocity        uk    :  0.32089E-01 0.23411E+02
   Dimensionless distance   yplus :  0.53417E+00 0.21172E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        926
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.16250E+03    3484   0.99213E+00   0.10614E+02 
c  VelocityY    0.16250E+03    3484   0.99213E+00   0.00000E+00 
c  VelocityZ    0.16250E+03    3484   0.99213E+00   0.00000E+00 
c  Pressure     0.36284E+01     619   0.78418E-02   0.12514E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -259.28          91.562        -0.51682        -0.21782
v  Velocity[Y]                 -159.63          344.25         0.89947         0.60683
v  Velocity[Z]                  -136.2           109.4        -0.13928       -0.052638
v  ǁVelocityǁ                 0.015256          345.44           3.851          2.6365
v  Pressure                     -49837      1.0217e+05           33740           23358
v  turbulent_viscosity       0.0010955          51.642         0.26772         0.15816
v  CourantNb                   0.15036      5.8935e+05          1202.5          683.85
v  FourierNb                    7.6584      4.6169e+05          482.97          216.57
v  total_pressure           4.5016e+05      6.0217e+05      5.3374e+05      5.2336e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.743      8.4563e+05          1685.5          900.41


 TIME FOR THE TIME STEP               96:        0.63640E+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        -0.649517437E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273292256E+00
Free inlet               13           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 0.36498E+03
   Friction velocity        uet   :  0.33294E-01 0.25094E+02
   Friction velocity        uk    :  0.33294E-01 0.25094E+02
   Dimensionless distance   yplus :  0.25095E+00 0.22694E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :       1019
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.23476E+03    3267   0.99364E+00   0.99785E+01 
c  VelocityY    0.23476E+03    3267   0.99364E+00   0.00000E+00 
c  VelocityZ    0.23476E+03    3267   0.99364E+00   0.00000E+00 
c  Pressure     0.38269E+01     596   0.78169E-02   0.12413E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -273.56          94.008        -0.36891        -0.22833
v  Velocity[Y]                 -175.78          380.37         0.80239         0.64561
v  Velocity[Z]                 -149.78          127.45        -0.19405       -0.082209
v  ǁVelocityǁ                0.0092754           382.7           4.302          3.0436
v  Pressure                     -53749       1.082e+05           35489           24531
v  turbulent_viscosity      0.00092802          56.014         0.27135         0.15968
v  CourantNb                   0.52047      6.5782e+05          1227.5          689.85
v  FourierNb                    7.7617      4.8645e+05          488.39          218.67
v  total_pressure           4.4625e+05       6.082e+05      5.3549e+05      5.2453e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          16.733      9.1889e+05          1715.9          908.52


 TIME FOR THE TIME STEP               97:        0.51192E+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        -0.131800174E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273295957E+00
Free inlet               13           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 0.40498E+03
   Friction velocity        uet   :  0.37462E-01 0.27442E+02
   Friction velocity        uk    :  0.37462E-01 0.27442E+02
   Dimensionless distance   yplus :  0.52863E+00 0.24818E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        731
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.21256E+03    3529   0.99040E+00   0.11326E+02 
c  VelocityY    0.21256E+03    3529   0.99040E+00   0.00000E+00 
c  VelocityZ    0.21256E+03    3529   0.99040E+00   0.00000E+00 
c  Pressure     0.41170E+01     613   0.77728E-02   0.12552E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -291.56          104.23        -0.63036        -0.24766
v  Velocity[Y]                 -190.79          414.92           1.068         0.65672
v  Velocity[Z]                 -154.43          132.65        -0.14497       -0.056631
v  ǁVelocityǁ                 0.036937          416.42          4.3886           2.974
v  Pressure                     -57803      1.1506e+05           37431           25877
v  turbulent_viscosity       0.0036295          62.005         0.30189         0.17938
v  CourantNb                   0.82274      7.0873e+05          1333.9          763.12
v  FourierNb                    9.3529      5.5296e+05          537.19          240.58
v  total_pressure            4.422e+05      6.1506e+05      5.3743e+05      5.2588e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          13.025      1.0325e+06          1871.1          1003.7


 TIME FOR THE TIME STEP               98:        0.63826E+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        -0.309545570E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273292484E+00
Free inlet               13           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 0.44194E+03
   Friction velocity        uet   :  0.31353E-01 0.29587E+02
   Friction velocity        uk    :  0.31353E-01 0.29587E+02
   Dimensionless distance   yplus :  0.36629E+00 0.26757E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        831
   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    0.30441E+03    3286   0.99228E+00   0.14140E+02 
c  VelocityY    0.30441E+03    3286   0.99228E+00   0.00000E+00 
c  VelocityZ    0.30441E+03    3286   0.99228E+00   0.00000E+00 
c  Pressure     0.43589E+01     614   0.78320E-02   0.12494E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -311.75          106.07        -0.43476        -0.24227
v  Velocity[Y]                 -210.43          456.98         0.77017         0.67627
v  Velocity[Z]                 -170.44          149.45        -0.15161       -0.078711
v  ǁVelocityǁ                 0.026384          459.44          5.0094           3.469
v  Pressure                     -62230      1.2195e+05           39520           27301
v  turbulent_viscosity      0.00075052          67.549         0.30463          0.1793
v  CourantNb                   0.48839      7.9247e+05          1396.8           779.5
v  FourierNb                    8.1755      5.4099e+05           541.8          242.05
v  total_pressure           4.3777e+05      6.2195e+05      5.3952e+05       5.273e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          11.104      1.1075e+06          1938.6          1021.6


 TIME FOR THE TIME STEP               99:        0.61366E+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        -0.771617528E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273292670E+00
Free inlet               13           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 0.48901E+03
   Friction velocity        uet   :  0.21912E-01 0.32289E+02
   Friction velocity        uk    :  0.21912E-01 0.32289E+02
   Dimensionless distance   yplus :  0.31174E+00 0.29201E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        739
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         17 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:    0.85285E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.28111E+03    3578   0.98679E+00   0.17364E+02 
c  VelocityY    0.28111E+03    3578   0.98679E+00   0.00000E+00 
c  VelocityZ    0.28111E+03    3578   0.98679E+00   0.00000E+00 
c  Pressure     0.46966E+01     617   0.77478E-02   0.12648E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -334.49          118.57        -0.59207        -0.25965
v  Velocity[Y]                 -231.12          496.92          1.1657         0.70898
v  Velocity[Z]                 -174.89          158.65        -0.12115       -0.054197
v  ǁVelocityǁ                 0.022861          498.71          4.8486          3.3069
v  Pressure                     -66740      1.2984e+05           41717           28825
v  turbulent_viscosity       0.0036851          74.935         0.34572         0.20238
v  CourantNb                   0.20969       8.584e+05          1547.8          872.74
v  FourierNb                    8.3384      6.1869e+05           611.1           269.9
v  total_pressure           4.3326e+05      6.2984e+05      5.4172e+05      5.2882e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          19.272      1.2265e+06          2158.9          1142.6


 TIME FOR THE TIME STEP              100:        0.62475E+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         0.431258805E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273294823E+00
Free inlet               13           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 0.53236E+03
   Friction velocity        uet   :  0.45526E-01 0.34750E+02
   Friction velocity        uk    :  0.45526E-01 0.34750E+02
   Dimensionless distance   yplus :  0.43623E+00 0.31427E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        667
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.40430E+03    3267   0.99027E+00   0.23651E+02 
c  VelocityY    0.40430E+03    3267   0.99027E+00   0.00000E+00 
c  VelocityZ    0.40430E+03    3267   0.99027E+00   0.00000E+00 
c  Pressure     0.49481E+01     593   0.77753E-02   0.12524E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -354.48          123.23        -0.50295        -0.27916
v  Velocity[Y]                 -253.74          550.98         0.98137         0.73799
v  Velocity[Z]                  -189.1          182.14        -0.29751         -0.1014
v  ǁVelocityǁ                 0.036953          554.14          5.6395          3.7944
v  Pressure                     -71975      1.3749e+05           43938           30305
v  turbulent_viscosity       0.0011026          81.384         0.34633         0.20164
v  CourantNb                   0.14512      9.5834e+05          1554.6          868.12
v  FourierNb                    7.2535      6.5184e+05          612.45          270.24
v  total_pressure           4.2802e+05      6.3749e+05      5.4394e+05      5.3031e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.028      1.3333e+06            2167          1138.4


 TIME FOR THE TIME STEP              101:        0.60355E+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        -0.777890592E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273297007E+00
Free inlet               13           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 0.59231E+03
   Friction velocity        uet   :  0.37027E-01 0.38116E+02
   Friction velocity        uk    :  0.37027E-01 0.38116E+02
   Dimensionless distance   yplus :  0.28739E+00 0.34470E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        660
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.37522E+03    3892   0.98545E+00   0.27490E+02 
c  VelocityY    0.37522E+03    3892   0.98545E+00   0.00000E+00 
c  VelocityZ    0.37522E+03    3892   0.98545E+00   0.00000E+00 
c  Pressure     0.53240E+01     618   0.77913E-02   0.12655E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -377.7          138.13        -0.82057        -0.29601
v  Velocity[Y]                 -276.61          597.81          1.1486         0.75259
v  Velocity[Z]                 -199.63          192.56        -0.38564       -0.053161
v  ǁVelocityǁ                  0.02807          600.05          5.8118          3.8748
v  Pressure                     -77105      1.4643e+05           46582           32164
v  turbulent_viscosity       0.0018059           90.32         0.38843         0.22627
v  CourantNb                   0.66498      1.0316e+06          1750.8          969.98
v  FourierNb                    8.0361      8.0241e+05           681.2          299.16
v  total_pressure            4.229e+05      6.4643e+05      5.4658e+05      5.3216e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          13.335       1.463e+06            2432          1269.1


 TIME FOR THE TIME STEP              102:        0.66825E+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        -0.124279745E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273295919E+00
Free inlet               13           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 0.64326E+03
   Friction velocity        uet   :  0.37934E-01 0.40945E+02
   Friction velocity        uk    :  0.37934E-01 0.40945E+02
   Dimensionless distance   yplus :  0.40698E+00 0.37029E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        528
   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    0.52900E+03    3354   0.98854E+00   0.31427E+02 
c  VelocityY    0.52900E+03    3354   0.98854E+00   0.00000E+00 
c  VelocityZ    0.52900E+03    3354   0.98854E+00   0.00000E+00 
c  Pressure     0.56295E+01     591   0.77727E-02   0.12573E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -400.75          135.97        -0.58544        -0.31632
v  Velocity[Y]                 -304.24          661.93          1.1297         0.79693
v  Velocity[Z]                 -213.59          221.64        -0.23656        -0.10181
v  ǁVelocityǁ                 0.018944          665.92          6.4945          4.4034
v  Pressure                     -83051      1.5506e+05           48975           33753
v  turbulent_viscosity       0.0017457          97.813         0.40001         0.23207
v  CourantNb                    1.2109      1.1516e+06            1841          1008.9
v  FourierNb                    9.1258      8.4737e+05          702.34          306.95
v  total_pressure           4.1695e+05      6.5506e+05      5.4898e+05      5.3375e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          17.893      1.6209e+06          2543.3          1315.9


 TIME FOR THE TIME STEP              103:        0.57600E+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         0.796128305E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273298890E+00
Free inlet               13           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 0.71519E+03
   Friction velocity        uet   :  0.30932E-01 0.44897E+02
   Friction velocity        uk    :  0.30932E-01 0.44897E+02
   Dimensionless distance   yplus :  0.59442E+00 0.40603E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        549
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.49981E+03    3957   0.98312E+00   0.27656E+02 
c  VelocityY    0.49981E+03    3957   0.98312E+00   0.00000E+00 
c  VelocityZ    0.49981E+03    3957   0.98312E+00   0.00000E+00 
c  Pressure     0.60596E+01     605   0.77273E-02   0.12707E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -430.55          156.47        -0.88201        -0.32499
v  Velocity[Y]                 -332.53          718.25          1.2969         0.81229
v  Velocity[Z]                  -222.4          228.56        -0.35075       -0.073435
v  ǁVelocityǁ                 0.021489          720.74           6.493          4.2892
v  Pressure                     -89156      1.6494e+05           51826           35729
v  turbulent_viscosity       0.0031611          108.32         0.44455         0.25941
v  CourantNb                   0.86369      1.2418e+06          2007.2          1114.3
v  FourierNb                    8.7112       9.663e+05          775.12           338.2
v  total_pressure           4.1084e+05      6.6494e+05      5.5183e+05      5.3573e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          12.475      1.7607e+06          2782.3          1452.5


 TIME FOR THE TIME STEP              104:        0.66677E+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        -0.142323497E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273303892E+00
Free inlet               13           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 0.77622E+03
   Friction velocity        uet   :  0.28860E-01 0.48215E+02
   Friction velocity        uk    :  0.28860E-01 0.48215E+02
   Dimensionless distance   yplus :  0.45928E+00 0.43603E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        498
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         18 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.70555E+03    3353   0.98641E+00   0.41997E+02 
c  VelocityY    0.70555E+03    3353   0.98641E+00   0.00000E+00 
c  VelocityZ    0.70555E+03    3353   0.98641E+00   0.00000E+00 
c  Pressure     0.64349E+01     619   0.79179E-02   0.12674E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -459.37          154.85        -0.71978        -0.33212
v  Velocity[Y]                 -365.69          790.76         0.82227         0.83693
v  Velocity[Z]                 -242.74          268.41        -0.30298        -0.13376
v  ǁVelocityǁ                  0.02794          796.07          7.6058          5.1002
v  Pressure                     -95576      1.7513e+05           55183           38010
v  turbulent_viscosity       0.0014124          117.44         0.45512         0.26208
v  CourantNb                    1.0191      1.3922e+06          2069.9          1126.7
v  FourierNb                    9.1862      9.3954e+05          796.07          344.47
v  total_pressure           4.0442e+05      6.7513e+05      5.5518e+05      5.3801e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          20.167      1.9541e+06            2866          1471.1


 TIME FOR THE TIME STEP              105:        0.58274E+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        -0.721081067E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273299560E+00
Free inlet               13           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 0.85783E+03
   Friction velocity        uet   :  0.23851E-01 0.52606E+02
   Friction velocity        uk    :  0.23851E-01 0.52606E+02
   Dimensionless distance   yplus :  0.46595E+00 0.47574E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        530
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.66892E+03    3969   0.97930E+00   0.47848E+02 
c  VelocityY    0.66892E+03    3969   0.97930E+00   0.00000E+00 
c  VelocityZ    0.66892E+03    3969   0.97930E+00   0.00000E+00 
c  Pressure     0.69205E+01     592   0.77035E-02   0.12798E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -486.88          178.95         -0.8947        -0.37011
v  Velocity[Y]                 -399.95          861.18           1.352         0.89521
v  Velocity[Z]                 -250.94          277.39        -0.24497       -0.080786
v  ǁVelocityǁ                0.0073749          864.59          7.1601          4.7934
v  Pressure                -1.0264e+05      1.8613e+05           58089           39996
v  turbulent_viscosity       0.0043735          129.79         0.51877         0.30299
v  CourantNb                    1.8032      1.4873e+06          2332.2          1282.7
v  FourierNb                    8.4906      1.1521e+06          899.17          389.72
v  total_pressure           3.9736e+05      6.8613e+05      5.5809e+05         5.4e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          17.803      2.1148e+06          3231.4          1672.5


 TIME FOR THE TIME STEP              106:        0.63179E+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        -0.171010703E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273304560E+00
Free inlet               13           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 0.93503E+03
   Friction velocity        uet   :  0.32470E-01 0.56717E+02
   Friction velocity        uk    :  0.32470E-01 0.56717E+02
   Dimensionless distance   yplus :  0.42128E+00 0.51292E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        376
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.93798E+03    3448   0.98411E+00   0.57721E+02 
c  VelocityY    0.93798E+03    3448   0.98411E+00   0.00000E+00 
c  VelocityZ    0.93798E+03    3448   0.98411E+00   0.00000E+00 
c  Pressure     0.73101E+01     593   0.77595E-02   0.12687E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -518.37           180.6        -0.83092        -0.38328
v  Velocity[Y]                  -437.6          953.87          1.4302         0.93356
v  Velocity[Z]                 -270.67          319.89        -0.32513        -0.15831
v  ǁVelocityǁ                 0.044268           959.8          8.4716          5.5715
v  Pressure                -1.1033e+05      1.9723e+05           61253           42099
v  turbulent_viscosity       0.0036527          141.48         0.51096         0.29608
v  CourantNb                    1.4853      1.6722e+06          2296.7          1251.8
v  FourierNb                    8.3628      1.1313e+06          887.11          383.77
v  total_pressure           3.8967e+05      6.9723e+05      5.6125e+05       5.421e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          18.684      2.3496e+06          3183.8          1635.6


 TIME FOR THE TIME STEP              107:        0.56471E+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        -0.729189330E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273303415E+00
Free inlet               13           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 0.10390E+04
   Friction velocity        uet   :  0.39679E-01 0.62195E+02
   Friction velocity        uk    :  0.39679E-01 0.62195E+02
   Dimensionless distance   yplus :  0.48390E+00 0.56247E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        415
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.90405E+03    4077   0.97621E+00   0.61407E+02 
c  VelocityY    0.90405E+03    4077   0.97621E+00   0.00000E+00 
c  VelocityZ    0.90405E+03    4077   0.97621E+00   0.00000E+00 
c  Pressure     0.78851E+01     617   0.77025E-02   0.12840E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -560.55          198.63         -1.1408        -0.40731
v  Velocity[Y]                  -481.5          1032.5            1.48         0.95314
v  Velocity[Z]                 -286.19          330.84        -0.41416       -0.091413
v  ǁVelocityǁ                 0.023673          1036.4          8.2561          5.3149
v  Pressure                -1.1805e+05      2.1018e+05           64954           44686
v  turbulent_viscosity       0.0042438          156.54         0.57369         0.33358
v  CourantNb                    0.2247      1.7973e+06          2620.7          1418.5
v  FourierNb                    9.0833      1.3921e+06          990.42          427.26
v  total_pressure           3.8195e+05      7.1018e+05      5.6495e+05      5.4469e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          17.041      2.5425e+06          3611.1          1845.7


 TIME FOR THE TIME STEP              108:        0.62704E+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         0.295826925E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273301056E+00
Free inlet               13           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 0.11258E+04
   Friction velocity        uet   :  0.39388E-01 0.66720E+02
   Friction velocity        uk    :  0.39388E-01 0.66720E+02
   Dimensionless distance   yplus :  0.44054E+00 0.60339E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        461
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         12 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.12519E+04    3570   0.98115E+00   0.10214E+03 
c  VelocityY    0.12519E+04    3570   0.98115E+00   0.00000E+00 
c  VelocityZ    0.12519E+04    3570   0.98115E+00   0.00000E+00 
c  Pressure     0.83668E+01     591   0.77178E-02   0.12788E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -591.54          202.39        -0.76748        -0.41397
v  Velocity[Y]                 -531.61          1138.2          1.2099          1.0323
v  Velocity[Z]                 -306.09           397.4        -0.41701        -0.16706
v  ǁVelocityǁ                 0.026748          1144.7           9.671          6.5075
v  Pressure                -1.2676e+05       2.228e+05           68303           46921
v  turbulent_viscosity       0.0028629          169.56         0.58074         0.33063
v  CourantNb                   0.90181      2.0154e+06          2666.4          1418.2
v  FourierNb                    7.7603      1.3559e+06            1011          429.88
v  total_pressure           3.7324e+05       7.228e+05       5.683e+05      5.4692e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          19.901      2.8269e+06          3677.4          1848.1


 TIME FOR THE TIME STEP              109:        0.59789E+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         0.106335083E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273307398E+00
Free inlet               13           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 0.12459E+04
   Friction velocity        uet   :  0.44442E-01 0.72926E+02
   Friction velocity        uk    :  0.44442E-01 0.72926E+02
   Dimensionless distance   yplus :  0.58107E+00 0.65951E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        359
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.12164E+04    4023   0.97537E+00   0.96615E+02 
c  VelocityY    0.12164E+04    4023   0.97537E+00   0.00000E+00 
c  VelocityZ    0.12164E+04    4023   0.97537E+00   0.00000E+00 
c  Pressure     0.89944E+01     613   0.76362E-02   0.12898E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -631.37          228.65         -1.1688        -0.48498
v  Velocity[Y]                 -577.87          1241.9          1.6284          1.0115
v  Velocity[Z]                 -316.97          398.68        -0.41553       -0.098035
v  ǁVelocityǁ                   0.0164          1246.4          9.2894          5.8912
v  Pressure                -1.3572e+05      2.3722e+05           72403           49757
v  turbulent_viscosity        0.003255          185.84         0.66807         0.38928
v  CourantNb                 0.0016135      2.1563e+06            2977          1629.3
v  FourierNb                    9.4406      1.5318e+06            1145          492.41
v  total_pressure           3.6428e+05      7.3722e+05       5.724e+05      5.4976e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           20.08       3.059e+06          4121.9          2121.7


 TIME FOR THE TIME STEP              110:        0.64783E+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        -0.133594693E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273302422E+00
Free inlet               13           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 0.13590E+04
   Friction velocity        uet   :  0.36963E-01 0.78710E+02
   Friction velocity        uk    :  0.36963E-01 0.78710E+02
   Dimensionless distance   yplus :  0.40451E+00 0.71181E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        376
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         11 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.16927E+04    3867   0.97885E+00   0.91215E+02 
c  VelocityY    0.16927E+04    3867   0.97885E+00   0.00000E+00 
c  VelocityZ    0.16927E+04    3867   0.97885E+00   0.00000E+00 
c  Pressure     0.95429E+01     592   0.77279E-02   0.12835E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -675.29          225.58         -1.0648        -0.48347
v  Velocity[Y]                  -636.1          1367.6          1.5172          1.0781
v  Velocity[Z]                  -348.1          459.01        -0.52096        -0.19773
v  ǁVelocityǁ                 0.034052          1375.8          10.649          6.9807
v  Pressure                -1.4544e+05      2.5177e+05           76531           52541
v  turbulent_viscosity       0.0032404          204.65         0.65701         0.37267
v  CourantNb                   0.90583      2.4305e+06          3013.9          1584.2
v  FourierNb                    8.7892      1.7639e+06          1144.1          482.04
v  total_pressure           3.5456e+05      7.5177e+05      5.7653e+05      5.5254e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          17.096       3.447e+06            4158          2066.3


 TIME FOR THE TIME STEP              111:        0.64010E+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        -0.610187394E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273314454E+00
Free inlet               13           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 0.15024E+04
   Friction velocity        uet   :  0.29893E-01 0.85970E+02
   Friction velocity        uk    :  0.29893E-01 0.85970E+02
   Dimensionless distance   yplus :  0.39522E+00 0.77747E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        328
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         16 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.16808E+04    4064   0.96964E+00   0.10214E+03 
c  VelocityY    0.16808E+04    4064   0.96964E+00   0.00000E+00 
c  VelocityZ    0.16808E+04    4064   0.96964E+00   0.00000E+00 
c  Pressure     0.10293E+02     596   0.75860E-02   0.12984E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -715.52          259.43         -1.3696        -0.52087
v  Velocity[Y]                 -698.18          1487.2          2.0179          1.1202
v  Velocity[Z]                 -359.89          475.27         -0.2156        -0.10289
v  ǁVelocityǁ                 0.026106          1492.8          10.537           6.699
v  Pressure                -1.5553e+05      2.6808e+05           80914           55558
v  turbulent_viscosity       0.0061478          226.07         0.73694         0.42409
v  CourantNb                    0.3412       2.615e+06          3340.1          1787.6
v  FourierNb                    8.7642      1.8591e+06          1268.6          538.34
v  total_pressure           3.4447e+05      7.6808e+05      5.8091e+05      5.5556e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          15.506      3.6943e+06          4608.7          2325.9


 TIME FOR THE TIME STEP              112:        0.66888E+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         0.144392330E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273318067E+00
Free inlet               13           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 0.16348E+04
   Friction velocity        uet   :  0.36188E-01 0.92608E+02
   Friction velocity        uk    :  0.36188E-01 0.92608E+02
   Dimensionless distance   yplus :  0.48036E+00 0.83751E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        488
   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    0.23085E+04    3504   0.97599E+00   0.16695E+03 
c  VelocityY    0.23085E+04    3504   0.97599E+00   0.00000E+00 
c  VelocityZ    0.23085E+04    3504   0.97599E+00   0.00000E+00 
c  Pressure     0.10934E+02     591   0.77431E-02   0.12932E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -764.61          264.28        -0.77213        -0.53109
v  Velocity[Y]                 -762.78          1647.7          1.7602          1.2082
v  Velocity[Z]                 -386.85          565.14        -0.71874        -0.24172
v  ǁVelocityǁ                 0.032619          1658.6          12.585          8.2752
v  Pressure                -1.6684e+05      2.8429e+05           85312           58508
v  turbulent_viscosity       0.0034073          245.77         0.75133         0.42616
v  CourantNb                  0.084031       2.922e+06          3424.1          1796.5
v  FourierNb                    7.2119      1.9607e+06            1299          546.39
v  total_pressure           3.3316e+05      7.8429e+05      5.8531e+05      5.5851e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          17.421      4.0482e+06            4723          2342.9


 TIME FOR THE TIME STEP              113:        0.55338E+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        -0.134792795E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273314735E+00
Free inlet               13           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 0.18166E+04
   Friction velocity        uet   :  0.32039E-01 0.10163E+03
   Friction velocity        uk    :  0.32039E-01 0.10163E+03
   Dimensionless distance   yplus :  0.43246E+00 0.91910E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        313
   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    0.23220E+04    4126   0.96704E+00   0.16647E+03 
c  VelocityY    0.23220E+04    4126   0.96704E+00   0.00000E+00 
c  VelocityZ    0.23220E+04    4126   0.96704E+00   0.00000E+00 
c  Pressure     0.11797E+02     614   0.76033E-02   0.13079E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -817.64          287.97         -1.6208         -0.5977
v  Velocity[Y]                 -836.14          1783.8          2.3096          1.1958
v  Velocity[Z]                 -411.05          576.58         -0.4965       -0.085078
v  ǁVelocityǁ                 0.057398          1790.7          11.544          7.3983
v  Pressure                -1.7806e+05      3.0328e+05           90647           62272
v  turbulent_viscosity       0.0039556          271.96         0.85995         0.49629
v  CourantNb                  0.093877      3.1356e+06          3907.4          2084.7
v  FourierNb                    9.6266      2.2284e+06          1471.9          623.44
v  total_pressure           3.2194e+05      8.0328e+05      5.9065e+05      5.6227e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          18.283       4.442e+06          5379.4          2708.1


 TIME FOR THE TIME STEP              114:        0.62378E+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        -0.270277139E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273309348E+00
Free inlet               13           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 0.19675E+04
   Friction velocity        uet   :  0.25338E-01 0.10905E+03
   Friction velocity        uk    :  0.25338E-01 0.10905E+03
   Dimensionless distance   yplus :  0.47328E+00 0.98618E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        345
   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    0.31359E+04    3644   0.97287E+00   0.20478E+03 
c  VelocityY    0.31359E+04    3644   0.97287E+00   0.00000E+00 
c  VelocityZ    0.31359E+04    3644   0.97287E+00   0.00000E+00 
c  Pressure     0.12512E+02     591   0.76968E-02   0.13002E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -865.34          294.45         -0.5329        -0.64023
v  Velocity[Y]                  -918.4          1972.7         0.96013          1.2928
v  Velocity[Z]                 -440.93          670.88        -0.33126        -0.23479
v  ǁVelocityǁ                 0.017248          1985.8          14.585          9.8198
v  Pressure                -1.9098e+05      3.2151e+05           95707           65640
v  turbulent_viscosity       0.0047466          294.35         0.83677         0.47319
v  CourantNb                   0.76955      3.5098e+06          3806.3          2000.6
v  FourierNb                    9.5442      2.3484e+06          1450.8          605.41
v  total_pressure           3.0902e+05      8.2151e+05      5.9571e+05      5.6564e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          13.641      4.9778e+06          5257.1            2606


 TIME FOR THE TIME STEP              115:        0.65634E+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        -0.155768671E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273320756E+00
Free inlet               13           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 0.21838E+04
   Friction velocity        uet   :  0.20676E-01 0.11958E+03
   Friction velocity        uk    :  0.20676E-01 0.11958E+03
   Dimensionless distance   yplus :  0.57641E+00 0.10814E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        368
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         14 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.32200E+04    4302   0.96466E+00   0.20257E+03 
c  VelocityY    0.32200E+04    4302   0.96466E+00   0.00000E+00 
c  VelocityZ    0.32200E+04    4302   0.96466E+00   0.00000E+00 
c  Pressure     0.13484E+02     594   0.75374E-02   0.13133E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -931.99          332.97         -1.6519        -0.73433
v  Velocity[Y]                 -1001.7          2145.3            2.22          1.3241
v  Velocity[Z]                 -454.77          689.58        -0.52463       -0.080228
v  ǁVelocityǁ                 0.040553          2153.3          12.934          8.4858
v  Pressure                -2.0442e+05      3.4209e+05      1.0147e+05           69624
v  turbulent_viscosity       0.0031005          326.37         0.98194         0.56517
v  CourantNb                    2.3287      3.7787e+06          4498.2          2432.9
v  FourierNb                     9.132      2.8986e+06          1686.8          706.95
v  total_pressure           2.9558e+05      8.4209e+05      6.0147e+05      5.6962e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          18.162      5.3386e+06            6185          3139.8


 TIME FOR THE TIME STEP              116:        0.64570E+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        -0.263233995E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273324375E+00
Free inlet               13           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 0.23744E+04
   Friction velocity        uet   :  0.41123E-01 0.12877E+03
   Friction velocity        uk    :  0.41123E-01 0.12877E+03
   Dimensionless distance   yplus :  0.44621E+00 0.11646E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        252
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.42710E+04    3754   0.97018E+00   0.31478E+03 
c  VelocityY    0.42710E+04    3754   0.97018E+00   0.00000E+00 
c  VelocityZ    0.42710E+04    3754   0.97018E+00   0.00000E+00 
c  Pressure     0.14415E+02     623   0.81223E-02   0.13150E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -998.13          328.19         -1.3519        -0.71682
v  Velocity[Y]                 -1106.7          2352.8          2.2811          1.3416
v  Velocity[Z]                 -500.52          822.75        -0.44745        -0.22607
v  ǁVelocityǁ                 0.066892          2367.3          17.951          12.394
v  Pressure                -2.1811e+05      3.6406e+05      1.0907e+05           74844
v  turbulent_viscosity       0.0065004          353.87         0.94736         0.53745
v  CourantNb                    2.1617      4.2375e+06          4283.7          2263.3
v  FourierNb                     9.997      3.0502e+06          1645.7          682.58
v  total_pressure           2.8189e+05      8.6406e+05      6.0907e+05      5.7484e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          14.013      5.9373e+06          5929.4          2945.9


 TIME FOR THE TIME STEP              117:        0.58047E+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        -0.205183142E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273326185E+00
Free inlet               13           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 0.26133E+04
   Friction velocity        uet   :  0.44329E-01 0.14019E+03
   Friction velocity        uk    :  0.44329E-01 0.14019E+03
   Dimensionless distance   yplus :  0.66304E+00 0.12678E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        167
   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    0.44095E+04    4244   0.96162E+00   0.36648E+03 
c  VelocityY    0.44095E+04    4244   0.96162E+00   0.00000E+00 
c  VelocityZ    0.44095E+04    4244   0.96162E+00   0.00000E+00 
c  Pressure     0.15525E+02     565   0.74874E-02   0.13266E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1054.8          377.57         -2.1806        -0.85063
v  Velocity[Y]                 -1208.2            2578          3.1364          1.5049
v  Velocity[Z]                 -513.36          828.01         -0.4154       -0.095139
v  ǁVelocityǁ                  0.12455          2588.1          14.361          9.6161
v  Pressure                 -2.343e+05      3.8635e+05      1.1397e+05           78154
v  turbulent_viscosity        0.004349          386.64          1.1809         0.69712
v  CourantNb                     1.794      4.5088e+06          5396.3          2945.6
v  FourierNb                    8.1808       3.175e+06          2006.4          848.38
v  total_pressure            2.657e+05      8.8635e+05      6.1397e+05      5.7815e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          16.172      6.3947e+06          7402.7            3794


 TIME FOR THE TIME STEP              118:        0.64003E+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         0.252464507E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273317398E+00
Free inlet               13           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 0.28641E+04
   Friction velocity        uet   :  0.54538E-01 0.15207E+03
   Friction velocity        uk    :  0.54538E-01 0.15207E+03
   Dimensionless distance   yplus :  0.91919E+00 0.13752E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         96
   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    0.59585E+04    4708   0.96878E+00   0.46219E+03 
c  VelocityY    0.59585E+04    4708   0.96878E+00   0.00000E+00 
c  VelocityZ    0.59585E+04    4708   0.96878E+00   0.00000E+00 
c  Pressure     0.16470E+02     584   0.77178E-02   0.13176E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1122.5          376.41         -1.2703        -0.85051
v  Velocity[Y]                 -1326.8          2846.7          1.9601          1.5698
v  Velocity[Z]                 -556.34           964.6        0.018218        -0.28898
v  ǁVelocityǁ                  0.07251          2864.5           18.68          12.875
v  Pressure                -2.5103e+05      4.0997e+05      1.2042e+05           82412
v  turbulent_viscosity        0.008174          427.16          1.0766         0.61312
v  CourantNb                    4.1507      5.0918e+06          4789.5          2535.7
v  FourierNb                    10.322      3.3993e+06          1859.3          770.13
v  total_pressure           2.4897e+05      9.0997e+05      6.2042e+05      5.8241e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          19.402      7.1233e+06          6648.8          3305.8


 TIME FOR THE TIME STEP              119:        0.82312E+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        -0.297543775E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273318125E+00
Free inlet               13           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 0.31714E+04
   Friction velocity        uet   :  0.41684E-01 0.16648E+03
   Friction velocity        uk    :  0.41684E-01 0.16648E+03
   Dimensionless distance   yplus :  0.46511E+00 0.15055E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        121
   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    0.62756E+04    4232   0.95757E+00   0.44430E+03 
c  VelocityY    0.62756E+04    4232   0.95757E+00   0.00000E+00 
c  VelocityZ    0.62756E+04    4232   0.95757E+00   0.00000E+00 
c  Pressure     0.17798E+02     614   0.75151E-02   0.13330E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1209.6          433.96         -2.2797        -0.94192
v  Velocity[Y]                 -1458.9          3083.8          2.7854          1.5697
v  Velocity[Z]                 -586.57             992        -0.67213       -0.059405
v  ǁVelocityǁ                   0.0437          3095.2          16.788          10.979
v  Pressure                -2.6799e+05      4.3706e+05      1.2814e+05           87823
v  turbulent_viscosity       0.0064372          472.79          1.2944         0.75181
v  CourantNb                 0.0082173      5.4602e+06          5787.4          3141.5
v  FourierNb                    9.3282       4.188e+06          2220.7          923.57
v  total_pressure           2.3201e+05      9.3706e+05      6.2814e+05      5.8782e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          10.636       7.689e+06          8008.1            4065


 TIME FOR THE TIME STEP              120:        0.66573E+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        -0.343913217E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273322921E+00
Free inlet               13           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 0.34380E+04
   Friction velocity        uet   :  0.23688E-01 0.17887E+03
   Friction velocity        uk    :  0.23688E-01 0.17887E+03
   Dimensionless distance   yplus :  0.30623E+00 0.16176E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        112
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         22 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.81217E+04    3855   0.96327E+00   0.69800E+03 
c  VelocityY    0.81217E+04    3855   0.96327E+00   0.00000E+00 
c  VelocityZ    0.81217E+04    3855   0.96327E+00   0.00000E+00 
c  Pressure     0.19036E+02     603   0.80321E-02   0.13340E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1277.6          436.58         -1.5559        -0.93482
v  Velocity[Y]                 -1602.1          3392.9          3.4068          1.6978
v  Velocity[Z]                 -630.69          1195.6        -0.21744        -0.28029
v  ǁVelocityǁ                 0.057945          3415.3           22.73          15.643
v  Pressure                 -2.862e+05      4.6456e+05       1.366e+05           93569
v  turbulent_viscosity       0.0072952          511.84          1.2419         0.70068
v  CourantNb                     2.392      6.1319e+06          5608.9          2931.5
v  FourierNb                    9.5357      4.4094e+06          2158.4          881.77
v  total_pressure            2.138e+05      9.6456e+05       6.366e+05      5.9357e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          27.728      8.4579e+06          7767.3          3813.3


 TIME FOR THE TIME STEP              121:        0.60784E+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         0.217809032E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273323850E+00
Free inlet               13           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 0.37940E+04
   Friction velocity        uet   :  0.47547E-01 0.19527E+03
   Friction velocity        uk    :  0.47547E-01 0.19527E+03
   Dimensionless distance   yplus :  0.78776E+00 0.17659E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         97
   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    0.87282E+04    4122   0.95851E+00   0.71911E+03 
c  VelocityY    0.87282E+04    4122   0.95851E+00   0.00000E+00 
c  VelocityZ    0.87282E+04    4122   0.95851E+00   0.00000E+00 
c  Pressure     0.20527E+02     572   0.74292E-02   0.13464E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1357.4          479.98         -2.9266         -1.0123
v  Velocity[Y]                 -1753.9          3724.5          3.8825          1.8081
v  Velocity[Z]                 -649.06          1193.4        0.032116        -0.11099
v  ǁVelocityǁ                 0.083446          3737.6          19.958          12.945
v  Pressure                -3.0665e+05      4.9399e+05      1.4323e+05           98070
v  turbulent_viscosity       0.0062581          559.13          1.5222         0.89724
v  CourantNb                    3.8084      6.5583e+06          6923.2          3742.4
v  FourierNb                    9.2543      4.5924e+06            2590          1083.5
v  total_pressure           1.9335e+05      9.9399e+05      6.4323e+05      5.9807e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          29.252      9.1967e+06          9513.2          4825.9


 TIME FOR THE TIME STEP              122:        0.62627E+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        -0.416516208E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273346150E+00
Free inlet               13           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 0.41644E+04
   Friction velocity        uet   :  0.51720E-01 0.21217E+03
   Friction velocity        uk    :  0.51720E-01 0.21217E+03
   Dimensionless distance   yplus :  0.83124E+00 0.19188E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         56
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.11533E+05    4865   0.96249E+00   0.98488E+03 
c  VelocityY    0.11533E+05    4865   0.96249E+00   0.00000E+00 
c  VelocityZ    0.11533E+05    4865   0.96249E+00   0.00000E+00 
c  Pressure     0.21870E+02     617   0.78397E-02   0.13415E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1460.7          490.52         -2.1296        -0.98422
v  Velocity[Y]                 -1912.4          4089.1          2.1717          1.8077
v  Velocity[Z]                 -721.07          1397.7         0.41346        -0.29926
v  ǁVelocityǁ                 0.033454          4116.8           25.97          17.077
v  Pressure                -3.2681e+05      5.2949e+05      1.5309e+05      1.0476e+05
v  turbulent_viscosity       0.0077127          617.44          1.4399         0.80684
v  CourantNb                    2.6452      7.3372e+06          6591.7          3404.6
v  FourierNb                    10.315      4.9032e+06            2511            1016
v  total_pressure           1.7319e+05      1.0295e+06      6.5309e+05      6.0476e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          19.087      1.0502e+07          9102.7          4420.6


 TIME FOR THE TIME STEP              123:        0.85542E+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        -0.316777709E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273335982E+00
Free inlet               13           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 0.45850E+04
   Friction velocity        uet   :  0.26298E-01 0.23120E+03
   Friction velocity        uk    :  0.26298E-01 0.23120E+03
   Dimensionless distance   yplus :  0.28406E+00 0.20908E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        217
   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    0.12568E+05    4201   0.95284E+00   0.86164E+03 
c  VelocityY    0.12568E+05    4201   0.95284E+00   0.00000E+00 
c  VelocityZ    0.12568E+05    4201   0.95284E+00   0.00000E+00 
c  Pressure     0.23640E+02     586   0.74170E-02   0.13565E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                   -1555          552.63         -3.0221         -1.2088
v  Velocity[Y]                 -2124.5          4448.2           4.108          1.9715
v  Velocity[Z]                 -741.29          1421.8        -0.42723       -0.077327
v  ǁVelocityǁ                  0.14831          4463.6          20.798          13.681
v  Pressure                -3.4974e+05      5.6479e+05      1.6062e+05      1.0985e+05
v  turbulent_viscosity       0.0035718          680.83          1.6986         0.97454
v  CourantNb                    2.5953      7.9693e+06          8021.1          4186.9
v  FourierNb                    7.8275      5.5883e+06            2928          1198.1
v  total_pressure           1.5026e+05      1.0648e+06      6.6062e+05      6.0985e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          18.144      1.1095e+07           10949          5384.9


 TIME FOR THE TIME STEP              124:        0.75352E+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        -0.389415855E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273336065E+00
Free inlet               13           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 0.49927E+04
   Friction velocity        uet   :  0.55507E-01 0.24948E+03
   Friction velocity        uk    :  0.55507E-01 0.24948E+03
   Dimensionless distance   yplus :  0.56412E+00 0.22561E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         62
   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    0.16215E+05    4266   0.95989E+00   0.11665E+04 
c  VelocityY    0.16215E+05    4266   0.95989E+00   0.00000E+00 
c  VelocityZ    0.16215E+05    4266   0.95989E+00   0.00000E+00 
c  Pressure     0.25229E+02     575   0.78738E-02   0.13532E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1652.8           548.9         -3.1094         -1.2321
v  Velocity[Y]                   -2292          4908.7          4.1162          2.1033
v  Velocity[Z]                 -796.65            1726        -0.18102        -0.40566
v  ǁVelocityǁ                  0.12814          4948.7          27.748          18.682
v  Pressure                -3.7501e+05      6.1788e+05      1.6987e+05      1.1595e+05
v  turbulent_viscosity       0.0067023          741.23          1.5939         0.89455
v  CourantNb                     2.681      8.8381e+06          7092.8          3673.8
v  FourierNb                    12.303      5.8921e+06          2784.1          1123.1
v  total_pressure           1.2499e+05      1.1179e+06      6.6987e+05      6.1595e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          39.333      1.2482e+07          9876.9          4796.9


 TIME FOR THE TIME STEP              125:        0.66856E+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        -0.971369919E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273362962E+00
Free inlet               13           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 0.55187E+04
   Friction velocity        uet   :  0.54140E-01 0.27285E+03
   Friction velocity        uk    :  0.54140E-01 0.27285E+03
   Dimensionless distance   yplus :  0.70716E+00 0.24675E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         56
   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    0.17838E+05    4044   0.95310E+00   0.13193E+04 
c  VelocityY    0.17838E+05    4044   0.95310E+00   0.00000E+00 
c  VelocityZ    0.17838E+05    4044   0.95310E+00   0.00000E+00 
c  Pressure     0.27335E+02     590   0.74335E-02   0.13701E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1757.5          635.79         -3.7096         -1.4339
v  Velocity[Y]                 -2541.9          5348.5          5.4155          2.0631
v  Velocity[Z]                  -838.7          1712.3         -1.2186       -0.024257
v  ǁVelocityǁ                 0.062973          5367.9          26.234          16.893
v  Pressure                -4.0045e+05      6.6249e+05      1.7982e+05      1.2285e+05
v  turbulent_viscosity       0.0090383           816.5          1.9092          1.1151
v  CourantNb                    1.0478      9.5295e+06          8682.2          4582.5
v  FourierNb                    10.141      6.6719e+06          3278.4          1349.5
v  total_pressure                99551      1.1625e+06      6.7982e+05      6.2285e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          20.051      1.3331e+07           11961            5932


 TIME FOR THE TIME STEP              126:        0.63841E+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        -0.874962032E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273352884E+00
Free inlet               13           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 0.60189E+04
   Friction velocity        uet   :  0.52134E-01 0.29489E+03
   Friction velocity        uk    :  0.52134E-01 0.29489E+03
   Dimensionless distance   yplus :  0.72292E+00 0.26668E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         65
   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    0.22866E+05    5135   0.95747E+00   0.23658E+04 
c  VelocityY    0.22866E+05    5135   0.95747E+00   0.00000E+00 
c  VelocityZ    0.22866E+05    5135   0.95747E+00   0.00000E+00 
c  Pressure     0.29149E+02     596   0.80532E-02   0.13647E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1865.5          624.77         -1.9323          -1.506
v  Velocity[Y]                 -2766.1          5889.3          3.2738          2.1212
v  Velocity[Z]                 -908.34          2041.7          1.5843         -0.2536
v  ǁVelocityǁ                 0.054258          5933.1          33.757           23.23
v  Pressure                -4.2778e+05      7.2496e+05      1.9191e+05      1.3083e+05
v  turbulent_viscosity        0.010639          891.02          1.8956          1.0626
v  CourantNb                    4.3856      1.0602e+07          8720.4          4427.2
v  FourierNb                    14.231      7.0745e+06          3310.3          1326.5
v  total_pressure                72219       1.225e+06      6.9191e+05      6.3083e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          30.167      1.4829e+07           12031          5753.6


 TIME FOR THE TIME STEP              127:        0.79139E+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         0.280803672E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273379212E+00
Free inlet               13           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 0.66444E+04
   Friction velocity        uet   :  0.51745E-01 0.32220E+03
   Friction velocity        uk    :  0.51745E-01 0.32220E+03
   Dimensionless distance   yplus :  0.82389E+00 0.29138E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         99
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         21 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.25355E+05    4134   0.95208E+00   0.21861E+04 
c  VelocityY    0.25355E+05    4134   0.95208E+00   0.00000E+00 
c  VelocityZ    0.25355E+05    4134   0.95208E+00   0.00000E+00 
c  Pressure     0.31621E+02     583   0.73258E-02   0.13826E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2022.5          722.31         -3.9622         -1.6849
v  Velocity[Y]                 -3057.1          6418.4          5.8185          2.3513
v  Velocity[Z]                 -933.12          2054.2        -0.86244       -0.023728
v  ǁVelocityǁ                  0.35779          6440.5          28.719          18.689
v  Pressure                -4.5758e+05      7.7579e+05      2.0207e+05      1.3786e+05
v  turbulent_viscosity       0.0057336          983.06          2.2323          1.3008
v  CourantNb                    0.6989      1.1498e+07           10418          5546.6
v  FourierNb                    9.7246      8.0626e+06          3845.3          1569.9
v  total_pressure                42418      1.2758e+06      7.0207e+05      6.3786e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          25.571      1.6009e+07           14263          7116.5


 TIME FOR THE TIME STEP              128:        0.69064E+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        -0.968621218E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273347754E+00
Free inlet               13           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 0.72428E+04
   Friction velocity        uet   :  0.61903E-01 0.34811E+03
   Friction velocity        uk    :  0.61903E-01 0.34811E+03
   Dimensionless distance   yplus :  0.75993E+00 0.31481E+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         23 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.31849E+05    3967   0.95500E+00   0.21186E+04 
c  VelocityY    0.31849E+05    3967   0.95500E+00   0.00000E+00 
c  VelocityZ    0.31849E+05    3967   0.95500E+00   0.00000E+00 
c  Pressure     0.33827E+02     631   0.80367E-02   0.13804E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2157.1          725.23         -3.2419         -1.6379
v  Velocity[Y]                   -3322          7041.8          2.3865          2.2482
v  Velocity[Z]                 -1029.5          2441.4       -0.015178        -0.31892
v  ǁVelocityǁ                  0.03762          7083.6           39.07          25.636
v  Pressure                -4.8521e+05      8.5452e+05      2.1994e+05      1.5035e+05
v  turbulent_viscosity       0.0089285            1069          2.1173          1.1807
v  CourantNb                    4.9295      1.2794e+07          9676.9          4923.2
v  FourierNb                    13.501      9.1771e+06          3733.7          1476.9
v  total_pressure                14788      1.3545e+06      7.1994e+05      6.5035e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          41.309      1.7865e+07           13411          6400.1


 TIME FOR THE TIME STEP              129:        0.70209E+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         0.107718937E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273352140E+00
Free inlet               13           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 0.79708E+04
   Friction velocity        uet   :  0.46466E-01 0.37936E+03
   Friction velocity        uk    :  0.46466E-01 0.37936E+03
   Dimensionless distance   yplus :  0.10626E+01 0.34308E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         85
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         25 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.35857E+05    4383   0.94914E+00   0.21769E+04 
c  VelocityY    0.35857E+05    4383   0.94914E+00   0.00000E+00 
c  VelocityZ    0.35857E+05    4383   0.94914E+00   0.00000E+00 
c  Pressure     0.36560E+02     582   0.73541E-02   0.13936E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2254.8          810.57         -5.2162         -1.7355
v  Velocity[Y]                 -3675.4            7702          5.3562          2.4827
v  Velocity[Z]                 -1068.7          2484.8        -0.32447        0.055471
v  ǁVelocityǁ                  0.11458          7729.6           33.94          21.447
v  Pressure                -5.1854e+05      9.1324e+05      2.3068e+05      1.5776e+05
v  turbulent_viscosity       0.0098851            1167          2.6791          1.5136
v  CourantNb                   0.32443      1.3834e+07           12102            6242
v  FourierNb                    10.262      9.5505e+06          4655.6          1862.5
v  total_pressure               -18542      1.4132e+06      7.3068e+05      6.5776e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          27.627      1.9287e+07           16758          8104.5


 TIME FOR THE TIME STEP              130:        0.69385E+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         0.486258904E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273356807E+00
Free inlet               13           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 0.87208E+04
   Friction velocity        uet   :  0.50709E-01 0.41129E+03
   Friction velocity        uk    :  0.50709E-01 0.41129E+03
   Dimensionless distance   yplus :  0.66927E+00 0.37196E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         55
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         20 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.45969E+05    5361   0.95644E+00   0.40267E+04 
c  VelocityY    0.45969E+05    5361   0.95644E+00   0.00000E+00 
c  VelocityZ    0.45969E+05    5361   0.95644E+00   0.00000E+00 
c  Pressure     0.39045E+02     606   0.79472E-02   0.13886E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2426.4          811.77         -2.4795         -1.8366
v  Velocity[Y]                 -3983.5          8500.2          3.9471          2.5264
v  Velocity[Z]                 -1148.2          2908.1        -0.56462        -0.29148
v  ǁVelocityǁ                  0.14697          8559.8          44.473          30.736
v  Pressure                  -5.53e+05      9.9954e+05      2.4666e+05      1.6834e+05
v  turbulent_viscosity       0.0095892          1286.1          2.4642          1.3723
v  CourantNb                    2.5605      1.5368e+07           11409          5688.9
v  FourierNb                    10.764      1.0202e+07          4340.6          1712.6
v  total_pressure               -53002      1.4995e+06      7.4666e+05      6.6834e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          28.224      2.1441e+07           15749          7401.5


 TIME FOR THE TIME STEP              131:        0.86101E+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        -0.389666919E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273367628E+00
Free inlet               13           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 0.96402E+04
   Friction velocity        uet   :  0.59024E-01 0.45010E+03
   Friction velocity        uk    :  0.59024E-01 0.45010E+03
   Dimensionless distance   yplus :  0.91508E+00 0.40705E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         34
   Total number of wall faces                   :       6590
------------------------------------------------------------


Incoming flow detained for         28 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.51919E+05    4324   0.94815E+00   0.39898E+04 
c  VelocityY    0.51919E+05    4324   0.94815E+00   0.00000E+00 
c  VelocityZ    0.51919E+05    4324   0.94815E+00   0.00000E+00 
c  Pressure     0.42467E+02     603   0.73500E-02   0.14084E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2614.5          984.28         -5.4773         -2.0466
v  Velocity[Y]                 -4426.1          9232.3          6.7393          2.6969
v  Velocity[Z]                 -1321.2          2952.8         -1.5608          0.1993
v  ǁVelocityǁ                  0.16191          9263.8          37.802          24.749
v  Pressure                -5.8859e+05      1.0723e+06      2.6186e+05      1.7909e+05
v  turbulent_viscosity        0.012746          1422.1          2.9352          1.6899
v  CourantNb                    2.7459       1.668e+07           13795          7287.3
v  FourierNb                    12.284      1.2562e+07          5121.1          2048.4
v  total_pressure               -88593      1.5723e+06      7.6186e+05      6.7909e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           44.42      2.3168e+07           18916          9335.7


 TIME FOR THE TIME STEP              132:        0.82041E+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        -0.385072248E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273374248E+00
Free inlet               13           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 0.10480E+05
   Friction velocity        uet   :  0.46219E-01 0.48527E+03
   Friction velocity        uk    :  0.46219E-01 0.48527E+03
   Dimensionless distance   yplus :  0.71643E+00 0.43885E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         55
   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    0.65595E+05    4304   0.95194E+00   0.48383E+04 
c  VelocityY    0.65595E+05    4304   0.95194E+00   0.00000E+00 
c  VelocityZ    0.65595E+05    4304   0.95194E+00   0.00000E+00 
c  Pressure     0.45521E+02     610   0.79114E-02   0.14071E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2739.1          916.02         -6.2091          -2.102
v  Velocity[Y]                 -4790.4           10177          3.4294          2.7589
v  Velocity[Z]                 -1297.7          3560.6         0.79924        -0.41686
v  ǁVelocityǁ                 0.072069           10261          48.864          31.581
v  Pressure                -6.2689e+05      1.1788e+06      2.8167e+05      1.9273e+05
v  turbulent_viscosity        0.011129          1543.5           2.797          1.5534
v  CourantNb                   0.16212      1.8524e+07           12832          6493.7
v  FourierNb                    13.454      1.2247e+07          4951.2          1938.8
v  total_pressure          -1.2689e+05      1.6788e+06      7.8167e+05      6.9273e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          42.037      2.5804e+07           17784          8432.4


 TIME FOR THE TIME STEP              133:        0.68034E+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        -0.156044012E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273391608E+00
Free inlet               13           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 0.11577E+05
   Friction velocity        uet   :  0.49236E-01 0.53079E+03
   Friction velocity        uk    :  0.49236E-01 0.53079E+03
   Dimensionless distance   yplus :  0.80309E+00 0.48002E+04
   ------------------------------------------------------
   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         23 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.74240E+05    4125   0.95037E+00   0.46567E+04 
c  VelocityY    0.74240E+05    4125   0.95037E+00   0.00000E+00 
c  VelocityZ    0.74240E+05    4125   0.95037E+00   0.00000E+00 
c  Pressure     0.49397E+02     495   0.72907E-02   0.14230E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2936.5          1169.1         -6.2542         -2.5887
v  Velocity[Y]                 -5287.6           11140          9.1628          3.1817
v  Velocity[Z]                 -1551.1          3589.6        -0.63352         0.32537
v  ǁVelocityǁ                  0.22174           11181          46.874          30.745
v  Pressure                -6.7308e+05      1.2586e+06      2.9279e+05      2.0009e+05
v  turbulent_viscosity        0.008731          1703.9          3.3655          1.8983
v  CourantNb                    2.8564      1.9963e+07           15470          7816.2
v  FourierNb                    10.569      1.3903e+07          5895.8          2333.9
v  total_pressure          -1.7308e+05      1.7586e+06      7.9279e+05      7.0009e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           18.83      2.7937e+07           21365           10150


 TIME FOR THE TIME STEP              134:        0.72219E+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        -0.604029783E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273205055E+00
Free inlet               13           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 0.12671E+05
   Friction velocity        uet   :  0.74243E-01 0.57584E+03
   Friction velocity        uk    :  0.74243E-01 0.57584E+03
   Dimensionless distance   yplus :  0.83015E+00 0.52076E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          9
   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    0.93571E+05    5810   0.95281E+00   0.80609E+04 
c  VelocityY    0.93571E+05    5810   0.95281E+00   0.00000E+00 
c  VelocityZ    0.93571E+05    5810   0.95281E+00   0.00000E+00 
c  Pressure     0.52732E+02     602   0.78420E-02   0.14151E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3112.4          1128.3         -3.1936         -2.3923
v  Velocity[Y]                 -5761.1           12230          4.7096          3.1112
v  Velocity[Z]                   -1495          4213.5          2.1912     -0.00071027
v  ǁVelocityǁ                 0.097449           12318          57.698          38.251
v  Pressure                -7.1837e+05      1.3762e+06      3.1287e+05      2.1358e+05
v  turbulent_viscosity        0.025146          1859.3          3.2941          1.8469
v  CourantNb                    11.782      2.2223e+07           15555          7785.7
v  FourierNb                      17.9      1.4729e+07          5836.1            2282
v  total_pressure          -2.1837e+05      1.8762e+06      8.1287e+05      7.1358e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          72.203       3.108e+07           21391           10068


 TIME FOR THE TIME STEP              135:        0.10064E+02

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


 INSTANT    0.136000000E+02   TIME STEP NUMBER             136
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.641325660E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273388698E+00
Free inlet               13           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 0.13947E+05
   Friction velocity        uet   :  0.58156E-01 0.62795E+03
   Friction velocity        uk    :  0.58156E-01 0.62795E+03
   Dimensionless distance   yplus :  0.10673E+01 0.56789E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         36
   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    0.10673E+06    4302   0.94539E+00   0.90308E+04 
c  VelocityY    0.10673E+06    4302   0.94539E+00   0.00000E+00 
c  VelocityZ    0.10673E+06    4302   0.94539E+00   0.00000E+00 
c  Pressure     0.57423E+02     562   0.72891E-02   0.14353E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3354.4          1429.2         -4.9988          -2.669
v  Velocity[Y]                 -6392.5           13304          10.002          3.5469
v  Velocity[Z]                 -1899.1          4275.9         -1.3534         0.51115
v  ǁVelocityǁ                  0.30006           13352          53.688          35.645
v  Pressure                -7.6897e+05      1.4703e+06      3.2679e+05      2.2336e+05
v  turbulent_viscosity        0.013027          2050.6           3.828          2.1674
v  CourantNb                     6.557      2.4154e+07           18211          9291.3
v  FourierNb                    8.6135      1.8114e+07          6753.9          2651.5
v  total_pressure          -2.6897e+05      1.9703e+06      8.2679e+05      7.2336e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          31.019      3.3555e+07           24965           11943


 TIME FOR THE TIME STEP              136:        0.75702E+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        -0.295777637E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273396767E+00
Free inlet               13           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 0.15183E+05
   Friction velocity        uet   :  0.67672E-01 0.67802E+03
   Friction velocity        uk    :  0.67672E-01 0.67802E+03
   Dimensionless distance   yplus :  0.10299E+01 0.61317E+04
   ------------------------------------------------------
   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         30 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.13153E+06    4375   0.95136E+00   0.97254E+04 
c  VelocityY    0.13153E+06    4375   0.95136E+00   0.00000E+00 
c  VelocityZ    0.13153E+06    4375   0.95136E+00   0.00000E+00 
c  Pressure     0.61649E+02     612   0.78279E-02   0.14337E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3580.9          1260.9         -6.6841         -2.8797
v  Velocity[Y]                 -6898.9           14649          7.0081          3.1857
v  Velocity[Z]                   -1646          5104.7         0.37019        -0.23491
v  ǁVelocityǁ                  0.27372           14736          62.114           40.48
v  Pressure                -8.1637e+05      1.6169e+06      3.5488e+05      2.4294e+05
v  turbulent_viscosity        0.022549          2227.9          3.7729          2.1096
v  CourantNb                    12.661      2.6783e+07           17898          8965.5
v  FourierNb                    20.534      1.7672e+07          6731.9            2605
v  total_pressure          -3.1637e+05      2.1169e+06      8.5488e+05      7.4294e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           46.49      3.7334e+07           24630           11570


 TIME FOR THE TIME STEP              137:        0.67369E+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         0.815563746E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273472106E+00
Free inlet               13           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 0.16749E+05
   Friction velocity        uet   :  0.45987E-01 0.74094E+03
   Friction velocity        uk    :  0.45987E-01 0.74094E+03
   Dimensionless distance   yplus :  0.73278E+00 0.67007E+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         29 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.15070E+06    4277   0.94742E+00   0.82320E+04 
c  VelocityY    0.15070E+06    4277   0.94742E+00   0.00000E+00 
c  VelocityZ    0.15070E+06    4277   0.94742E+00   0.00000E+00 
c  Pressure     0.66974E+02     581   0.73144E-02   0.14501E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3812.6          1715.8         -9.5638         -3.1747
v  Velocity[Y]                 -7654.2           15989          7.7835          3.5769
v  Velocity[Z]                 -2230.6          5175.5          1.1384         0.71204
v  ǁVelocityǁ                  0.30225           16047          59.032          38.324
v  Pressure                -8.7238e+05      1.7317e+06      3.7199e+05      2.5472e+05
v  turbulent_viscosity        0.022204          2431.1          4.3938          2.4733
v  CourantNb                    4.5171      2.8967e+07           20031           10022
v  FourierNb                    18.004      1.9857e+07          7761.9          3032.5
v  total_pressure          -3.7238e+05      2.2317e+06      8.7199e+05      7.5472e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          27.669       4.046e+07           27793           13054


 TIME FOR THE TIME STEP              138:        0.77605E+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        -0.357865067E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273415255E+00
Free inlet               13           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 0.18286E+05
   Friction velocity        uet   :  0.74764E-01 0.80225E+03
   Friction velocity        uk    :  0.74764E-01 0.80225E+03
   Dimensionless distance   yplus :  0.10691E+01 0.72552E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         21
   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    0.19137E+06    5596   0.95027E+00   0.22301E+05 
c  VelocityY    0.19137E+06    5596   0.95027E+00   0.00000E+00 
c  VelocityZ    0.19137E+06    5596   0.95027E+00   0.00000E+00 
c  Pressure     0.71935E+02     612   0.82924E-02   0.14485E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                   -4009          1577.3         -6.1488         -3.0798
v  Velocity[Y]                 -8323.3           17603          8.5238          3.6276
v  Velocity[Z]                   -1944          6075.6         0.70554         0.30543
v  ǁVelocityǁ                  0.11539           17733          84.811          57.388
v  Pressure                -9.2677e+05      1.9072e+06      4.0245e+05      2.7554e+05
v  turbulent_viscosity        0.021164          2674.2          4.3171          2.4015
v  CourantNb                     17.25      3.2163e+07           20139          9911.7
v  FourierNb                    17.824      2.1193e+07          7736.7          2971.2
v  total_pressure          -4.2677e+05      2.4072e+06      9.0245e+05      7.7554e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          57.309      4.4912e+07           27875           12883


 TIME FOR THE TIME STEP              139:        0.96645E+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        -0.104399912E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273481781E+00
Free inlet               13           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 0.20179E+05
   Friction velocity        uet   :  0.64478E-01 0.87710E+03
   Friction velocity        uk    :  0.64478E-01 0.87710E+03
   Dimensionless distance   yplus :  0.79962E+00 0.79321E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         28
   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    0.21946E+06    5007   0.94665E+00   0.23319E+05 
c  VelocityY    0.21946E+06    5007   0.94665E+00   0.00000E+00 
c  VelocityZ    0.21946E+06    5007   0.94665E+00   0.00000E+00 
c  Pressure     0.78242E+02     549   0.72097E-02   0.14653E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -4343.9          2045.7         -9.8519          -3.589
v  Velocity[Y]                 -9200.7           19186          15.286          4.1189
v  Velocity[Z]                 -2742.1          6195.9         0.76481         0.83747
v  ǁVelocityǁ                  0.46081           19255          68.768          45.243
v  Pressure                -9.9119e+05      2.0347e+06      4.1944e+05      2.8681e+05
v  turbulent_viscosity        0.015356          2959.2          5.1807          3.0192
v  CourantNb                    2.5499      3.4857e+07           26103           13363
v  FourierNb                    16.873      2.6125e+07          9158.6          3600.3
v  total_pressure          -4.9119e+05      2.5347e+06      9.1944e+05      7.8681e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          43.813      4.8465e+07           35262           16963


 TIME FOR THE TIME STEP              140:        0.87081E+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        -0.102347590E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273440826E+00
Free inlet               13           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 0.21990E+05
   Friction velocity        uet   :  0.75140E-01 0.94819E+03
   Friction velocity        uk    :  0.75140E-01 0.94819E+03
   Dimensionless distance   yplus :  0.90260E+00 0.85750E+04
   ------------------------------------------------------
   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         25 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.27450E+06    5653   0.94876E+00   0.19858E+05 
c  VelocityY    0.27450E+06    5653   0.94876E+00   0.00000E+00 
c  VelocityZ    0.27450E+06    5653   0.94876E+00   0.00000E+00 
c  Pressure     0.83936E+02     635   0.78502E-02   0.14614E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -4700.3          1781.5         -10.727          -3.524
v  Velocity[Y]                 -9999.9           21091          6.3143          3.8253
v  Velocity[Z]                 -2349.3          7232.6          3.4322         0.11421
v  ǁVelocityǁ                  0.38054           21246          90.522          56.773
v  Pressure                -1.0498e+06      2.2429e+06      4.5983e+05      3.1526e+05
v  turbulent_viscosity        0.022037          3211.7          4.8895          2.6993
v  CourantNb                    3.8991      3.8733e+07           23420           11543
v  FourierNb                    16.954      2.5426e+07          8857.1          3359.5
v  total_pressure          -5.4985e+05      2.7429e+06      9.5983e+05      8.1526e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          81.668      5.3988e+07           32277           14902


 TIME FOR THE TIME STEP              141:        0.90258E+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        -0.418192194E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273458884E+00
Free inlet               13           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 0.24232E+05
   Friction velocity        uet   :  0.56699E-01 0.10355E+04
   Friction velocity        uk    :  0.56699E-01 0.10355E+04
   Dimensionless distance   yplus :  0.99826E+00 0.93643E+04
   ------------------------------------------------------
   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         31 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.31651E+06    4643   0.94541E+00   0.17378E+05 
c  VelocityY    0.31651E+06    4643   0.94541E+00   0.00000E+00 
c  VelocityZ    0.31651E+06    4643   0.94541E+00   0.00000E+00 
c  Pressure     0.91626E+02     518   0.72465E-02   0.14824E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -5119.1          2447.6         -10.501         -4.5678
v  Velocity[Y]                  -11058           23083          12.158          4.5531
v  Velocity[Z]                 -3207.5          7502.3         0.71471          1.2971
v  ǁVelocityǁ                  0.15254           23175           80.52          52.275
v  Pressure                 -1.125e+06      2.3967e+06      4.7573e+05      3.2577e+05
v  turbulent_viscosity        0.029333          3551.9          6.0296          3.3266
v  CourantNb                    3.9659      4.1992e+07           28767           13970
v  FourierNb                    16.446      2.8916e+07           10808          4127.9
v  total_pressure          -6.2499e+05      2.8967e+06      9.7573e+05      8.2577e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          89.431       5.859e+07           39575           18098


 TIME FOR THE TIME STEP              142:        0.82105E+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        -0.101053374E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273500106E+00
Free inlet               13           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 0.26522E+05
   Friction velocity        uet   :  0.76503E-01 0.11240E+04
   Friction velocity        uk    :  0.76503E-01 0.11240E+04
   Dimensionless distance   yplus :  0.11323E+01 0.10165E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          9
   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    0.39542E+06    5240   0.95152E+00   0.21091E+05 
c  VelocityY    0.39542E+06    5240   0.95152E+00   0.00000E+00 
c  VelocityZ    0.39542E+06    5240   0.95152E+00   0.00000E+00 
c  Pressure     0.97842E+02     602   0.75459E-02   0.14706E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -5646.2          2239.6         -10.083         -4.4777
v  Velocity[Y]                  -11923           25419          9.6389          4.6508
v  Velocity[Z]                 -2884.1            8674        -0.65594         0.53735
v  ǁVelocityǁ                  0.20757           25604          96.031          62.535
v  Pressure                -1.2006e+06      2.6159e+06      5.0865e+05      3.4851e+05
v  turbulent_viscosity        0.018113          3868.8          5.8519          3.2335
v  CourantNb                    1.0514      4.6442e+07           27347           13289
v  FourierNb                    17.262      3.0662e+07           10622          4011.3
v  total_pressure          -7.0059e+05      3.1159e+06      1.0086e+06      8.4851e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          60.542         6.5e+07           37969           17300


 TIME FOR THE TIME STEP              143:        0.91179E+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        -0.220095836E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273472069E+00
Free inlet               13           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 0.29252E+05
   Friction velocity        uet   :  0.67983E-01 0.12286E+04
   Friction velocity        uk    :  0.67983E-01 0.12286E+04
   Dimensionless distance   yplus :  0.11157E+01 0.11111E+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         44 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.45410E+06    4939   0.94403E+00   0.24510E+05 
c  VelocityY    0.45410E+06    4939   0.94403E+00   0.00000E+00 
c  VelocityZ    0.45410E+06    4939   0.94403E+00   0.00000E+00 
c  Pressure     0.10716E+03     587   0.73874E-02   0.14955E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -6145.3          2962.5         -14.012         -4.7398
v  Velocity[Y]                  -13287           27647            12.5          4.9956
v  Velocity[Z]                 -3862.4          8941.2         0.56942          1.9062
v  ǁVelocityǁ                  0.25159           27754          105.58          67.169
v  Pressure                -1.2794e+06      2.8017e+06      5.3625e+05       3.681e+05
v  turbulent_viscosity        0.022234            4264          6.4377          3.5776
v  CourantNb                    11.494      5.0472e+07           31236           15357
v  FourierNb                    14.624      3.4821e+07           11645          4416.1
v  total_pressure          -7.7945e+05      3.3017e+06      1.0362e+06       8.681e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          54.387      7.1008e+07           42881           19774


 TIME FOR THE TIME STEP              144:        0.86817E+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         0.345745297E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273506212E+00
Free inlet               13           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 0.31841E+05
   Friction velocity        uet   :  0.70509E-01 0.13271E+04
   Friction velocity        uk    :  0.70509E-01 0.13271E+04
   Dimensionless distance   yplus :  0.11126E+01 0.12002E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          9
   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    0.56847E+06    4884   0.94816E+00   0.32096E+05 
c  VelocityY    0.56847E+06    4884   0.94816E+00   0.00000E+00 
c  VelocityZ    0.56847E+06    4884   0.94816E+00   0.00000E+00 
c  Pressure     0.11562E+03     612   0.79755E-02   0.14970E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -6737.8          2583.9         -12.642          -4.768
v  Velocity[Y]                  -14465           30395          4.6997           4.924
v  Velocity[Z]                 -3464.6           10551          4.9142         0.96995
v  ǁVelocityǁ                  0.23665           30630             108          70.025
v  Pressure                -1.3571e+06      3.1003e+06      5.8487e+05      4.0238e+05
v  turbulent_viscosity        0.033102          4634.6          6.9728           3.829
v  CourantNb                    3.9384       5.597e+07           34826           16741
v  FourierNb                    23.708      3.6729e+07           12724          4758.3
v  total_pressure          -8.5711e+05      3.6003e+06      1.0849e+06      9.0238e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          55.879      7.8008e+07           47549           21499


 TIME FOR THE TIME STEP              145:        0.86400E+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        -0.337533330E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273628029E+00
Free inlet               13           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 0.35083E+05
   Friction velocity        uet   :  0.64223E-01 0.14496E+04
   Friction velocity        uk    :  0.64223E-01 0.14496E+04
   Dimensionless distance   yplus :  0.10927E+01 0.13109E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          7
   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    0.65445E+06    4830   0.94684E+00   0.31569E+05 
c  VelocityY    0.65445E+06    4830   0.94684E+00   0.00000E+00 
c  VelocityZ    0.65445E+06    4830   0.94684E+00   0.00000E+00 
c  Pressure     0.12620E+03     569   0.73968E-02   0.15156E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -7383.3          3558.7         -14.428         -5.9896
v  Velocity[Y]                  -15915           33248           15.29          5.5346
v  Velocity[Z]                 -4787.5           10720        -0.15757          2.8001
v  ǁVelocityǁ                  0.25899           33369           115.1          75.307
v  Pressure                -1.5038e+06      3.3161e+06      6.1241e+05      4.2174e+05
v  turbulent_viscosity        0.037403          5141.7          7.7475          4.3023
v  CourantNb                    8.2676      6.0734e+07           35571           17376
v  FourierNb                    22.811      4.5167e+07           14051          5314.5
v  total_pressure          -1.0038e+06      3.8161e+06      1.1124e+06      9.2174e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          45.098      8.4641e+07           49622           22691


 TIME FOR THE TIME STEP              146:        0.83795E+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        -0.244227415E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273565593E+00
Free inlet               13           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 0.38360E+05
   Friction velocity        uet   :  0.92737E-01 0.15724E+04
   Friction velocity        uk    :  0.92737E-01 0.15724E+04
   Dimensionless distance   yplus :  0.10352E+01 0.14220E+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         30 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.81554E+06    5395   0.94898E+00   0.75044E+05 
c  VelocityY    0.81554E+06    5395   0.94898E+00   0.00000E+00 
c  VelocityZ    0.81554E+06    5395   0.94898E+00   0.00000E+00 
c  Pressure     0.13559E+03     609   0.82678E-02   0.15106E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -7983.8          3295.2         -6.3398         -5.4097
v  Velocity[Y]                  -17288           36606          14.311           5.106
v  Velocity[Z]                 -3883.3           12760          7.7965          2.2089
v  ǁVelocityǁ                  0.24266           36892          144.07          99.526
v  Pressure                 -1.626e+06      3.6579e+06      6.6323e+05       4.569e+05
v  turbulent_viscosity        0.036837            5582           7.877          4.3742
v  CourantNb                    26.364      6.7377e+07           38549           18600
v  FourierNb                    24.529      4.7764e+07           14461          5395.4
v  total_pressure           -1.126e+06      4.1579e+06      1.1632e+06       9.569e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          113.71      9.3943e+07           53010           23995


 TIME FOR THE TIME STEP              147:        0.94728E+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        -0.211441502E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273605279E+00
Free inlet               13           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 0.42324E+05
   Friction velocity        uet   :  0.71469E-01 0.17198E+04
   Friction velocity        uk    :  0.71469E-01 0.17198E+04
   Dimensionless distance   yplus :  0.11148E+01 0.15553E+05
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          8
   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    0.94244E+06    5013   0.94263E+00   0.89305E+05 
c  VelocityY    0.94244E+06    5013   0.94263E+00   0.00000E+00 
c  VelocityZ    0.94244E+06    5013   0.94263E+00   0.00000E+00 
c  Pressure     0.14822E+03     567   0.71863E-02   0.15296E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -8789.2          4327.5         -13.803         -6.4364
v  Velocity[Y]                  -19202           39891          21.046          5.8438
v  Velocity[Z]                 -5667.9           12809          -3.413          3.2327
v  ǁVelocityǁ                    0.481           40036          127.89           84.87
v  Pressure                -1.8717e+06      3.9181e+06      6.9344e+05      4.7769e+05
v  turbulent_viscosity        0.027963          6146.7          9.2869           5.408
v  CourantNb                    9.8154      7.2714e+07           45241           22840
v  FourierNb                    21.702      5.0255e+07           16698          6423.9
v  total_pressure          -1.3717e+06      4.4181e+06      1.1934e+06      9.7769e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           68.42      1.0131e+08           61940           29264


 TIME FOR THE TIME STEP              148:        0.88013E+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        -0.198460006E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273681953E+00
Free inlet               13           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 0.46151E+05
   Friction velocity        uet   :  0.78816E-01 0.18611E+04
   Friction velocity        uk    :  0.78816E-01 0.18611E+04
   Dimensionless distance   yplus :  0.10072E+01 0.16831E+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         31 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.11776E+07    5242   0.94906E+00   0.82165E+05 
c  VelocityY    0.11776E+07    5242   0.94906E+00   0.00000E+00 
c  VelocityZ    0.11776E+07    5242   0.94906E+00   0.00000E+00 
c  Pressure     0.16058E+03     643   0.86014E-02   0.15344E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -9744.5          3833.1         -16.173          -6.554
v  Velocity[Y]                  -20759           43878          13.483          5.1392
v  Velocity[Z]                 -5042.2           15165          10.588           2.645
v  ǁVelocityǁ                  0.67266           44197          162.88          107.36
v  Pressure                -1.9884e+06      4.3564e+06      7.7692e+05      5.3808e+05
v  turbulent_viscosity         0.02971          6699.3          8.9341          4.9146
v  CourantNb                    9.0405      8.1009e+07           43644           21133
v  FourierNb                    25.836       5.745e+07           16591          6093.9
v  total_pressure          -1.4884e+06      4.8564e+06      1.2769e+06      1.0381e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          96.587      1.1416e+08           60235           27227


 TIME FOR THE TIME STEP              149:        0.78417E+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        -0.634571504E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273692810E+00
Free inlet               13           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 0.50836E+05
   Friction velocity        uet   :  0.59473E-01 0.20328E+04
   Friction velocity        uk    :  0.59473E-01 0.20328E+04
   Dimensionless distance   yplus :  0.11864E+01 0.18384E+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         32 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:    0.85567E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.13596E+07    5893   0.94443E+00   0.82337E+05 
c  VelocityY    0.13596E+07    5893   0.94443E+00   0.00000E+00 
c  VelocityZ    0.13596E+07    5893   0.94443E+00   0.00000E+00 
c  Pressure     0.17464E+03     588   0.73435E-02   0.15452E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -10595          5203.7         -23.011         -7.6382
v  Velocity[Y]                  -23036           47832           12.14          5.6167
v  Velocity[Z]                 -6843.2           15523          7.1412          4.1241
v  ǁVelocityǁ                  0.34479           48011          147.49          94.551
v  Pressure                -2.2813e+06      4.6698e+06      8.1629e+05      5.6432e+05
v  turbulent_viscosity         0.09293          7412.4          11.005          6.1747
v  CourantNb                    6.7986      8.7814e+07           51988           25300
v  FourierNb                    37.994       6.504e+07           20035          7535.2
v  total_pressure          -1.7813e+06      5.1698e+06      1.3163e+06      1.0643e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          122.36      1.2214e+08           72023           32835


 TIME FOR THE TIME STEP              150:        0.10138E+02

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


 INSTANT    0.151000000E+02   TIME STEP NUMBER             151
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.190536122E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273714167E+00
Free inlet               13           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 0.55430E+05
   Friction velocity        uet   :  0.98233E-01 0.22000E+04
   Friction velocity        uk    :  0.98233E-01 0.22000E+04
   Dimensionless distance   yplus :  0.10682E+01 0.19895E+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         37 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.16925E+07    4914   0.94761E+00   0.16379E+06 
c  VelocityY    0.16925E+07    4914   0.94761E+00   0.00000E+00 
c  VelocityZ    0.16925E+07    4914   0.94761E+00   0.00000E+00 
c  Pressure     0.18910E+03     641   0.90649E-02   0.15486E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -11805          4479.2          -15.84           -6.73
v  Velocity[Y]                  -24958           52681          29.187          5.8275
v  Velocity[Z]                   -5836           18138          1.2979          3.7512
v  ǁVelocityǁ                  0.94721           53092          217.51           149.9
v  Pressure                -2.4209e+06      5.1951e+06      9.1199e+05      6.3124e+05
v  turbulent_viscosity         0.03318          8046.4          10.289          5.5921
v  CourantNb                    13.661      9.7377e+07           50890           24055
v  FourierNb                    23.197      6.3673e+07           19195            6983
v  total_pressure          -1.9209e+06      5.6951e+06       1.412e+06      1.1312e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          101.33      1.3576e+08           70085           31038


 TIME FOR THE TIME STEP              151:        0.90204E+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         0.588897200E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273680387E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.20852E+00 0.61175E+05
   Friction velocity        uet   :  0.86729E-01 0.24075E+04
   Friction velocity        uk    :  0.86729E-01 0.24075E+04
   Dimensionless distance   yplus :  0.11994E+01 0.21772E+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         39 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.19510E+07    4943   0.94457E+00   0.14813E+06 
c  VelocityY    0.19510E+07    4943   0.94457E+00   0.00000E+00 
c  VelocityZ    0.19510E+07    4943   0.94457E+00   0.00000E+00 
c  Pressure     0.20609E+03     537   0.70690E-02   0.15623E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -12889          6137.6         -23.295         -8.8916
v  Velocity[Y]                  -27586           57603           21.18          7.2501
v  Velocity[Z]                 -8170.9           18566            3.44          5.8342
v  ǁVelocityǁ                  0.80696           57817          155.55          104.57
v  Pressure                -2.7852e+06      5.5619e+06      9.4898e+05      6.5809e+05
v  turbulent_viscosity        0.062964            8879          13.406          7.9116
v  CourantNb                     12.57      1.0522e+08           66611           33276
v  FourierNb                     37.08      7.2531e+07           24122          9268.1
v  total_pressure          -2.2852e+06      6.0619e+06       1.449e+06      1.1581e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          158.87      1.4651e+08           90733           42544


 TIME FOR THE TIME STEP              152:        0.74519E+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         0.100896430E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273696748E+00
Free inlet               13           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 0.66873E+05
   Friction velocity        uet   :  0.15248E+00 0.26118E+04
   Friction velocity        uk    :  0.15248E+00 0.26118E+04
   Dimensionless distance   yplus :  0.18921E+01 0.23620E+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         25 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.24398E+07    4884   0.94699E+00   0.22958E+06 
c  VelocityY    0.24398E+07    4884   0.94699E+00   0.00000E+00 
c  VelocityZ    0.24398E+07    4884   0.94699E+00   0.00000E+00 
c  Pressure     0.22557E+03     675   0.10126E-01   0.15805E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -13435          6049.8         -3.8911         -8.6139
v  Velocity[Y]                  -30101           63231          29.121          3.6315
v  Velocity[Z]                 -6808.9           22257          12.172          6.4959
v  ǁVelocityǁ                   0.8413           63717          289.12          204.48
v  Pressure                -2.8531e+06      6.2991e+06      1.1189e+06      7.7922e+05
v  turbulent_viscosity        0.069931          9674.6          11.703          6.5212
v  CourantNb                    41.821      1.1694e+08           55333           26431
v  FourierNb                    43.001      7.6489e+07           21863          7994.2
v  total_pressure          -2.3531e+06      6.7991e+06      1.6189e+06      1.2792e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          203.41      1.6294e+08           77196           34425


 TIME FOR THE TIME STEP              153:        0.86108E+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        -0.207200560E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273872970E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.26133E+00 0.73574E+05
   Friction velocity        uet   :  0.85005E-01 0.28503E+04
   Friction velocity        uk    :  0.85005E-01 0.28503E+04
   Dimensionless distance   yplus :  0.18353E+01 0.25777E+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    0.27808E+07    5972   0.94149E+00   0.29208E+06 
c  VelocityY    0.27808E+07    5972   0.94149E+00   0.00000E+00 
c  VelocityZ    0.27808E+07    5972   0.94149E+00   0.00000E+00 
c  Pressure     0.24352E+03     535   0.69947E-02   0.15783E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -14868          7290.9         -28.038         -9.6928
v  Velocity[Y]                  -33234           68850          22.309          6.4848
v  Velocity[Z]                   -9975           22402          -2.778          6.9247
v  ǁVelocityǁ                  0.37413           69126          175.35          117.34
v  Pressure                -3.3024e+06      6.7239e+06      1.1544e+06      8.0141e+05
v  turbulent_viscosity         0.14708           10686          16.506          9.9095
v  CourantNb                    2.5145      1.2686e+08           85243           43463
v  FourierNb                    61.032      9.3904e+07           29729           11429
v  total_pressure          -2.8024e+06      7.2239e+06      1.6544e+06      1.3014e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          99.545      1.7654e+08      1.1497e+05           54892


 TIME FOR THE TIME STEP              154:        0.10338E+02

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


 INSTANT    0.155000000E+02   TIME STEP NUMBER             155
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.252802387E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273838552E+00
Free inlet               13           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 0.80103E+05
   Friction velocity        uet   :  0.70911E-01 0.30812E+04
   Friction velocity        uk    :  0.70911E-01 0.30812E+04
   Dimensionless distance   yplus :  0.11633E+01 0.27864E+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         32 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.34766E+07    6659   0.94875E+00   0.25140E+06 
c  VelocityY    0.34766E+07    6659   0.94875E+00   0.00000E+00 
c  VelocityZ    0.34766E+07    6659   0.94875E+00   0.00000E+00 
c  Pressure     0.26304E+03     640   0.89763E-02   0.15754E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -17212          7026.1          -31.94         -9.1667
v  Velocity[Y]                  -36031           76068        -0.94257          6.0339
v  Velocity[Z]                 -8619.3           26221          30.267          5.9574
v  ǁVelocityǁ                  0.96231           76628          275.98          181.92
v  Pressure                 -3.583e+06      7.4053e+06      1.2698e+06      8.8271e+05
v  turbulent_viscosity        0.060235           11590          13.047          7.2537
v  CourantNb                    31.854      1.4137e+08           63438           29971
v  FourierNb                    26.865       9.174e+07           24620          8899.8
v  total_pressure           -3.083e+06      7.9053e+06      1.7698e+06      1.3827e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           98.45      1.9548e+08           88058           38871


 TIME FOR THE TIME STEP              155:        0.96837E+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         0.195465465E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273837245E+00
Free inlet               13           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 0.88652E+05
   Friction velocity        uet   :  0.44314E-01 0.33812E+04
   Friction velocity        uk    :  0.44314E-01 0.33812E+04
   Dimensionless distance   yplus :  0.11797E+01 0.30578E+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         33 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.40607E+07    5118   0.94423E+00   0.19654E+06 
c  VelocityY    0.40607E+07    5118   0.94423E+00   0.00000E+00 
c  VelocityZ    0.40607E+07    5118   0.94423E+00   0.00000E+00 
c  Pressure     0.28814E+03     568   0.72428E-02   0.15942E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -18385            8969         -28.526          -12.18
v  Velocity[Y]                  -39792           82865           18.29          7.2203
v  Velocity[Z]                  -11716           26949          13.417           9.925
v  ǁVelocityǁ                  0.19276           83188           220.2          140.45
v  Pressure                -4.1109e+06      7.9319e+06      1.3186e+06      9.1743e+05
v  turbulent_viscosity        0.083709           12830          17.503          9.8209
v  CourantNb                    19.257      1.5231e+08           87161           41809
v  FourierNb                    47.999      1.0463e+08           32426           11920
v  total_pressure          -3.6109e+06      8.4319e+06      1.8186e+06      1.4174e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           124.7      2.1277e+08      1.1959e+05           53729


 TIME FOR THE TIME STEP              156:        0.76787E+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        -0.114801357E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273797219E+00
Free inlet               13           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 0.96567E+05
   Friction velocity        uet   :  0.10892E+00 0.36570E+04
   Friction velocity        uk    :  0.10892E+00 0.36570E+04
   Dimensionless distance   yplus :  0.11767E+01 0.33072E+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         30 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.50487E+07    5088   0.94648E+00   0.58939E+06 
c  VelocityY    0.50487E+07    5088   0.94648E+00   0.00000E+00 
c  VelocityZ    0.50487E+07    5088   0.94648E+00   0.00000E+00 
c  Pressure     0.31920E+03     680   0.11925E-01   0.16272E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -20833          7312.5         -33.829         -12.564
v  Velocity[Y]                  -43231           90743          111.73         0.27538
v  Velocity[Z]                 -9781.1           32006           6.298          5.3089
v  ǁVelocityǁ                   4.1513           91548          509.32          352.04
v  Pressure                -4.1876e+06      9.0028e+06      1.5873e+06      1.1123e+06
v  turbulent_viscosity        0.043907           13924          15.607          8.4813
v  CourantNb                    47.677      1.6887e+08           78283           35971
v  FourierNb                    37.067       1.101e+08           29746           10563
v  total_pressure          -3.6876e+06      9.5028e+06      2.0873e+06      1.6123e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          128.51      2.3572e+08      1.0803e+05           46533


 TIME FOR THE TIME STEP              157:        0.90118E+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        -0.320221348E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274103855E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.54848E+00 0.10594E+06
   Friction velocity        uet   :  0.15413E+00 0.39816E+04
   Friction velocity        uk    :  0.15413E+00 0.39816E+04
   Dimensionless distance   yplus :  0.22492E+01 0.36007E+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         46 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.58174E+07    5284   0.94274E+00   0.58275E+06 
c  VelocityY    0.58174E+07    5284   0.94274E+00   0.00000E+00 
c  VelocityZ    0.58174E+07    5284   0.94274E+00   0.00000E+00 
c  Pressure     0.34207E+03     518   0.68058E-02   0.16109E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -22265           10757         -39.783         -13.994
v  Velocity[Y]                  -47885           99651          25.763          7.4784
v  Velocity[Z]                  -14058           32256          13.297          9.0383
v  ǁVelocityǁ                   1.5055      1.0004e+05          249.06          162.15
v  Pressure                -4.8189e+06      9.6376e+06       1.622e+06      1.1338e+06
v  turbulent_viscosity         0.26802           15325           24.98           15.46
v  CourantNb                    37.713      1.8211e+08      1.4292e+05           71666
v  FourierNb                    98.185      1.3456e+08           44575           17397
v  total_pressure          -4.3189e+06      1.0138e+07       2.122e+06      1.6338e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1001.6      2.5446e+08      1.8749e+05           89063


 TIME FOR THE TIME STEP              158:        0.92251E+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        -0.401457500E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.272557229E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.27561E+00 0.11639E+06
   Friction velocity        uet   :  0.10690E+00 0.43407E+04
   Friction velocity        uk    :  0.10690E+00 0.43407E+04
   Dimensionless distance   yplus :  0.14901E+01 0.39255E+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         39 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.73170E+07    5030   0.94949E+00   0.57610E+06 
c  VelocityY    0.73170E+07    5030   0.94949E+00   0.00000E+00 
c  VelocityZ    0.73170E+07    5030   0.94949E+00   0.00000E+00 
c  Pressure     0.37110E+03     690   0.10290E-01   0.16122E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -24483            9748         -47.875         -15.303
v  Velocity[Y]                  -51886      1.0956e+05         -4.3453          1.1579
v  Velocity[Z]                  -12464           37940          47.114          12.891
v  ǁVelocityǁ                   1.9052      1.1038e+05          455.35          316.26
v  Pressure                -4.9866e+06      1.0857e+07      1.9172e+06      1.3503e+06
v  turbulent_viscosity        0.079175           16818          18.544          10.178
v  CourantNb                    53.459      2.0305e+08           89401           41131
v  FourierNb                    53.302      1.3284e+08           35423           12569
v  total_pressure          -4.4866e+06      1.1357e+07      2.4172e+06      1.8503e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           194.2      2.8303e+08      1.2482e+05           53701


 TIME FOR THE TIME STEP              159:        0.79917E+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        -0.524638316E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.273943733E+00
Free inlet               13           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 0.12812E+06
   Friction velocity        uet   :  0.29386E+00 0.47411E+04
   Friction velocity        uk    :  0.29386E+00 0.47411E+04
   Dimensionless distance   yplus :  0.15851E+01 0.42877E+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    0.84348E+07    5798   0.94200E+00   0.63723E+06 
c  VelocityY    0.84348E+07    5798   0.94200E+00   0.00000E+00 
c  VelocityZ    0.84348E+07    5798   0.94200E+00   0.00000E+00 
c  Pressure     0.40605E+03     548   0.74547E-02   0.16277E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -26582           12867         -54.593         -16.424
v  Velocity[Y]                  -57746      1.1923e+05          30.201          6.9118
v  Velocity[Z]                  -17331           38345         -5.8192          14.453
v  ǁVelocityǁ                  0.54243      1.1966e+05          307.77          198.91
v  Pressure                -5.7896e+06      1.1567e+07      1.9744e+06      1.3864e+06
v  turbulent_viscosity         0.41224           18514          25.909          15.579
v  CourantNb                    42.282      2.2016e+08      1.3709e+05           67361
v  FourierNb                    151.93      1.5088e+08           47542           17886
v  total_pressure          -5.2896e+06      1.2067e+07      2.4744e+06      1.8864e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          649.83       3.055e+08      1.8463e+05           85247


 TIME FOR THE TIME STEP              160:        0.10049E+02

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


 INSTANT    0.161000000E+02   TIME STEP NUMBER             161
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.664989981E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274042462E+00
Free inlet               13           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 0.13952E+06
   Friction velocity        uet   :  0.72357E-01 0.51273E+04
   Friction velocity        uk    :  0.72357E-01 0.51273E+04
   Dimensionless distance   yplus :  0.11093E+01 0.46369E+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         33 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10333E+08    5761   0.94475E+00   0.12639E+07 
c  VelocityY    0.10333E+08    5761   0.94475E+00   0.00000E+00 
c  VelocityZ    0.10333E+08    5761   0.94475E+00   0.00000E+00 
c  Pressure     0.44798E+03     647   0.11489E-01   0.16504E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -29601           11192         -57.874         -15.456
v  Velocity[Y]                  -62575      1.3094e+05          51.293           4.384
v  Velocity[Z]                  -13590           46700          27.728          16.732
v  ǁVelocityǁ                   1.7107      1.3184e+05          545.45          384.83
v  Pressure                -6.1394e+06      1.2876e+07      2.2065e+06       1.552e+06
v  turbulent_viscosity        0.088657           20114          21.771          11.951
v  CourantNb                    33.377      2.4489e+08      1.0907e+05           50024
v  FourierNb                    50.772      1.5903e+08           41848           14758
v  total_pressure          -5.6394e+06      1.3376e+07      2.7065e+06       2.052e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          204.05      3.4045e+08      1.5092e+05           64782


 TIME FOR THE TIME STEP              161:        0.85158E+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        -0.147838420E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274480790E+00
Free inlet               13           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 0.15352E+06
   Friction velocity        uet   :  0.95085E-01 0.55990E+04
   Friction velocity        uk    :  0.95085E-01 0.55990E+04
   Dimensionless distance   yplus :  0.20277E+01 0.50635E+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         41 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.11933E+08    5710   0.94519E+00   0.13376E+07 
c  VelocityY    0.11933E+08    5710   0.94519E+00   0.00000E+00 
c  VelocityZ    0.11933E+08    5710   0.94519E+00   0.00000E+00 
c  Pressure     0.48191E+03     534   0.69180E-02   0.16363E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -32071           15500         -48.158         -19.636
v  Velocity[Y]                  -68852       1.438e+05           40.56          6.3793
v  Velocity[Z]                  -20412           46759          29.286          18.088
v  ǁVelocityǁ                   0.3628      1.4433e+05          386.06           242.9
v  Pressure                 -7.067e+06      1.3778e+07      2.2694e+06      1.5937e+06
v  turbulent_viscosity         0.14509           21902          31.377          18.686
v  CourantNb                    28.857      2.6362e+08      1.6148e+05           81089
v  FourierNb                    84.598      1.7874e+08           57272           21638
v  total_pressure           -6.567e+06      1.4278e+07      2.7694e+06      2.0937e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           483.1       3.673e+08      2.1875e+05      1.0273e+05


 TIME FOR THE TIME STEP              162:        0.99134E+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        -0.456018280E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274261985E+00
Free inlet               13           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 0.16846E+06
   Friction velocity        uet   :  0.72000E-01 0.60983E+04
   Friction velocity        uk    :  0.72000E-01 0.60983E+04
   Dimensionless distance   yplus :  0.11544E+01 0.55150E+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         40 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.15145E+08    5984   0.94753E+00   0.12538E+07 
c  VelocityY    0.15145E+08    5984   0.94753E+00   0.00000E+00 
c  VelocityZ    0.15145E+08    5984   0.94753E+00   0.00000E+00 
c  Pressure     0.52362E+03     641   0.10410E-01   0.16356E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -35077           14190         -93.765           -18.5
v  Velocity[Y]                  -74915      1.5753e+05         -13.029           3.655
v  Velocity[Z]                  -18474           54213          74.044          16.051
v  ǁVelocityǁ                   2.5246      1.5865e+05          599.51          412.59
v  Pressure                -7.5542e+06      1.5283e+07      2.5048e+06      1.7557e+06
v  turbulent_viscosity        0.065627           24210          25.423          13.854
v  CourantNb                    2.1521      2.9345e+08      1.3385e+05           60257
v  FourierNb                    46.945      1.9109e+08           49210           17220
v  total_pressure          -7.0542e+06      1.5783e+07      3.0048e+06      2.2557e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          197.76      4.0933e+08      1.8306e+05           77477


 TIME FOR THE TIME STEP              163:        0.89463E+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        -0.663364203E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274416061E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.12257E+00 0.18495E+06
   Friction velocity        uet   :  0.54106E-01 0.66462E+04
   Friction velocity        uk    :  0.54106E-01 0.66462E+04
   Dimensionless distance   yplus :  0.13066E+01 0.60105E+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    0.17525E+08    5172   0.94090E+00   0.11958E+07 
c  VelocityY    0.17525E+08    5172   0.94090E+00   0.00000E+00 
c  VelocityZ    0.17525E+08    5172   0.94090E+00   0.00000E+00 
c  Pressure     0.57248E+03     516   0.73067E-02   0.16481E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -38860           18191         -62.281         -22.548
v  Velocity[Y]                  -83259      1.7188e+05          27.461          8.6416
v  Velocity[Z]                  -25003           55228          26.338          24.328
v  ǁVelocityǁ                   2.0142      1.7251e+05          373.42          258.16
v  Pressure                -8.6694e+06       1.635e+07      2.5725e+06      1.8063e+06
v  turbulent_viscosity         0.25505           26692          35.176          20.329
v  CourantNb                     34.94      3.1894e+08      1.8202e+05           89367
v  FourierNb                    109.02      2.1737e+08           65370           24060
v  total_pressure          -8.1694e+06       1.685e+07      3.0725e+06      2.3063e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          250.42      4.4196e+08      2.4739e+05      1.1343e+05


 TIME FOR THE TIME STEP              164:        0.81634E+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         0.437476119E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274491848E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.20939E+00 0.20186E+06
   Friction velocity        uet   :  0.11245E+00 0.72041E+04
   Friction velocity        uk    :  0.11245E+00 0.72041E+04
   Dimensionless distance   yplus :  0.11030E+01 0.65150E+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         29 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.21874E+08    4554   0.94752E+00   0.22843E+07 
c  VelocityY    0.21874E+08    4554   0.94752E+00   0.00000E+00 
c  VelocityZ    0.21874E+08    4554   0.94752E+00   0.00000E+00 
c  Pressure     0.62724E+03     682   0.11089E-01   0.16610E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -40443           18642         -21.516         -21.004
v  Velocity[Y]                  -89777      1.8975e+05          77.268         -4.8095
v  Velocity[Z]                  -19555           67476           27.89          23.565
v  ǁVelocityǁ                   4.4749      1.9128e+05          851.26          620.13
v  Pressure                -8.8902e+06      1.8544e+07      3.0774e+06      2.1745e+06
v  turbulent_viscosity         0.18956           29044          29.031          16.073
v  CourantNb                    154.22       3.531e+08      1.3793e+05           63877
v  FourierNb                    118.37      2.2953e+08           56491           19674
v  total_pressure          -8.3902e+06      1.9044e+07      3.5774e+06      2.6745e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          673.34      4.9123e+08      1.9442e+05           83552


 TIME FOR THE TIME STEP              165:        0.69727E+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         0.574449071E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275005329E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.27538E+01 0.22307E+06
   Friction velocity        uet   :  0.40536E+00 0.78991E+04
   Friction velocity        uk    :  0.40536E+00 0.78991E+04
   Dimensionless distance   yplus :  0.76319E+01 0.71436E+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    0.24930E+08    6533   0.94121E+00   0.29693E+07 
c  VelocityY    0.24930E+08    6533   0.94121E+00   0.00000E+00 
c  VelocityZ    0.24930E+08    6533   0.94121E+00   0.00000E+00 
c  Pressure     0.68051E+03     554   0.69920E-02   0.16596E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -44582           22261         -80.243         -24.934
v  Velocity[Y]                  -99427      2.0626e+05          50.853          5.5913
v  Velocity[Z]                  -29464           67073         -14.285          27.147
v  ǁVelocityǁ                  0.74708      2.0709e+05           482.4          332.59
v  Pressure                -1.0272e+07      1.9787e+07      3.1692e+06      2.2365e+06
v  turbulent_viscosity         0.81639           32045          43.731          26.876
v  CourantNb                    145.92      3.8178e+08       2.444e+05      1.2425e+05
v  FourierNb                    307.82      2.6043e+08           79909           30307
v  total_pressure          -9.7719e+06      2.0287e+07      3.6692e+06      2.7365e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          990.82      5.3181e+08      3.2431e+05      1.5456e+05


 TIME FOR THE TIME STEP              166:        0.11377E+02

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


 INSTANT    0.167000000E+02   TIME STEP NUMBER             167
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.125961619E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.274914589E+00
Free inlet               13           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 0.24247E+06
   Friction velocity        uet   :  0.14550E+00 0.85309E+04
   Friction velocity        uk    :  0.14550E+00 0.85309E+04
   Dimensionless distance   yplus :  0.13784E+01 0.77149E+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         39 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30639E+08    6786   0.94542E+00   0.26591E+07 
c  VelocityY    0.30639E+08    6786   0.94542E+00   0.00000E+00 
c  VelocityZ    0.30639E+08    6786   0.94542E+00   0.00000E+00 
c  Pressure     0.73638E+03     643   0.96426E-02   0.16515E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -52166           20683         -105.07         -22.742
v  Velocity[Y]             -1.0855e+05      2.2662e+05         -35.784          3.6189
v  Velocity[Z]                  -25460           79199          120.05          25.787
v  ǁVelocityǁ                   2.9808      2.2798e+05          752.78          485.06
v  Pressure                -1.1128e+07      2.1792e+07      3.5031e+06      2.4763e+06
v  turbulent_viscosity         0.20303           34759          32.962          18.419
v  CourantNb                     79.83      4.2584e+08      1.7247e+05           79934
v  FourierNb                     97.51      2.7504e+08           64668           22405
v  total_pressure          -1.0628e+07      2.2292e+07      4.0031e+06      2.9763e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          227.27       5.882e+08      2.3714e+05      1.0234e+05


 TIME FOR THE TIME STEP              167:        0.11797E+02

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


 INSTANT    0.168000000E+02   TIME STEP NUMBER             168
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.329294019E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275028321E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.64046E+00 0.26708E+06
   Friction velocity        uet   :  0.14974E+00 0.93269E+04
   Friction velocity        uk    :  0.14974E+00 0.93269E+04
   Dimensionless distance   yplus :  0.22706E+01 0.84348E+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         40 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.35720E+08    5503   0.94338E+00   0.21611E+07 
c  VelocityY    0.35720E+08    5503   0.94338E+00   0.00000E+00 
c  VelocityZ    0.35720E+08    5503   0.94338E+00   0.00000E+00 
c  Pressure     0.81083E+03     441   0.76676E-02   0.16733E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -55251           26796         -42.679         -31.551
v  Velocity[Y]             -1.1949e+05      2.4835e+05          55.169           8.442
v  Velocity[Z]                  -35665           80270          38.929          35.924
v  ǁVelocityǁ                    4.443      2.4925e+05           609.6          405.25
v  Pressure                -1.2924e+07      2.3154e+07      3.5388e+06      2.5013e+06
v  turbulent_viscosity         0.22259           37948          47.283          25.656
v  CourantNb                    87.462      4.5924e+08      2.3719e+05      1.0998e+05
v  FourierNb                    120.15      3.3551e+08           90715           31827
v  total_pressure          -1.2424e+07      2.3654e+07      4.0388e+06      3.0013e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           409.7      6.4047e+08      3.2791e+05      1.4181e+05


 TIME FOR THE TIME STEP              168:        0.95756E+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         0.378447409E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.272258973E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.15297E+01 0.29243E+06
   Friction velocity        uet   :  0.28518E+00 0.10142E+05
   Friction velocity        uk    :  0.28518E+00 0.10142E+05
   Dimensionless distance   yplus :  0.37310E+01 0.91718E+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         41 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.45280E+08    5724   0.94592E+00   0.29168E+07 
c  VelocityY    0.45280E+08    5724   0.94592E+00   0.00000E+00 
c  VelocityZ    0.45280E+08    5724   0.94592E+00   0.00000E+00 
c  Pressure     0.89648E+03     672   0.12024E-01   0.16954E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -62019           22971         -104.71         -28.394
v  Velocity[Y]             -1.3023e+05      2.7173e+05          81.083         0.81317
v  Velocity[Z]                  -31679           94448          97.864            32.9
v  ǁVelocityǁ                   3.6981      2.7376e+05          1013.4          696.87
v  Pressure                -1.3488e+07      2.6033e+07      4.1084e+06      2.9193e+06
v  turbulent_viscosity          0.1557           41816          41.986          22.849
v  CourantNb                    34.819      5.0954e+08      2.1187e+05           95939
v  FourierNb                    99.782      3.3028e+08           82279           28321
v  total_pressure          -1.2988e+07      2.6533e+07      4.6084e+06      3.4193e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          500.29      7.1012e+08      2.9415e+05      1.2426e+05


 TIME FOR THE TIME STEP              169:        0.86790E+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        -0.177026362E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275018702E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.16611E+01 0.32062E+06
   Friction velocity        uet   :  0.28454E+00 0.11042E+05
   Friction velocity        uk    :  0.28454E+00 0.11042E+05
   Dimensionless distance   yplus :  0.58581E+01 0.99856E+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         37 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.52299E+08    5960   0.94337E+00   0.33563E+07 
c  VelocityY    0.52299E+08    5960   0.94337E+00   0.00000E+00 
c  VelocityZ    0.52299E+08    5960   0.94337E+00   0.00000E+00 
c  Pressure     0.96431E+03     530   0.71910E-02   0.16780E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -66629           32669         -104.21         -35.713
v  Velocity[Y]               -1.44e+05      2.9723e+05          64.729          5.5148
v  Velocity[Z]                  -43754           95458          67.787          39.599
v  ǁVelocityǁ                   2.4661      2.9831e+05          674.46          434.76
v  Pressure                 -1.558e+07      2.7709e+07      4.2064e+06      2.9834e+06
v  turbulent_viscosity         0.52809           46199          60.585          35.631
v  CourantNb                    225.39      5.5282e+08      3.0395e+05      1.4698e+05
v  FourierNb                    161.34      3.7473e+08      1.1225e+05           41578
v  total_pressure           -1.508e+07      2.8209e+07      4.7064e+06      3.4834e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          521.96      7.6948e+08       4.162e+05      1.8856e+05


 TIME FOR THE TIME STEP              170:        0.90236E+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        -0.334257327E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275336812E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.27744E+00 0.35068E+06
   Friction velocity        uet   :  0.94102E-01 0.11996E+05
   Friction velocity        uk    :  0.94102E-01 0.11996E+05
   Dimensionless distance   yplus :  0.17407E+01 0.10848E+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    0.64003E+08    5380   0.94617E+00   0.55152E+07 
c  VelocityY    0.64003E+08    5380   0.94617E+00   0.00000E+00 
c  VelocityZ    0.64003E+08    5380   0.94617E+00   0.00000E+00 
c  Pressure     0.10625E+04     679   0.13414E-01   0.16945E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -74788           29788         -99.565         -31.786
v  Velocity[Y]             -1.5517e+05      3.2699e+05         -29.472         -7.1464
v  Velocity[Z]                  -35327      1.1512e+05          96.508          37.207
v  ǁVelocityǁ                   6.4588      3.2898e+05          1240.5          854.17
v  Pressure                -1.6094e+07      3.1321e+07      4.9547e+06      3.5142e+06
v  turbulent_viscosity         0.31936           50188          47.474          26.008
v  CourantNb                    52.361      6.1406e+08      2.4272e+05      1.0756e+05
v  FourierNb                     122.7      4.3043e+08           94379           32045
v  total_pressure          -1.5594e+07      3.1821e+07      5.4547e+06      4.0142e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          549.48      8.5244e+08      3.3709e+05       1.396e+05


 TIME FOR THE TIME STEP              171:        0.93839E+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        -0.105829950E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275790674E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.12891E+01 0.38630E+06
   Friction velocity        uet   :  0.21769E+00 0.13118E+05
   Friction velocity        uk    :  0.21769E+00 0.13118E+05
   Dimensionless distance   yplus :  0.47703E+01 0.11864E+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    0.74413E+08    5510   0.94184E+00   0.50834E+07 
c  VelocityY    0.74413E+08    5510   0.94184E+00   0.00000E+00 
c  VelocityZ    0.74413E+08    5510   0.94184E+00   0.00000E+00 
c  Pressure     0.11517E+04     485   0.71645E-02   0.16892E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -79755           39129           -71.3         -43.464
v  Velocity[Y]             -1.7262e+05      3.5643e+05           39.96           4.762
v  Velocity[Z]                  -51183      1.1605e+05          23.727          48.959
v  ǁVelocityǁ                   2.5967      3.5774e+05          780.51          518.87
v  Pressure                -1.8546e+07      3.3407e+07      5.0488e+06      3.5816e+06
v  turbulent_viscosity          0.5658           54743          73.678          43.286
v  CourantNb                    370.41      6.6342e+08      3.7006e+05      1.7815e+05
v  FourierNb                    251.04      4.8201e+08      1.3789e+05           50426
v  total_pressure          -1.8046e+07      3.3907e+07      5.5488e+06      4.0816e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1329.7      9.2487e+08      5.0794e+05      2.2858e+05


 TIME FOR THE TIME STEP              172:        0.94709E+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         0.137754689E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.276211776E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.16794E+01 0.42112E+06
   Friction velocity        uet   :  0.32124E+00 0.14209E+05
   Friction velocity        uk    :  0.32124E+00 0.14209E+05
   Dimensionless distance   yplus :  0.45348E+01 0.12850E+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    0.93769E+08    6398   0.94619E+00   0.74334E+07 
c  VelocityY    0.93769E+08    6398   0.94619E+00   0.00000E+00 
c  VelocityZ    0.93769E+08    6398   0.94619E+00   0.00000E+00 
c  Pressure     0.12537E+04     660   0.11172E-01   0.16844E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -91054           34258         -159.61         -39.074
v  Velocity[Y]             -1.8715e+05       3.924e+05          301.31         -11.147
v  Velocity[Z]                  -46004      1.3511e+05          87.498          51.088
v  ǁVelocityǁ                   2.7905      3.9526e+05          1528.7          999.11
v  Pressure                -1.9714e+07      3.7201e+07      5.7206e+06      4.0563e+06
v  turbulent_viscosity         0.32135           60138          55.551          30.267
v  CourantNb                    239.34       7.365e+08      2.8077e+05      1.2582e+05
v  FourierNb                    159.73      4.7488e+08      1.1027e+05           37455
v  total_pressure          -1.9214e+07      3.7701e+07      6.2206e+06      4.5563e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          690.66      1.0263e+09      3.9104e+05      1.6328e+05


 TIME FOR THE TIME STEP              173:        0.10984E+02

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


 INSTANT    0.174000000E+02   TIME STEP NUMBER             174
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.505065553E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275590820E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.17666E+01 0.46447E+06
   Friction velocity        uet   :  0.31858E+00 0.15558E+05
   Friction velocity        uk    :  0.31858E+00 0.15558E+05
   Dimensionless distance   yplus :  0.51806E+01 0.14070E+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    0.10883E+09    5597   0.94334E+00   0.78124E+07 
c  VelocityY    0.10883E+09    5597   0.94334E+00   0.00000E+00 
c  VelocityZ    0.10883E+09    5597   0.94334E+00   0.00000E+00 
c  Pressure     0.13740E+04     475   0.71171E-02   0.16975E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -97562           45616         -133.43         -49.371
v  Velocity[Y]             -2.0689e+05      4.2757e+05          165.37          5.3633
v  Velocity[Z]                  -58156      1.3835e+05          94.294          59.132
v  ǁVelocityǁ                   5.7755      4.2916e+05           968.6          604.55
v  Pressure                -2.2769e+07      3.9586e+07      5.7649e+06      4.0966e+06
v  turbulent_viscosity         0.77823           66740          81.967          47.246
v  CourantNb                    65.061        7.98e+08      4.5663e+05      2.1189e+05
v  FourierNb                    190.16      5.4316e+08      1.5533e+05           55865
v  total_pressure          -2.2269e+07      4.0086e+07      6.2649e+06      4.5966e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1556.2       1.122e+09      6.1196e+05      2.6776e+05


 TIME FOR THE TIME STEP              174:        0.83076E+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        -0.416368871E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.270905462E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.22726E+01 0.50576E+06
   Friction velocity        uet   :  0.39188E+00 0.16836E+05
   Friction velocity        uk    :  0.39188E+00 0.16836E+05
   Dimensionless distance   yplus :  0.57644E+01 0.15225E+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         37 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.13497E+09    5096   0.94549E+00   0.18350E+08 
c  VelocityY    0.13497E+09    5096   0.94549E+00   0.00000E+00 
c  VelocityZ    0.13497E+09    5096   0.94549E+00   0.00000E+00 
c  Pressure     0.15316E+04     667   0.12135E-01   0.17342E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0356e+05           43790         -137.13         -47.671
v  Velocity[Y]             -2.2478e+05      4.7023e+05          199.21         -11.632
v  Velocity[Z]                  -45207      1.6931e+05          238.16           61.27
v  ǁVelocityǁ                   10.172      4.7441e+05          2086.6            1431
v  Pressure                -2.3571e+07      4.4773e+07      6.6371e+06       4.706e+06
v  turbulent_viscosity         0.39892           72219          68.353          36.714
v  CourantNb                    97.955      8.8469e+08      3.4528e+05      1.4922e+05
v  FourierNb                    182.12      5.7008e+08      1.3681e+05           45878
v  total_pressure          -2.3071e+07      4.5273e+07      7.1371e+06       5.206e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          908.57      1.2327e+09      4.8209e+05       1.951e+05


 TIME FOR THE TIME STEP              175:        0.91850E+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        -0.152849846E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.275936038E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.14231E+01 0.55722E+06
   Friction velocity        uet   :  0.37378E+00 0.18418E+05
   Friction velocity        uk    :  0.37378E+00 0.18418E+05
   Dimensionless distance   yplus :  0.24969E+01 0.16656E+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    0.15420E+09    5892   0.93981E+00   0.20023E+08 
c  VelocityY    0.15420E+09    5892   0.93981E+00   0.00000E+00 
c  VelocityZ    0.15420E+09    5892   0.93981E+00   0.00000E+00 
c  Pressure     0.16427E+04     498   0.71961E-02   0.17089E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1177e+05           55128         -85.349         -56.336
v  Velocity[Y]             -2.4866e+05      5.1409e+05          86.603          4.1574
v  Velocity[Z]                  -72013      1.6804e+05          10.469          72.601
v  ǁVelocityǁ                   4.9317       5.163e+05          1172.3          830.05
v  Pressure                -2.7358e+07      4.7542e+07      6.5966e+06      4.6836e+06
v  turbulent_viscosity         0.65998           79747          103.94          62.104
v  CourantNb                     510.1      9.5286e+08       5.958e+05      2.9088e+05
v  FourierNb                    330.26      6.4764e+08      1.9337e+05           71532
v  total_pressure          -2.6858e+07      4.8042e+07      7.0966e+06      5.1836e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          987.83      1.3281e+09      7.8917e+05      3.6241e+05


 TIME FOR THE TIME STEP              176:        0.10335E+02

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


 INSTANT    0.177000000E+02   TIME STEP NUMBER             177
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.203812173E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.269224228E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.31242E+01 0.60898E+06
   Friction velocity        uet   :  0.49518E+00 0.19999E+05
   Friction velocity        uk    :  0.49518E+00 0.19999E+05
   Dimensionless distance   yplus :  0.71411E+01 0.18086E+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    0.19397E+09    6834   0.94751E+00   0.19243E+08 
c  VelocityY    0.19397E+09    6834   0.94751E+00   0.00000E+00 
c  VelocityZ    0.19397E+09    6834   0.94751E+00   0.00000E+00 
c  Pressure     0.17688E+04     584   0.86667E-02   0.16879E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.2891e+05           52174         -256.88         -51.674
v  Velocity[Y]             -2.6941e+05       5.664e+05          120.38          4.0362
v  Velocity[Z]                  -59626      1.9995e+05          358.91           69.96
v  ǁVelocityǁ                   2.0481      5.7102e+05          1844.5          1205.3
v  Pressure                -3.0162e+07      5.1939e+07      6.9288e+06      4.9065e+06
v  turbulent_viscosity         0.41904           86918          76.798          42.606
v  CourantNb                    186.97      1.0649e+09      4.1121e+05      1.8966e+05
v  FourierNb                    174.05      6.8666e+08      1.5425e+05           52009
v  total_pressure          -2.9662e+07      5.2439e+07      7.4288e+06      5.4065e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1903.6      1.4726e+09      5.6546e+05      2.4167e+05


 TIME FOR THE TIME STEP              177:        0.99510E+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         0.451823502E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.277826011E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.59541E+00 0.67191E+06
   Friction velocity        uet   :  0.23489E+00 0.21909E+05
   Friction velocity        uk    :  0.23489E+00 0.21909E+05
   Dimensionless distance   yplus :  0.14632E+01 0.19813E+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    0.22532E+09    5753   0.94247E+00   0.17315E+08 
c  VelocityY    0.22532E+09    5753   0.94247E+00   0.00000E+00 
c  VelocityZ    0.22532E+09    5753   0.94247E+00   0.00000E+00 
c  Pressure     0.19632E+04     474   0.81247E-02   0.17170E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.3926e+05           65977         -6.7169         -72.304
v  Velocity[Y]             -2.9797e+05      6.1743e+05          130.18           11.63
v  Velocity[Z]                  -89144      1.9904e+05          49.846          102.73
v  ǁVelocityǁ                   8.6476      6.1979e+05          1352.3          983.91
v  Pressure                -3.4742e+07      5.5226e+07       6.892e+06      4.9011e+06
v  turbulent_viscosity         0.56992           95823          101.31          56.692
v  CourantNb                     30.69      1.1434e+09      5.7079e+05       2.629e+05
v  FourierNb                    161.37      8.4333e+08      1.9767e+05           68715
v  total_pressure          -3.4242e+07      5.5726e+07       7.392e+06      5.4011e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1369.8      1.5971e+09      7.6846e+05      3.3161e+05


 TIME FOR THE TIME STEP              178:        0.84052E+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         0.176985000E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.269724637E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.68169E+01 0.73247E+06
   Friction velocity        uet   :  0.74615E+00 0.23736E+05
   Friction velocity        uk    :  0.74615E+00 0.23736E+05
   Dimensionless distance   yplus :  0.10381E+02 0.21466E+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         24 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.28107E+09    6118   0.94526E+00   0.36940E+08 
c  VelocityY    0.28107E+09    6118   0.94526E+00   0.00000E+00 
c  VelocityZ    0.28107E+09    6118   0.94526E+00   0.00000E+00 
c  Pressure     0.21735E+04     641   0.12098E-01   0.17365E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.5008e+05           62578          -265.3         -64.225
v  Velocity[Y]             -3.2496e+05      6.7711e+05          293.81         -7.9794
v  Velocity[Z]                  -74509      2.3891e+05          400.34          94.166
v  ǁVelocityǁ                   8.2047      6.8246e+05          2839.9          1949.4
v  Pressure                -3.6817e+07      6.1777e+07      7.7557e+06      5.5003e+06
v  turbulent_viscosity         0.80081      1.0433e+05          92.558          51.082
v  CourantNb                    906.71      1.2744e+09      4.7649e+05      2.1994e+05
v  FourierNb                    357.21      8.9138e+08      1.8738e+05           62443
v  total_pressure          -3.6317e+07      6.2277e+07      8.2557e+06      6.0003e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2695.1      1.7742e+09      6.6387e+05      2.8238e+05


 TIME FOR THE TIME STEP              179:        0.96064E+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        -0.101640918E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.277832281E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.21106E+01 0.80486E+06
   Friction velocity        uet   :  0.36239E+00 0.25907E+05
   Friction velocity        uk    :  0.36239E+00 0.25907E+05
   Dimensionless distance   yplus :  0.58249E+01 0.23429E+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         37 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.32079E+09    6071   0.93984E+00   0.36439E+08 
c  VelocityY    0.32079E+09    6071   0.93984E+00   0.00000E+00 
c  VelocityZ    0.32079E+09    6071   0.93984E+00   0.00000E+00 
c  Pressure     0.23366E+04     446   0.68833E-02   0.17132E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6167e+05           78681         -133.92          -81.55
v  Velocity[Y]               -3.59e+05      7.3787e+05           137.9          2.3238
v  Velocity[Z]             -1.0793e+05      2.4178e+05          212.84          110.91
v  ǁVelocityǁ                   6.3429      7.4103e+05          1384.5          952.31
v  Pressure                -4.1915e+07      6.6085e+07      7.8605e+06      5.5897e+06
v  turbulent_viscosity          1.0895      1.1539e+05          140.41          85.075
v  CourantNb                    181.24      1.3812e+09      8.1636e+05      3.9434e+05
v  FourierNb                    315.75      9.3503e+08      2.6271e+05           96967
v  total_pressure          -4.1415e+07      6.6585e+07      8.3605e+06      6.0897e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          966.53      1.9393e+09      1.0791e+06       4.913e+05


 TIME FOR THE TIME STEP              180:        0.90033E+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        -0.198406721E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.277777065E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.14008E+01 0.87655E+06
   Friction velocity        uet   :  0.28922E+00 0.28044E+05
   Friction velocity        uk    :  0.28922E+00 0.28044E+05
   Dimensionless distance   yplus :  0.38582E+01 0.25362E+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    0.39297E+09    6467   0.94646E+00   0.32795E+08 
c  VelocityY    0.39297E+09    6467   0.94646E+00   0.00000E+00 
c  VelocityZ    0.39297E+09    6467   0.94646E+00   0.00000E+00 
c  Pressure     0.25373E+04     642   0.10218E-01   0.17035E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8491e+05           77508         -311.71         -77.433
v  Velocity[Y]             -3.8968e+05       8.153e+05          83.848         -16.451
v  Velocity[Z]                  -88013      2.8982e+05          453.88          114.55
v  ǁVelocityǁ                   12.489       8.204e+05            2546          1743.8
v  Pressure                 -4.524e+07      7.3128e+07      8.8422e+06      6.2957e+06
v  turbulent_viscosity          1.0213      1.2494e+05          102.51          55.963
v  CourantNb                    285.18      1.5373e+09      5.2088e+05      2.2849e+05
v  FourierNb                    414.81      1.0682e+09      2.1108e+05           69062
v  total_pressure           -4.474e+07      7.3628e+07      9.3422e+06      6.7957e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          743.96      2.1242e+09      7.3197e+05      2.9755e+05


 TIME FOR THE TIME STEP              181:        0.93684E+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        -0.414054641E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.278981091E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.43584E+01 0.97007E+06
   Friction velocity        uet   :  0.59390E+00 0.30815E+05
   Friction velocity        uk    :  0.59390E+00 0.30815E+05
   Dimensionless distance   yplus :  0.87563E+01 0.27868E+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    0.46160E+09    5560   0.94280E+00   0.32725E+08 
c  VelocityY    0.46160E+09    5560   0.94280E+00   0.00000E+00 
c  VelocityZ    0.46160E+09    5560   0.94280E+00   0.00000E+00 
c  Pressure     0.28014E+04     422   0.79334E-02   0.17250E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.0027e+05           95886         -72.503         -108.99
v  Velocity[Y]             -4.2987e+05      8.8846e+05          281.99          9.0823
v  Velocity[Z]             -1.1936e+05      2.8919e+05          213.58          157.45
v  ǁVelocityǁ                   9.6822      8.9176e+05          2008.7          1461.5
v  Pressure                -5.1792e+07      7.7911e+07      8.8229e+06      6.3037e+06
v  turbulent_viscosity          1.2797      1.3666e+05          145.59          82.582
v  CourantNb                     223.3      1.6531e+09      7.8404e+05      3.6848e+05
v  FourierNb                    521.86      1.2064e+09      2.8487e+05           98909
v  total_pressure          -5.1292e+07      7.8411e+07      9.3229e+06      6.8037e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            1916      2.3074e+09      1.0689e+06      4.6739e+05


 TIME FOR THE TIME STEP              182:        0.82092E+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        -0.230001294E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.266484060E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.10830E+01 0.10567E+07
   Friction velocity        uet   :  0.28219E+00 0.33367E+05
   Friction velocity        uk    :  0.28219E+00 0.33367E+05
   Dimensionless distance   yplus :  0.25291E+01 0.30176E+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         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.58142E+09    5738   0.94534E+00   0.63801E+08 
c  VelocityY    0.58142E+09    5738   0.94534E+00   0.00000E+00 
c  VelocityZ    0.58142E+09    5738   0.94534E+00   0.00000E+00 
c  Pressure     0.30811E+04     642   0.11275E-01   0.17347E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.1332e+05           92188         -329.87          -94.56
v  Velocity[Y]             -4.6871e+05      9.7575e+05          244.97          -15.09
v  Velocity[Z]             -1.0314e+05      3.4459e+05          602.78          144.54
v  ǁVelocityǁ                   15.607      9.8331e+05            3528          2454.6
v  Pressure                -5.4774e+07      8.7404e+07      1.0021e+07      7.1365e+06
v  turbulent_viscosity          2.3477      1.5001e+05          128.68          73.463
v  CourantNb                    531.87       1.842e+09      6.9514e+05      3.1962e+05
v  FourierNb                    661.94      1.1835e+09      2.6007e+05           87401
v  total_pressure          -5.4274e+07      8.7904e+07      1.0521e+07      7.6365e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            2892      2.5674e+09      9.5521e+05      4.0702e+05


 TIME FOR THE TIME STEP              183:        0.10232E+02

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


 INSTANT    0.184000000E+02   TIME STEP NUMBER             184
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.424368331E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.279876263E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.14862E+01 0.11629E+07
   Friction velocity        uet   :  0.29797E+00 0.36474E+05
   Friction velocity        uk    :  0.29797E+00 0.36474E+05
   Dimensionless distance   yplus :  0.40992E+01 0.32985E+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    0.66512E+09    5849   0.93974E+00   0.70308E+08 
c  VelocityY    0.66512E+09    5849   0.93974E+00   0.00000E+00 
c  VelocityZ    0.66512E+09    5849   0.93974E+00   0.00000E+00 
c  Pressure     0.33366E+04     481   0.73843E-02   0.17214E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.3265e+05      1.1459e+05         -205.49         -120.19
v  Velocity[Y]             -5.1746e+05      1.0626e+06           26.09          1.7826
v  Velocity[Z]             -1.5527e+05      3.4699e+05          214.48          176.18
v  ǁVelocityǁ                   8.2179      1.0669e+06          2040.8          1418.6
v  Pressure                -6.2432e+07      9.3302e+07       1.015e+07      7.2619e+06
v  turbulent_viscosity          1.4054      1.6607e+05          188.89          113.09
v  CourantNb                    911.89      1.9924e+09      1.0392e+06      5.0035e+05
v  FourierNb                     509.7      1.3462e+09      3.5829e+05      1.3007e+05
v  total_pressure          -6.1932e+07      9.3802e+07       1.065e+07      7.7619e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3275.8      2.8019e+09      1.3975e+06      6.3041e+05


 TIME FOR THE TIME STEP              184:        0.88043E+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        -0.244164931E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.266779848E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.43566E+01 0.12658E+07
   Friction velocity        uet   :  0.58003E+00 0.39470E+05
   Friction velocity        uk    :  0.58003E+00 0.39470E+05
   Dimensionless distance   yplus :  0.81190E+01 0.35695E+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         29 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.83154E+09    6642   0.94710E+00   0.71598E+08 
c  VelocityY    0.83154E+09    6642   0.94710E+00   0.00000E+00 
c  VelocityZ    0.83154E+09    6642   0.94710E+00   0.00000E+00 
c  Pressure     0.36214E+04     624   0.92150E-02   0.17112E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6922e+05      1.0828e+05         -404.51         -106.86
v  Velocity[Y]             -5.6018e+05      1.1744e+06          562.61          -28.77
v  Velocity[Z]             -1.3089e+05      4.1051e+05          293.11          179.74
v  ǁVelocityǁ                   9.8852      1.1837e+06          3545.7            2329
v  Pressure                -6.7745e+07      1.0292e+08      1.1214e+07      8.0026e+06
v  turbulent_viscosity          1.1993      1.8008e+05          146.87          80.756
v  CourantNb                    242.28      2.2182e+09      7.5295e+05       3.324e+05
v  FourierNb                    828.71      1.4215e+09      3.0105e+05           98890
v  total_pressure          -6.7245e+07      1.0342e+08      1.1714e+07      8.5026e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1380.8      3.0604e+09       1.054e+06      4.3129e+05


 TIME FOR THE TIME STEP              185:        0.10801E+02

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


 INSTANT    0.186000000E+02   TIME STEP NUMBER             186
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.912043878E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.279715450E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.24993E+01 0.14008E+07
   Friction velocity        uet   :  0.40478E+00 0.43376E+05
   Friction velocity        uk    :  0.40478E+00 0.43376E+05
   Dimensionless distance   yplus :  0.67486E+01 0.39227E+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         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.97181E+09    6028   0.94243E+00   0.74315E+08 
c  VelocityY    0.97181E+09    6028   0.94243E+00   0.00000E+00 
c  VelocityZ    0.97181E+09    6028   0.94243E+00   0.00000E+00 
c  Pressure     0.39944E+04     494   0.76182E-02   0.17296E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.9039e+05      1.3536e+05         -223.29         -129.14
v  Velocity[Y]             -6.2035e+05       1.281e+06          312.93           8.641
v  Velocity[Z]             -1.8563e+05      4.1444e+05          353.09          202.58
v  ǁVelocityǁ                   17.376       1.286e+06          2937.9          1965.1
v  Pressure                -7.6897e+07       1.101e+08      1.1408e+07       8.225e+06
v  turbulent_viscosity          1.0433      1.9943e+05          199.08           112.6
v  CourantNb                    102.46      2.3856e+09      1.1059e+06      4.9883e+05
v  FourierNb                    355.47      1.6217e+09      3.9347e+05      1.3515e+05
v  total_pressure          -7.6397e+07       1.106e+08      1.1908e+07       8.725e+06


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1471.3      3.3676e+09      1.4994e+06      6.3397e+05


 TIME FOR THE TIME STEP              186:        0.88789E+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         0.221533620E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.265069430E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.92948E+01 0.15276E+07
   Friction velocity        uet   :  0.11174E+01 0.47023E+05
   Friction velocity        uk    :  0.11174E+01 0.47023E+05
   Dimensionless distance   yplus :  0.16605E+02 0.42525E+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         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.12118E+10    6024   0.94536E+00   0.13197E+09 
c  VelocityY    0.12118E+10    6024   0.94536E+00   0.00000E+00 
c  VelocityZ    0.12118E+10    6024   0.94536E+00   0.00000E+00 
c  Pressure     0.44479E+04     656   0.12681E-01   0.17579E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.1569e+05        1.27e+05         -683.84         -133.98
v  Velocity[Y]             -6.7478e+05      1.4038e+06         -155.33         -56.901
v  Velocity[Z]             -1.5405e+05      4.9836e+05          774.39          203.77
v  ǁVelocityǁ                   10.872      1.4153e+06          5354.6          3800.7
v  Pressure                -8.0141e+07      1.2475e+08      1.3629e+07      9.7348e+06
v  turbulent_viscosity          1.9219      2.1689e+05          186.52          102.67
v  CourantNb                    379.32      2.6496e+09      1.0146e+06      4.4681e+05
v  FourierNb                      1252      1.7095e+09      3.8007e+05      1.2535e+05
v  total_pressure          -7.9641e+07      1.2525e+08      1.4129e+07      1.0235e+07


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4743.6      3.6935e+09      1.3947e+06      5.7215e+05


 TIME FOR THE TIME STEP              187:        0.92196E+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        -0.592040523E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.280578687E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.71655E+01 0.16772E+07
   Friction velocity        uet   :  0.79121E+00 0.51299E+05
   Friction velocity        uk    :  0.79121E+00 0.51299E+05
   Dimensionless distance   yplus :  0.13387E+02 0.46393E+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         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.13797E+10    6019   0.93974E+00   0.12901E+09 
c  VelocityY    0.13797E+10    6019   0.93974E+00   0.00000E+00 
c  VelocityZ    0.13797E+10    6019   0.93974E+00   0.00000E+00 
c  Pressure     0.47880E+04     474   0.72855E-02   0.17341E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.3903e+05      1.6191e+05         -294.82         -152.88
v  Velocity[Y]              -7.458e+05      1.5309e+06          83.874         -11.101
v  Velocity[Z]             -2.0776e+05      5.0074e+05          323.93          252.63
v  ǁVelocityǁ                   27.002      1.5374e+06            2419          1769.6
v  Pressure                 -9.071e+07      1.3369e+08      1.4145e+07      1.0222e+07
v  turbulent_viscosity          1.3011      2.3944e+05          284.48          169.05
v  CourantNb                    361.01      2.8684e+09       1.549e+06      7.5297e+05
v  FourierNb                    668.07       1.939e+09      5.4013e+05      1.9503e+05
v  total_pressure           -9.021e+07      1.3419e+08      1.4645e+07      1.0722e+07


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4053.9      3.9879e+09      2.0891e+06        9.48e+05


 TIME FOR THE TIME STEP              188:        0.10382E+02

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


 INSTANT    0.189000000E+02   TIME STEP NUMBER             189
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590         0.103718466E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.271991859E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.12240E+02 0.18281E+07
   Friction velocity        uet   :  0.14325E+01 0.55589E+05
   Friction velocity        uk    :  0.14325E+01 0.55589E+05
   Dimensionless distance   yplus :  0.15718E+02 0.50272E+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    0.17275E+10    5511   0.94703E+00   0.11204E+09 
c  VelocityY    0.17275E+10    5511   0.94703E+00   0.00000E+00 
c  VelocityZ    0.17275E+10    5511   0.94703E+00   0.00000E+00 
c  Pressure     0.52165E+04     663   0.10775E-01   0.17295E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.7972e+05      1.6499e+05         -277.48         -159.14
v  Velocity[Y]              -8.077e+05      1.6938e+06          64.346          -82.57
v  Velocity[Z]              -1.827e+05      5.9266e+05           622.2          260.26
v  ǁVelocityǁ                   31.135      1.7068e+06          5435.9          3834.2
v  Pressure                -9.5915e+07      1.5004e+08      1.7103e+07      1.2298e+07
v  turbulent_viscosity          2.3707      2.5978e+05          193.61          106.71
v  CourantNb                    774.82      3.2011e+09      9.5715e+05      4.1954e+05
v  FourierNb                    911.08      2.2195e+09      4.0761e+05      1.3071e+05
v  total_pressure          -9.5415e+07      1.5054e+08      1.7603e+07      1.2798e+07


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          5507.4      4.4216e+09      1.3648e+06      5.5025e+05


 TIME FOR THE TIME STEP              189:        0.83293E+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        -0.630665442E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.284461214E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.60944E+01 0.20254E+07
   Friction velocity        uet   :  0.76045E+00 0.61165E+05
   Friction velocity        uk    :  0.76045E+00 0.61165E+05
   Dimensionless distance   yplus :  0.14613E+02 0.55315E+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    0.19893E+10    6503   0.94093E+00   0.15710E+09 
c  VelocityY    0.19893E+10    6503   0.94093E+00   0.00000E+00 
c  VelocityZ    0.19893E+10    6503   0.94093E+00   0.00000E+00 
c  Pressure     0.57209E+04     371   0.72477E-02   0.17406E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.0757e+05      1.9618e+05         -643.54         -170.17
v  Velocity[Y]             -8.9205e+05      1.8426e+06          307.89         -38.354
v  Velocity[Z]             -2.6401e+05      5.9921e+05          148.33          300.32
v  ǁVelocityǁ                   9.9783      1.8502e+06          3450.8            2415
v  Pressure                -1.0987e+08      1.5957e+08      1.7117e+07      1.2281e+07
v  turbulent_viscosity          3.6326      2.8765e+05          302.72          173.82
v  CourantNb                    185.44        3.45e+09      1.6474e+06      7.8005e+05
v  FourierNb                    1427.7      2.3401e+09      5.9311e+05      2.0556e+05
v  total_pressure          -1.0937e+08      1.6007e+08      1.7617e+07      1.2781e+07


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4216.6      4.8189e+09      2.2405e+06      9.8561e+05


 TIME FOR THE TIME STEP              190:        0.95177E+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        -0.491345842E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.271144814E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.29704E+01 0.22021E+07
   Friction velocity        uet   :  0.43106E+00 0.66132E+05
   Friction velocity        uk    :  0.43106E+00 0.66132E+05
   Dimensionless distance   yplus :  0.76262E+01 0.59806E+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         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.24463E+10    7122   0.94369E+00   0.18282E+09 
c  VelocityY    0.24463E+10    7122   0.94369E+00   0.00000E+00 
c  VelocityZ    0.24463E+10    7122   0.94369E+00   0.00000E+00 
c  Pressure     0.62405E+04     660   0.10385E-01   0.17374E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.7006e+05      1.7938e+05         -520.94         -155.03
v  Velocity[Y]             -9.7723e+05      2.0179e+06         -365.61         -82.982
v  Velocity[Z]             -2.2515e+05       7.141e+05          821.06           286.7
v  ǁVelocityǁ                   6.1301      2.0307e+06          5814.5          3657.3
v  Pressure                -1.1679e+08      1.7827e+08       2.041e+07      1.4629e+07
v  turbulent_viscosity           1.443      3.1152e+05          236.59          127.64
v  CourantNb                    1.0254      3.8412e+09      1.2696e+06      5.5888e+05
v  FourierNb                    527.33      2.4587e+09      4.9722e+05       1.586e+05
v  total_pressure          -1.1629e+08      1.7877e+08       2.091e+07      1.5129e+07


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2559.1      5.3061e+09      1.7668e+06      7.1747e+05


 TIME FOR THE TIME STEP              191:        0.10437E+02

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


 INSTANT    0.192000000E+02   TIME STEP NUMBER             192
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.705966318E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.284654352E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.42734E+01 0.24177E+07
   Friction velocity        uet   :  0.70989E+00 0.72156E+05
   Friction velocity        uk    :  0.70989E+00 0.72156E+05
   Dimensionless distance   yplus :  0.63238E+01 0.65254E+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         37 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.28599E+10    5703   0.94132E+00   0.14926E+09 
c  VelocityY    0.28599E+10    5703   0.94132E+00   0.00000E+00 
c  VelocityZ    0.28599E+10    5703   0.94132E+00   0.00000E+00 
c  Pressure     0.68486E+04     399   0.77903E-02   0.17461E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9985e+05      2.3715e+05         -438.68         -197.44
v  Velocity[Y]             -1.0793e+06      2.2078e+06          95.261         -53.174
v  Velocity[Z]             -3.2221e+05      7.2202e+05          275.11          365.02
v  ǁVelocityǁ                   21.419      2.2162e+06          4235.1          2809.8
v  Pressure                -1.3335e+08      1.8991e+08      2.0449e+07      1.4669e+07
v  turbulent_viscosity          3.4159      3.4013e+05          361.58          196.28
v  CourantNb                    146.55      4.1458e+09      1.8372e+06      7.9929e+05
v  FourierNb                    1529.7      2.7661e+09      7.1529e+05      2.4257e+05
v  total_pressure          -1.3285e+08      1.9041e+08      2.0949e+07      1.5169e+07


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4081.8      5.7862e+09      2.5525e+06      1.0419e+06


 TIME FOR THE TIME STEP              192:        0.84578E+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        -0.314545265E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.272997386E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.58537E+01 0.26439E+07
   Friction velocity        uet   :  0.74882E+00 0.78442E+05
   Friction velocity        uk    :  0.74882E+00 0.78442E+05
   Dimensionless distance   yplus :  0.13454E+02 0.70940E+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         32 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.36146E+10    6255   0.94672E+00   0.16789E+09 
c  VelocityY    0.36146E+10    6255   0.94672E+00   0.00000E+00 
c  VelocityZ    0.36146E+10    6255   0.94672E+00   0.00000E+00 
c  Pressure     0.74471E+04     659   0.97134E-02   0.17360E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6942e+05      2.1612e+05         -372.71         -217.48
v  Velocity[Y]             -1.1584e+06      2.4312e+06           812.5         -112.93
v  Velocity[Z]             -2.9475e+05      8.3303e+05          249.16           375.6
v  ǁVelocityǁ                    18.92      2.4487e+06          6668.2          4601.8
v  Pressure                -1.4324e+08      2.1076e+08      2.3895e+07      1.7202e+07
v  turbulent_viscosity          1.9773       3.754e+05          301.15          161.94
v  CourantNb                    493.59      4.6028e+09      1.5372e+06      6.5678e+05
v  FourierNb                    753.31      3.2027e+09      6.2835e+05      2.0169e+05
v  total_pressure          -1.4274e+08      2.1126e+08      2.4395e+07      1.7702e+07


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          2445.3      6.4086e+09      2.1655e+06      8.5847e+05


 TIME FOR THE TIME STEP              193:        0.11036E+02

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


 INSTANT    0.194000000E+02   TIME STEP NUMBER             194
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.219204212E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.286113377E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.20320E+02 0.29145E+07
   Friction velocity        uet   :  0.19254E+01 0.85917E+05
   Friction velocity        uk    :  0.19254E+01 0.85917E+05
   Dimensionless distance   yplus :  0.26880E+02 0.77699E+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    0.41803E+10    5965   0.94195E+00   0.20027E+09 
c  VelocityY    0.41803E+10    5965   0.94195E+00   0.00000E+00 
c  VelocityZ    0.41803E+10    5965   0.94195E+00   0.00000E+00 
c  Pressure     0.81958E+04     484   0.74451E-02   0.17517E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.0813e+05       2.826e+05         -871.12         -226.19
v  Velocity[Y]             -1.2897e+06      2.6541e+06          503.03         -38.386
v  Velocity[Z]             -3.8374e+05      8.6249e+05          988.09          419.65
v  ǁVelocityǁ                   27.313      2.6647e+06          5690.4          3631.4
v  Pressure                -1.6393e+08       2.239e+08      2.3684e+07      1.7057e+07
v  turbulent_viscosity          2.5224      4.1401e+05          383.33          220.41
v  CourantNb                    3133.6      4.9952e+09      2.1106e+06      9.6274e+05
v  FourierNb                    757.31      3.3627e+09      7.6318e+05      2.6082e+05
v  total_pressure          -1.6343e+08       2.244e+08      2.4184e+07      1.7557e+07


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          8861.7      6.9472e+09      2.8737e+06      1.2236e+06


 TIME FOR THE TIME STEP              194:        0.85713E+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         0.112611071E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.253149710E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.14323E+02 0.31804E+07
   Friction velocity        uet   :  0.16636E+01 0.93223E+05
   Friction velocity        uk    :  0.16636E+01 0.93223E+05
   Dimensionless distance   yplus :  0.18764E+02 0.84307E+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    0.51167E+10    4850   0.94408E+00   0.44066E+09 
c  VelocityY    0.51167E+10    4850   0.94408E+00   0.00000E+00 
c  VelocityZ    0.51167E+10    4850   0.94408E+00   0.00000E+00 
c  Pressure     0.90910E+04     697   0.13780E-01   0.17735E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.5359e+05      2.8049e+05         -437.72         -261.83
v  Velocity[Y]             -1.3962e+06      2.9132e+06          -9.749         -177.04
v  Velocity[Z]             -3.0401e+05       1.047e+06          600.66          468.37
v  ǁVelocityǁ                   118.72      2.9322e+06           12167          8388.6
v  Pressure                -1.6615e+08      2.5878e+08      3.2326e+07      2.3237e+07
v  turbulent_viscosity          2.8777      4.4994e+05             366          196.15
v  CourantNb                    941.87      5.5258e+09      2.0001e+06      8.4243e+05
v  FourierNb                    1164.7      3.8393e+09      7.6517e+05      2.4465e+05
v  total_pressure          -1.6565e+08      2.5928e+08      3.2826e+07      2.3737e+07


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          6297.5      7.6904e+09      2.7653e+06      1.0871e+06


 TIME FOR THE TIME STEP              195:        0.74279E+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        -0.407105990E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.290971967E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.32234E+02 0.34980E+07
   Friction velocity        uet   :  0.31445E+01 0.10190E+06
   Friction velocity        uk    :  0.31445E+01 0.10190E+06
   Dimensionless distance   yplus :  0.37389E+02 0.92152E+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         36 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.58639E+10    6615   0.93871E+00   0.49013E+09 
c  VelocityY    0.58639E+10    6615   0.93871E+00   0.00000E+00 
c  VelocityZ    0.58639E+10    6615   0.93871E+00   0.00000E+00 
c  Pressure     0.98235E+04     459   0.70870E-02   0.17561E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0603e+05      3.4009e+05         -987.15          -279.3
v  Velocity[Y]             -1.5465e+06      3.1779e+06          33.836         -102.13
v  Velocity[Z]             -4.5673e+05        1.04e+06          246.75          571.13
v  ǁVelocityǁ                   15.077      3.1907e+06            5379          3711.4
v  Pressure                -1.8937e+08      2.7607e+08      3.2749e+07      2.3626e+07
v  turbulent_viscosity          7.8931      4.9045e+05          619.36          363.03
v  CourantNb                    653.08      5.9754e+09       3.451e+06      1.6339e+06
v  FourierNb                    3443.4      3.9903e+09      1.1787e+06       4.219e+05
v  total_pressure          -1.8887e+08      2.7657e+08      3.3249e+07      2.4126e+07


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           24272      8.3401e+09      4.6298e+06      2.0558e+06


 TIME FOR THE TIME STEP              196:        0.95713E+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        -0.144754499E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.289842811E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.85560E+01 0.38133E+07
   Friction velocity        uet   :  0.10595E+01 0.11047E+06
   Friction velocity        uk    :  0.10595E+01 0.11047E+06
   Dimensionless distance   yplus :  0.14994E+02 0.99901E+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         37 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.74243E+10    7722   0.94735E+00   0.42494E+09 
c  VelocityY    0.74243E+10    7722   0.94735E+00   0.00000E+00 
c  VelocityZ    0.74243E+10    7722   0.94735E+00   0.00000E+00 
c  Pressure     0.10646E+05     606   0.92124E-02   0.17408E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.1457e+05      3.1288e+05         -1267.3         -288.32
v  Velocity[Y]             -1.6828e+06      3.5001e+06         -177.53         -134.75
v  Velocity[Z]             -4.2498e+05      1.2141e+06          1259.9          536.19
v  ǁVelocityǁ                   7.6432      3.5258e+06          8690.7          5740.7
v  Pressure                -2.0635e+08      3.0359e+08      3.5214e+07      2.5278e+07
v  turbulent_viscosity          2.4344      5.3789e+05          393.71          216.51
v  CourantNb                    131.41       6.661e+09      2.0494e+06      8.6675e+05
v  FourierNb                      1065      4.5996e+09      8.3727e+05      2.6507e+05
v  total_pressure          -2.0585e+08      3.0409e+08      3.5714e+07      2.5778e+07


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          4673.1      9.2058e+09      2.8867e+06      1.1318e+06


 TIME FOR THE TIME STEP              197:        0.11248E+02

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


 INSTANT    0.198000000E+02   TIME STEP NUMBER             198
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          84        -0.273282681E+00
Smooth wall               5        6590        -0.145973945E-12
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.296735847E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.96128E+01 0.42058E+07
   Friction velocity        uet   :  0.11742E+01 0.12107E+06
   Friction velocity        uk    :  0.11742E+01 0.12107E+06
   Dimensionless distance   yplus :  0.91365E+01 0.10949E+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    0.86739E+10    5632   0.94198E+00   0.47092E+09 
c  VelocityY    0.86739E+10    5632   0.94198E+00   0.00000E+00 
c  VelocityZ    0.86739E+10    5632   0.94198E+00   0.00000E+00 
c  Pressure     0.11793E+05     519   0.82884E-02   0.17643E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7544e+05      4.0217e+05         -755.88         -343.51
v  Velocity[Y]             -1.8614e+06      3.8096e+06          474.84         -53.071
v  Velocity[Z]             -5.6127e+05      1.2403e+06          628.97          630.22
v  ǁVelocityǁ                   73.622      3.8242e+06            7643          5668.1
v  Pressure                -2.3704e+08      3.2152e+08      3.4637e+07      2.5107e+07
v  turbulent_viscosity          1.2668      5.9739e+05          533.84          291.85
v  CourantNb                    290.85      7.2087e+09       2.846e+06      1.2521e+06
v  FourierNb                     902.6      4.8514e+09      1.0853e+06      3.5815e+05
v  total_pressure          -2.3654e+08      3.2202e+08      3.5137e+07      2.5607e+07


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3200.6      1.0046e+10      3.9313e+06      1.6103e+06


 TIME FOR THE TIME STEP              198:        0.83845E+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        -0.105191203E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.242714084E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.28299E+02 0.45756E+07
   Friction velocity        uet   :  0.26296E+01 0.13101E+06
   Friction velocity        uk    :  0.26296E+01 0.13101E+06
   Dimensionless distance   yplus :  0.45769E+02 0.11848E+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         30 outlet faces on         82

   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.10568E+11    6413   0.94359E+00   0.13419E+10 
c  VelocityY    0.10568E+11    6413   0.94359E+00   0.00000E+00 
c  VelocityZ    0.10568E+11    6413   0.94359E+00   0.00000E+00 
c  Pressure     0.12881E+05     610   0.10555E-01   0.17594E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -9.5801e+05       3.832e+05         -707.32         -321.76
v  Velocity[Y]             -2.0186e+06       4.188e+06          645.42         -66.622
v  Velocity[Z]             -4.2934e+05      1.5238e+06          1509.5          652.33
v  ǁVelocityǁ                   52.096      4.2176e+06           13776          9317.4
v  Pressure                -2.5492e+08      3.5708e+08      3.7738e+07      2.7231e+07
v  turbulent_viscosity          9.1701      6.4657e+05          511.55          287.96
v  CourantNb                    15.872      7.9682e+09      2.6844e+06      1.2154e+06
v  FourierNb                    2704.7      5.0934e+09       1.062e+06      3.4566e+05
v  total_pressure          -2.5442e+08      3.5758e+08      3.8238e+07      2.7731e+07


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           17363      1.1224e+10      3.7464e+06       1.561e+06


 TIME FOR THE TIME STEP              199:        0.94532E+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        -0.131648425E-11
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          82         0.306437329E+00
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.90384E+01 0.50402E+07
   Friction velocity        uet   :  0.11456E+01 0.14342E+06
   Friction velocity        uk    :  0.11456E+01 0.14342E+06
   Dimensionless distance   yplus :  0.13868E+02 0.12971E+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


 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:    0.86856E-02



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.12128E+11    6121   0.93824E+00   0.14641E+10 
c  VelocityY    0.12128E+11    6121   0.93824E+00   0.00000E+00 
c  VelocityZ    0.12128E+11    6121   0.93824E+00   0.00000E+00 
c  Pressure     0.14104E+05     387   0.76704E-02   0.17612E+00 
---------------------------------------------------------------
  
  

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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0141e+06       4.926e+05         -607.81         -355.82
v  Velocity[Y]               -2.23e+06      4.5719e+06          510.13         -104.36
v  Velocity[Z]             -6.1004e+05      1.4966e+06          733.29          785.15
v  ǁVelocityǁ                   54.526      4.5905e+06          8647.7          6361.4
v  Pressure                -2.8939e+08      3.8104e+08      3.7778e+07      2.7441e+07
v  turbulent_viscosity          5.4028       7.054e+05          732.88          427.79
v  CourantNb                    1349.6      8.5941e+09      4.1044e+06      1.9005e+06
v  FourierNb                    2904.3      6.1989e+09      1.4407e+06      5.0092e+05
v  total_pressure          -2.8889e+08      3.8154e+08      3.8278e+07      2.7941e+07


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          5128.8      1.2004e+10      5.5451e+06      2.4014e+06


 TIME FOR THE TIME STEP              200:        0.91258E+01

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.10204E-03
      -----------------------                                



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




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


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

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:           1142.032 s
  System CPU time:            3.696 s
  Total CPU time:          4583.148 s

  Elapsed time:            1148.937 s
  CPU / elapsed time          0.997

Memory use summary:

  Total memory used:                             610.605 MiB
                             local minimum:      152.195 MiB  (rank 3)
                             local maximum:      153.457 MiB  (rank 1)
  Theoretical instrumented dynamic memory:       102.421 MiB
                             local minimum:       25.164 MiB  (rank 0)
                             local maximum:       26.022 MiB  (rank 1)
