command: 
 /usr/local/libexec/code_saturne/cs_solver --param s4_std_ke_3.xml --mpi

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

                                  (R)
                      Code_Saturne

                      Version 4.0.0


  Copyright (C) 1998-2015 EDF S.A., France

  revision 4.0.0
  build lun 04 mag 2015 16:44:11 CEST
  MPI version 2.1 (Open MPI 1.6.5)


  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:                ven 26 giu 2015 10:35:26 CEST
  System:              Linux 3.19.0-22-generic
  Machine:             celsius
  Processor:           model name	: Intel(R) Xeon(R) CPU E3-1225 v3 @ 3.20GHz
  Memory:              15934 MB
  User:                claudio (claudio)
  Directory:           /home/claudio/Documents/Atos/DP4/1L5/06_CFD/DP4_1L5_PA_mod_p40_test/S4_STD_KE/RESU/20150626-1035
  MPI ranks:           1
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)

 Reading metadata from file: "mesh_input"

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

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


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




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


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

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

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


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

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


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


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

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

       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         )
                               (1: temperature              )
                               (2: enthalpy                 )
                               (3: total energy             )
       ITPSCL =              0 (0: none                     )
                               (1: temperature in Kelvin    )
                               (2: temperature in Celsius   )
       ISCALT =             -1 (Thermal scalar number       )


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

 --- Continuous phase:

   - Commons
       ITURB  =             21 (Turbulence model            )
       IDEUCH =              1 (0: one-scale model          )
                               (1: two-scale model          )
                               (2: invariant wall function  )
       IWALLT =              0 (Exch. coeff. correlation    )
                               (0: not activated            )
                               (1: activated                )
       YPLULI =    0.23810E+01 (Limit Y+                    )
       ILOGPO =              1 (0: power law (forbidden for
                                              k-epsilon)    )
                               (1: one-scale log law        )
       IGRHOK =              0 (1: computed Grad(rho k)     )

   - Linear production k-epsilon (ITURB = 21)
       ALMAX  =    0.25000E-01 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       ICLKEP =              0 (k-epsilon clipping model    )
       IKECOU =              0 (k-epsilon coupling mode     )
       IGRAKE =              0 (Account for gravity         )
       RELAXV =    0.10000E+01 for k        (Relaxation)
       RELAXV =    0.10000E+01 for epsilon  (Relaxation)

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

 --- Constants

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

   - Linear production k-epsilon (ITURB = 21)
       Ce1    =    0.14400E+01 (Cepsilon 1: production coef.)
       CE2    =    0.19200E+01 (Cepsilon 2: dissipat.  coef.)
       SIGMAK =    0.10000E+01 (Prandtl relative to k       )
       SIGMAE =    0.13000E+01 (Prandtl relative to epsilon )
       CMU    =    0.90000E-01 (Cmu constant                )


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


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

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


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

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

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

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

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

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

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

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


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

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

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


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


 ** STOKES
    ------
       IDILAT =              1 (1 : without unsteady term
                                    in the continuity equation
                                2 : with unsteady term in 
                                    the continuity equation)
       IPOROS =              0 (0 : without porous media
                                1 : with porous media)
       IPHYDR =              0 (1: account for explicit
                                   balance between pressure
                                   gradient, gravity source
                                   terms, and head losses     )
       ICALHY =              0 (1: compute hydrastatic
                                   pressure for Dirichlet
                                   conditions for pressure
                                   on outlet                  )
       IPRCO  =              1 (1: pressure-continuity        )
       IPUCOU =              0 (1: reinforced U-P coupling    )
       NTERUP =              1 (n: n sweeps on navsto for
                                   velocity/pressure coupling )

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

       RELAXV =    0.46000E+00 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-03  0.0000E+00
 Pressure            100      2  0.1000E-04  0.1000E-03  0.0000E+00
 k                   100      1  0.1000E-04  0.1000E-03  0.0000E+00
 epsilon             100      1  0.1000E-04  0.1000E-03  0.0000E+00
-----------------------------------------------------------

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

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


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


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


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


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

------------------------------------
 Variable              EPSILO IDIRCL
------------------------------------
 Velocity          0.1000E-04      1
 Pressure          0.1000E-04      1
 k                 0.1000E-04      1
 epsilon           0.1000E-04      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    )


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


 ** 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 =            800 (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


Velocity
Pressure
k
epsilon
TurbVisc
CourantNb
FourierNb
total_pressure
Local Time Step
         --           --

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

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

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

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

         2 Velocity                       0
         5 Pressure                       0
         6 k                              0
         7 epsilon                        0
        10 TurbVisc                    -999
        11 CourantNb                   -999
        12 FourierNb                   -999
        13 total_pressure              -999
        14 Local Time Step             -999
         --           --                --

 --- Additional post-processing variables (ipstdv)
       ipstfo =              6 (Force exerted by the
                                     fluid on the boundary)
       ipstft =              1 (Thermal flux   at boundary)
       ipsttb =              0 (Temperature    at boundary)
       ipstnu =              0 (Dimensionless thermal
                                          flux at boundary)


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


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

       IALE   =              0 (1: activated                )
       NALINF =              0 (Fluid initialization
                                                  iterations)
       IFLXMW =              0 (ALE mass flux computation
                                0: thanks to vertices
                                1: thanks to mesh velocity)


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


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

  -1: name: results
      directory: postprocessing
      format: MED 3.0.6
      options: 
      time dependency: fixed mesh
      output: every 100 time steps and at calculation end


 Reading file:        mesh_input

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

  -1: name: results
      directory: postprocessing
      format: MED 3.0.6
      options: 
      time dependency: fixed mesh
      output: every 100 time steps and at calculation end


 Reading file:        mesh_input

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

  -1: name: results
      directory: postprocessing
      format: MED 3.0.6
      options: 
      time dependency: fixed mesh
      output: every 100 time steps and at calculation end


 Reading file:        mesh_input

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

  -1: name: results
      directory: postprocessing
      format: MED 3.0.6
      options: 
      time dependency: fixed mesh
      output: every 100 time steps and at calculation end


 Reading file:        mesh_input

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

  -1: name: results
      directory: postprocessing
      format: MED 3.0.6
      options: 
      time dependency: fixed mesh
      output: every 100 time steps and at calculation end


 Reading file:        mesh_input

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

  -1: name: results
      directory: postprocessing
      format: MED 3.0.6
      options: 
      time dependency: fixed mesh
      output: every 100 time steps and at calculation end


 Reading file:        mesh_input
 Finished reading:    mesh_input
 Finished reading:    mesh_input
 Finished reading:    mesh_input
 Finished reading:    mesh_input
 Finished reading:    mesh_input
 Finished reading:    mesh_input

 Extended neighborhood structures definition

 Extended neighborhood structures definition

 Extended neighborhood structures definition

 Extended neighborhood structures definition

 Extended neighborhood structures definition

 Extended neighborhood structures definition
 Number of cells:                                      281798

 ----------------------------------------------------------
 Number of cells + halo cells:                         281798


 ----------------------------------------------------------
 Number of interior faces:                             543050

 ----------------------------------------------------------
 Number of boundary faces:                             41092

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =        752
      2 : [          3 ;          4 ] =     281046

 ----------------------------------------------------------
 Number of cells:                                      281798

 ----------------------------------------------------------
 Number of cells + halo cells:                         281798


 ----------------------------------------------------------
 Number of interior faces:                             543050

 ----------------------------------------------------------
 Number of boundary faces:                             41092

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =        752
      2 : [          3 ;          4 ] =     281046

 ----------------------------------------------------------
 Number of cells:                                      281798

 ----------------------------------------------------------
 Number of cells + halo cells:                         281798


 ----------------------------------------------------------
 Number of interior faces:                             543050

 ----------------------------------------------------------
 Number of boundary faces:                             41092

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =        752
      2 : [          3 ;          4 ] =     281046

 ----------------------------------------------------------
 Number of cells:                                      281798

 ----------------------------------------------------------
 Number of cells + halo cells:                         281798


 ----------------------------------------------------------
 Number of interior faces:                             543050

 ----------------------------------------------------------
 Number of boundary faces:                             41092

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =        752
      2 : [          3 ;          4 ] =     281046

 ----------------------------------------------------------
 Number of cells:                                      281798

 ----------------------------------------------------------
 Number of cells + halo cells:                         281798


 ----------------------------------------------------------
 Number of interior faces:                             543050

 ----------------------------------------------------------
 Number of boundary faces:                             41092

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =        752
      2 : [          3 ;          4 ] =     281046

 ----------------------------------------------------------
 Number of cells:                                      281798

 ----------------------------------------------------------
 Number of cells + halo cells:                         281798


 ----------------------------------------------------------
 Number of interior faces:                             543050

 ----------------------------------------------------------
 Number of boundary faces:                             41092

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =        752
      2 : [          3 ;          4 ] =     281046

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

 Start unwarping algorithm


  Histogram of the boundary faces warping before unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         2.27374e-13

      1 : [ 0.00000e+00 ; 2.27374e-14 [ =      41090
      2 : [ 2.27374e-14 ; 4.54747e-14 [ =          1
      3 : [ 4.54747e-14 ; 6.82121e-14 [ =          0
      4 : [ 6.82121e-14 ; 9.09495e-14 [ =          0
      5 : [ 9.09495e-14 ; 1.13687e-13 [ =          0
      6 : [ 1.13687e-13 ; 1.36424e-13 [ =          0
      7 : [ 1.36424e-13 ; 1.59162e-13 [ =          0
      8 : [ 1.59162e-13 ; 1.81899e-13 [ =          0
      9 : [ 1.81899e-13 ; 2.04636e-13 [ =          0
     10 : [ 2.04636e-13 ; 2.27374e-13 ] =          1

  Histogram of the interior faces warping before unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         2.84217e-14

      1 : [ 0.00000e+00 ; 3.55271e-15 [ =     541597
      2 : [ 3.55271e-15 ; 7.10543e-15 [ =          0
      3 : [ 7.10543e-15 ; 1.06581e-14 [ =          0
      4 : [ 1.06581e-14 ; 1.42109e-14 [ =          0
      5 : [ 1.42109e-14 ; 1.77636e-14 [ =       1452
      6 : [ 1.77636e-14 ; 2.13163e-14 [ =          0
      7 : [ 2.13163e-14 ; 2.48690e-14 [ =          0
      8 : [ 2.48690e-14 ; 2.84217e-14 ] =          1

Unwarping algorithm converged at iteration 51 

  Histogram of the boundary faces warping after unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         2.27374e-13

      1 : [ 0.00000e+00 ; 2.27374e-14 [ =      41090
      2 : [ 2.27374e-14 ; 4.54747e-14 [ =          1
      3 : [ 4.54747e-14 ; 6.82121e-14 [ =          0
      4 : [ 6.82121e-14 ; 9.09495e-14 [ =          0
      5 : [ 9.09495e-14 ; 1.13687e-13 [ =          0
      6 : [ 1.13687e-13 ; 1.36424e-13 [ =          0
      7 : [ 1.36424e-13 ; 1.59162e-13 [ =          0
      8 : [ 1.59162e-13 ; 1.81899e-13 [ =          0
      9 : [ 1.81899e-13 ; 2.04636e-13 [ =          0
     10 : [ 2.04636e-13 ; 2.27374e-13 ] =          1

  Histogram of the interior faces warping after unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         2.84217e-14

      1 : [ 0.00000e+00 ; 3.55271e-15 [ =     541657
      2 : [ 3.55271e-15 ; 7.10543e-15 [ =          0
      3 : [ 7.10543e-15 ; 1.06581e-14 [ =          0
      4 : [ 1.06581e-14 ; 1.42109e-14 [ =          0
      5 : [ 1.42109e-14 ; 1.77636e-14 [ =       1392
      6 : [ 1.77636e-14 ; 2.13163e-14 [ =          0
      7 : [ 2.13163e-14 ; 2.48690e-14 [ =          0
      8 : [ 2.48690e-14 ; 2.84217e-14 ] =          1

 End unwarping algorithm


 Renumbering mesh:

   renumbering for cells:
     pre-numbering:                       none
     cells adjacent to ghost cells last:  no
     numbering:                           none

   renumbering for interior faces:
     cell adjacency pre-ordering:         lowest id first
     faces adjacent to ghost cells last:  no
     numbering:                           none

   renumbering for boundary faces:
     numbering:                           none

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

 Matrix bandwidth for volume mesh :          281012
 Matrix profile/lines for volume mesh :      150011

 Mesh coordinates:               minimum    and maximum
                       X : -1.2500000e-02  3.6300000e-02
                       Y : -4.0999997e-02  4.1100000e-02
                       Z : -1.9600000e-01  2.6999587e-02
 Mesh
     Number of cells:          281798
     Number of interior faces: 543050
     Number of boundary faces: 41092
     Number of vertices:       58517

 Groups:
    "inlet"
       boundary faces:           46
    "outlet"
       boundary faces:           46
    "spool"
       boundary faces:        12041
    "wall"
       boundary faces:        28959


 Start unwarping algorithm


  Histogram of the boundary faces warping before unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         2.27374e-13

      1 : [ 0.00000e+00 ; 2.27374e-14 [ =      41090
      2 : [ 2.27374e-14 ; 4.54747e-14 [ =          1
      3 : [ 4.54747e-14 ; 6.82121e-14 [ =          0
      4 : [ 6.82121e-14 ; 9.09495e-14 [ =          0
      5 : [ 9.09495e-14 ; 1.13687e-13 [ =          0
      6 : [ 1.13687e-13 ; 1.36424e-13 [ =          0
      7 : [ 1.36424e-13 ; 1.59162e-13 [ =          0
      8 : [ 1.59162e-13 ; 1.81899e-13 [ =          0
      9 : [ 1.81899e-13 ; 2.04636e-13 [ =          0
     10 : [ 2.04636e-13 ; 2.27374e-13 ] =          1

  Histogram of the interior faces warping before unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         2.84217e-14

      1 : [ 0.00000e+00 ; 3.55271e-15 [ =     541597
      2 : [ 3.55271e-15 ; 7.10543e-15 [ =          0
      3 : [ 7.10543e-15 ; 1.06581e-14 [ =          0
      4 : [ 1.06581e-14 ; 1.42109e-14 [ =          0
      5 : [ 1.42109e-14 ; 1.77636e-14 [ =       1452
      6 : [ 1.77636e-14 ; 2.13163e-14 [ =          0
      7 : [ 2.13163e-14 ; 2.48690e-14 [ =          0
      8 : [ 2.48690e-14 ; 2.84217e-14 ] =          1

Unwarping algorithm converged at iteration 51 

  Histogram of the boundary faces warping after unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         2.27374e-13

      1 : [ 0.00000e+00 ; 2.27374e-14 [ =      41090
      2 : [ 2.27374e-14 ; 4.54747e-14 [ =          1
      3 : [ 4.54747e-14 ; 6.82121e-14 [ =          0
      4 : [ 6.82121e-14 ; 9.09495e-14 [ =          0
      5 : [ 9.09495e-14 ; 1.13687e-13 [ =          0
      6 : [ 1.13687e-13 ; 1.36424e-13 [ =          0
      7 : [ 1.36424e-13 ; 1.59162e-13 [ =          0
      8 : [ 1.59162e-13 ; 1.81899e-13 [ =          0
      9 : [ 1.81899e-13 ; 2.04636e-13 [ =          0
     10 : [ 2.04636e-13 ; 2.27374e-13 ] =          1

  Histogram of the interior faces warping after unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         2.84217e-14

      1 : [ 0.00000e+00 ; 3.55271e-15 [ =     541657
      2 : [ 3.55271e-15 ; 7.10543e-15 [ =          0
      3 : [ 7.10543e-15 ; 1.06581e-14 [ =          0
      4 : [ 1.06581e-14 ; 1.42109e-14 [ =          0
      5 : [ 1.42109e-14 ; 1.77636e-14 [ =       1392
      6 : [ 1.77636e-14 ; 2.13163e-14 [ =          0
      7 : [ 2.13163e-14 ; 2.48690e-14 [ =          0
      8 : [ 2.48690e-14 ; 2.84217e-14 ] =          1

 End unwarping algorithm


 Renumbering mesh:

   renumbering for cells:
     pre-numbering:                       none
     cells adjacent to ghost cells last:  no
     numbering:                           none

   renumbering for interior faces:
     cell adjacency pre-ordering:         lowest id first
     faces adjacent to ghost cells last:  no
     numbering:                           none

   renumbering for boundary faces:
     numbering:                           none

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

 Matrix bandwidth for volume mesh :          281012
 Matrix profile/lines for volume mesh :      150011

 Mesh coordinates:               minimum    and maximum
                       X : -1.2500000e-02  3.6300000e-02
                       Y : -4.0999997e-02  4.1100000e-02
                       Z : -1.9600000e-01  2.6999587e-02
 Mesh
     Number of cells:          281798
     Number of interior faces: 543050
     Number of boundary faces: 41092
     Number of vertices:       58517

 Groups:
    "inlet"
       boundary faces:           46
    "outlet"
       boundary faces:           46
    "spool"
       boundary faces:        12041
    "wall"
       boundary faces:        28959

 --- Information on the volumes
       Minimum control volume      =  8.2511771e-17
       Maximum control volume      =  1.2573842e-07
       Total volume for the domain =  2.4563177e-04

  Criterion 1: Orthogonality:
    Number of bad cells detected: 37 -->   0 %

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

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 62 -->   0 %

  Criterion 4: Cells Volume Ratio:
    Number of bad cells detected: 55 -->   0 %

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

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

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

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

 Computing geometric quantities (1.5 s)
                                                             

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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Pressure          0.0000E+00  0.0000E+00
  k                 0.6000E-03  0.6000E-03
  epsilon           0.5291E-04  0.5291E-04
 ---------------------------------

                dt  0.1000E-01  0.1000E-01
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.100000000E-01   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  0.5389E+00  0.5389E+00
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2          46
Smooth wall               5       41000
Rough wall                6           0
Symmetry                  4           0
Free outlet               3          46
Free inlet               13           0
Convective inlet         15           0
Free surface             14           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.17627E-01   0.19512E-01  -0.19600E+00



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46         0.000000000E+00
Smooth wall               5       41000         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.000000000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+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    :  0.71516E-05 0.46005E-02
   Dimensionless distance   yplus :  0.91255E-09 0.25844E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      41000
   Total number of wall faces                   :      41000
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          1
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.40272E-01      15   0.13912E+00   0.93503E+02 0.28672E+03 
c  Velocity[X]                                      0.13857E+02 
c  Velocity[Y]                                      0.25235E+02 
c  Velocity[Z]                                      0.54411E+02 
c  Pressure     0.39909E-01    2004   0.53027E+01   0.97898E+00 0.37727E+03 
c  k            0.52769E-02      42   0.45410E-01   0.15099E-02 0.92926E+02 
c  epsilon      0.17035E+00      44   0.23354E-01   0.31074E+01 0.94562E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon        
a  Local Time Step      2.8941e-09                        222927


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.78786          4.0337         0.10855        0.039886
v  Velocity[Y]             -3.0184          5.3982         0.13007        0.088416
v  Velocity[Z]             -5.0521           3.309       -0.020468       0.0029897
v  ǁVelocityǁ             0.005864          6.7945         0.33683           0.663
v  Pressure                  35.77           54658           30146           28472
v  k                    5.5024e-09        0.045325      0.00038354       0.0011531
v  epsilon              5.2489e-05          1.6423        0.001546        0.040263
v  TurbVisc                0.53889         0.53889         0.53889         0.53889
v  CourantNb                     0               0               0               0
v  FourierNb                3.3671      3.4553e+06          317.83          9.9458
v  total_pressure       5.0004e+05      5.5466e+05      5.3015e+05      5.2847e+05
v  Local Time Step           0.001           0.011        0.001379       0.0077333


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          3.3671      3.4553e+06          317.83          9.9458


 TIME FOR THE TIME STEP                1:        0.18059E+03

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


 INSTANT    0.200000000E-01   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442453838E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15543E+00 0.29584E+01
   Friction velocity        uet   :  0.15079E-01 0.22103E+02
   Friction velocity        uk    :  0.15003E-01 0.22103E+02
   Dimensionless distance   yplus :  0.26100E-02 0.69409E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         68
   Nb of faces within the viscous sub-layer     :      35489
   Total number of wall faces                   :      41000
------------------------------------------------------------


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


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10217E+01      33   0.26536E-01   0.28175E+02 0.16403E+03 
c  Velocity[X]                                      0.15848E+01 
c  Velocity[Y]                                      0.32721E+01 
c  Velocity[Z]                                      0.23318E+02 
c  Pressure     0.34972E-01    1674   0.18649E+01   0.97118E+00 0.75409E+03 
c  k            0.17900E-01      31   0.30925E-01   0.18867E+00 0.92912E+03 
c  epsilon      0.31516E+03      30   0.24817E-01   0.12414E+09 0.99964E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon        
a  Local Time Step      4.2223e-08                        236595


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.57187          2.9371         0.14014        0.047994
v  Velocity[Y]             -2.9204          5.1179         0.16546         0.10963
v  Velocity[Z]             -4.5166          2.8197       -0.029071       0.0027594
v  ǁVelocityǁ            0.0038704          6.0412         0.43361         0.84258
v  Pressure                 115.15           59983           32371           30980
v  k                    4.9388e-09          2.0476       0.0031674       0.0039276
v  epsilon              5.2427e-05           84935          35.462          11.089
v  TurbVisc             4.5323e-11         0.53823         0.23769         0.22118
v  CourantNb            0.00025155          3308.8           3.008          1.1174
v  FourierNb               0.04679      2.3684e+05          43.756          2.4989
v  total_pressure       5.0012e+05      5.5998e+05      5.3237e+05      5.3098e+05
v  Local Time Step           0.001          0.0121       0.0010561       0.0014749


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0468      2.3751e+05          46.764          3.6162


 TIME FOR THE TIME STEP                2:        0.15993E+03

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


 INSTANT    0.300000000E-01   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.349019187E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442483855E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41103E+00 0.18712E+01
   Friction velocity        uet   :  0.14947E-01 0.14784E+02
   Friction velocity        uk    :  0.14711E-01 0.14784E+02
   Dimensionless distance   yplus :  0.16186E-02 0.69741E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        501
   Nb of faces within the viscous sub-layer     :      34814
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15701E+01      27   0.17541E-01   0.10997E+02 0.98169E+02 
c  Velocity[X]                                      0.11746E+01 
c  Velocity[Y]                                      0.19440E+01 
c  Velocity[Z]                                      0.78782E+01 
c  Pressure     0.72786E-01    1545   0.45752E+00   0.15933E+01 0.36197E+03 
c  k            0.15629E-01      11   0.14469E-01   0.12405E+00 0.16360E+04 
c  epsilon      0.25030E+03       8   0.24482E-01   0.11473E+09 0.17910E+05 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00091793                            42
a  epsilon                -0.95448                             3
a  Local Time Step      4.2206e-08                        234571


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.57575          3.0043         0.15984        0.051413
v  Velocity[Y]             -2.2839          3.6207          0.1812          0.1213
v  Velocity[Z]             -4.1969          2.6189       -0.035701      0.00062236
v  ǁVelocityǁ           0.00023748          5.5938         0.49024         0.93883
v  Pressure                 78.456           39376           22345           20669
v  k                    4.8321e-09         0.37138       0.0010765       0.0029956
v  epsilon              5.2995e-05          8324.5          2.3568          1.4602
v  TurbVisc             3.2516e-11         0.52478        0.068448         0.01927
v  CourantNb            0.00025982          1447.1          2.9647          1.1331
v  FourierNb               0.03859      2.3693e+05          31.231         0.77834
v  total_pressure       5.0008e+05      5.3938e+05      5.2234e+05      5.2067e+05
v  Local Time Step           0.001         0.01331       0.0010616        0.001469


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83267      2.3724e+05          34.195          1.9115


 TIME FOR THE TIME STEP                3:        0.15731E+03

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


 INSTANT    0.400000000E-01   TIME STEP NUMBER               4
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.789528405E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442526344E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60408E+00 0.15750E+01
   Friction velocity        uet   :  0.11385E-01 0.56885E+01
   Friction velocity        uk    :  0.11380E-01 0.56885E+01
   Dimensionless distance   yplus :  0.54967E-03 0.69408E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        817
   Nb of faces within the viscous sub-layer     :      34466
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16076E+01      25   0.15000E-01   0.26352E+01 0.50036E+02 
c  Velocity[X]                                      0.61514E+00 
c  Velocity[Y]                                      0.10211E+01 
c  Velocity[Z]                                      0.99893E+00 
c  Pressure     0.30635E-01    2127   0.66618E+00   0.55895E+00 0.14046E+04 
c  k            0.14167E-01      10   0.19143E-02   0.14895E-02 0.16788E+03 
c  epsilon      0.14952E+03       7   0.11280E-02   0.11112E+06 0.48318E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.9011e-05                            59
a  epsilon                 -1.3087                            23
a  Local Time Step      4.2202e-08                        231444


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.61314          3.1017         0.16607        0.050956
v  Velocity[Y]             -2.5641           4.242         0.17763         0.12191
v  Velocity[Z]              -5.031          3.0899       -0.039879     -0.00091082
v  ǁVelocityǁ           0.00026894          6.2955         0.50526         0.94644
v  Pressure                  -3762           12111          8165.8            6728
v  k                    6.5333e-10         0.49695         0.00104       0.0031023
v  epsilon              1.5961e-05          9950.1          1.8028          1.2101
v  TurbVisc             1.5776e-12         0.51091        0.061335        0.016531
v  CourantNb            0.00090759          566.62          2.7092          1.1441
v  FourierNb              0.036536      2.3696e+05          30.345         0.73462
v  total_pressure       4.9624e+05      5.1211e+05      5.0817e+05      5.0673e+05
v  Local Time Step           0.001        0.014641        0.001073       0.0014779


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59196      2.3707e+05          33.054          1.8787


 TIME FOR THE TIME STEP                4:        0.19423E+03

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


 INSTANT    0.500000000E-01   TIME STEP NUMBER               5
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.210731266E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442509344E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51624E+00 0.15606E+01
   Friction velocity        uet   :  0.11076E-01 0.69726E+01
   Friction velocity        uk    :  0.11057E-01 0.69726E+01
   Dimensionless distance   yplus :  0.65820E-03 0.69781E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        818
   Nb of faces within the viscous sub-layer     :      34596
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14844E+01      23   0.15095E-01   0.26817E+01 0.50654E+02 
c  Velocity[X]                                      0.61442E+00 
c  Velocity[Y]                                      0.10091E+01 
c  Velocity[Z]                                      0.10582E+01 
c  Pressure     0.41802E-01    2040   0.39249E+00   0.71234E+00 0.13784E+04 
c  k            0.14064E-01      14   0.13004E-02   0.98933E-03 0.13260E+03 
c  epsilon      0.10429E+03      13   0.17665E-02   0.18618E+06 0.85020E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.2075e-05                            19
a  epsilon                -0.04506                            19
a  Local Time Step      4.2218e-08                        227833


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.73224           3.116          0.1677        0.050205
v  Velocity[Y]             -2.8164          4.8585         0.16764         0.11881
v  Velocity[Z]             -5.7962          3.9303        -0.04179     -0.00091227
v  ǁVelocityǁ           0.00016541          6.8645         0.50587         0.92701
v  Pressure                -9002.5          5587.6          2784.6          1645.7
v  k                    8.0707e-10         0.46384        0.001073       0.0032493
v  epsilon              4.1815e-06          9241.7          1.6551           1.185
v  TurbVisc             5.3206e-13         0.49164        0.055569        0.014647
v  CourantNb            0.00030918          501.94          2.6729          1.1539
v  FourierNb              0.035395      2.3687e+05          29.604         0.70249
v  total_pressure         4.91e+05      5.0559e+05      5.0278e+05      5.0165e+05
v  Local Time Step           0.001        0.016105       0.0010857       0.0014882


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48665      2.3708e+05          32.277          1.8564


 TIME FOR THE TIME STEP                5:        0.16319E+03

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


 INSTANT    0.600000000E-01   TIME STEP NUMBER               6
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.306523941E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442502733E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70898E+00 0.15734E+01
   Friction velocity        uet   :  0.66604E-02 0.56393E+01
   Friction velocity        uk    :  0.66524E-02 0.56393E+01
   Dimensionless distance   yplus :  0.54555E-03 0.69757E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        717
   Nb of faces within the viscous sub-layer     :      34743
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14068E+01      23   0.16874E-01   0.24318E+01 0.49562E+02 
c  Velocity[X]                                      0.68548E+00 
c  Velocity[Y]                                      0.96875E+00 
c  Velocity[Z]                                      0.77756E+00 
c  Pressure     0.29370E-01    1502   0.15214E+00   0.49317E+00 0.19970E+03 
c  k            0.14316E-01      14   0.58332E-03   0.46441E-03 0.87125E+02 
c  epsilon      0.10141E+03      13   0.78104E-03   0.19889E+05 0.28364E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.1028e-05                            10
a  epsilon               -0.077301                             9
a  Local Time Step      4.2256e-08                        225379


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -0.9985          3.0642         0.17047        0.050209
v  Velocity[Y]             -2.9269            4.83         0.16011         0.11686
v  Velocity[Z]             -6.3041          3.7067       -0.042206     -0.00034429
v  ǁVelocityǁ            4.616e-05          7.1648         0.50932         0.91638
v  Pressure                -8073.6          6264.6          3590.3          2573.2
v  k                     1.808e-09         0.49693       0.0011061        0.003365
v  epsilon              2.9885e-06           10027          1.6878          1.1874
v  TurbVisc             1.6535e-13         0.46381        0.049136        0.013083
v  CourantNb            0.00078608           481.7          2.7136          1.1637
v  FourierNb              0.034972      2.3665e+05          28.611         0.67067
v  total_pressure       4.9193e+05      5.0626e+05      5.0359e+05      5.0257e+05
v  Local Time Step           0.001        0.017716       0.0010995       0.0014989


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49849      2.3705e+05          31.325          1.8344


 TIME FOR THE TIME STEP                6:        0.14267E+03

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


 INSTANT    0.700000000E-01   TIME STEP NUMBER               7
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.211163343E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442476117E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85040E+00 0.16355E+01
   Friction velocity        uet   :  0.13095E-02 0.69400E+01
   Friction velocity        uk    :  0.13097E-02 0.69400E+01
   Dimensionless distance   yplus :  0.45189E-03 0.70098E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        652
   Nb of faces within the viscous sub-layer     :      34780
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13988E+01      26   0.17819E-01   0.21253E+01 0.46576E+02 
c  Velocity[X]                                      0.67865E+00 
c  Velocity[Y]                                      0.85235E+00 
c  Velocity[Z]                                      0.59427E+00 
c  Pressure     0.18937E-01    1401   0.14721E+00   0.31930E+00 0.28265E+03 
c  k            0.14473E-01      17   0.14338E-02   0.46261E-03 0.85742E+02 
c  epsilon      0.94633E+02      16   0.22672E-02   0.32899E+05 0.38391E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.2014e-05                            22
a  epsilon                 -11.235                            33
a  Local Time Step      4.2273e-08                        223420


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7379           3.211         0.17551        0.050548
v  Velocity[Y]             -3.2247          5.0443         0.15617         0.11663
v  Velocity[Z]             -6.6051          4.1095       -0.042239      0.00011424
v  ǁVelocityǁ            0.0001833           7.311         0.51877         0.91793
v  Pressure                  -5857            8201          5575.9          4531.6
v  k                    1.6582e-09         0.51971       0.0011502       0.0034646
v  epsilon              1.3669e-06           11008          1.8059          1.1962
v  TurbVisc             7.7334e-14         0.43992        0.043683        0.011854
v  CourantNb            0.00094645          516.68          2.7926          1.1738
v  FourierNb              0.034884      2.3656e+05          27.786         0.64515
v  total_pressure       4.9414e+05       5.082e+05      5.0558e+05      5.0453e+05
v  Local Time Step           0.001        0.019487       0.0011137       0.0015092


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44153      2.3708e+05          30.579           1.819


 TIME FOR THE TIME STEP                7:        0.12306E+03

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


 INSTANT    0.800000000E-01   TIME STEP NUMBER               8
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.127524328E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442440679E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.90908E+00 0.16828E+01
   Friction velocity        uet   :  0.10826E-01 0.98682E+01
   Friction velocity        uk    :  0.10822E-01 0.98682E+01
   Dimensionless distance   yplus :  0.76058E-03 0.70704E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        637
   Nb of faces within the viscous sub-layer     :      34799
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14173E+01      24   0.17853E-01   0.19766E+01 0.44532E+02 
c  Velocity[X]                                      0.62486E+00 
c  Velocity[Y]                                      0.77819E+00 
c  Velocity[Z]                                      0.57352E+00 
c  Pressure     0.18681E-01    1577   0.15289E+00   0.31897E+00 0.11480E+03 
c  k            0.14684E-01      13   0.49485E-03   0.39206E-03 0.77625E+02 
c  epsilon      0.96516E+02       9   0.54455E-03   0.17902E+05 0.28675E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.7147e-06                             5
a  epsilon               -0.017409                            11
a  Local Time Step      4.2277e-08                        221989


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6731          3.3089         0.18182         0.05074
v  Velocity[Y]             -3.4336          4.9899         0.15426         0.11711
v  Velocity[Z]             -6.6856          4.4952       -0.042335       0.0002359
v  ǁVelocityǁ           2.3204e-05          7.4795         0.53149          0.9239
v  Pressure                -4258.9          9790.7          6551.6          5445.7
v  k                    1.8979e-09         0.53211       0.0011841       0.0035584
v  epsilon              1.5832e-06           11613          1.8202           1.215
v  TurbVisc             5.3024e-14         0.41658        0.038919        0.010856
v  CourantNb            0.00044323          607.87          2.8904          1.1837
v  FourierNb              0.034856      2.3654e+05          27.072         0.62384
v  total_pressure       4.9574e+05      5.0979e+05      5.0655e+05      5.0545e+05
v  Local Time Step           0.001        0.021436       0.0011283       0.0015202


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6261      2.3714e+05          29.962          1.8076


 TIME FOR THE TIME STEP                8:        0.16026E+03

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


 INSTANT    0.900000000E-01   TIME STEP NUMBER               9
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.175343388E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442481833E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89262E+00 0.16344E+01
   Friction velocity        uet   :  0.19680E-02 0.12367E+02
   Friction velocity        uk    :  0.19686E-02 0.12367E+02
   Dimensionless distance   yplus :  0.92562E-03 0.71297E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        635
   Nb of faces within the viscous sub-layer     :      34777
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14319E+01      24   0.18721E-01   0.18884E+01 0.43178E+02 
c  Velocity[X]                                      0.57849E+00 
c  Velocity[Y]                                      0.75792E+00 
c  Velocity[Z]                                      0.55203E+00 
c  Pressure     0.17249E-01    1647   0.13397E+00   0.29765E+00 0.10636E+02 
c  k            0.14886E-01      19   0.76588E-03   0.28910E-03 0.65077E+02 
c  epsilon      0.89848E+02      13   0.64572E-03   0.86016E+04 0.20267E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.5055e-05                             7
a  epsilon                -0.99546                            12
a  Local Time Step      4.2277e-08                        220851


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1984          3.1903         0.18839        0.050623
v  Velocity[Y]             -3.2643          4.7673         0.15267         0.11746
v  Velocity[Z]             -6.7642          4.7553       -0.042355      0.00022166
v  ǁVelocityǁ           6.4611e-05           7.539         0.54501         0.92893
v  Pressure                -4090.4          9776.4            6571          5445.1
v  k                    2.6343e-09         0.48775       0.0012328       0.0036457
v  epsilon              7.0872e-06           10181          2.0099          1.2403
v  TurbVisc             7.6893e-14         0.39694        0.035606        0.010087
v  CourantNb            0.00012475          815.82          2.9941          1.1934
v  FourierNb              0.034809      2.3653e+05          26.662          0.6094
v  total_pressure       4.9591e+05      5.0978e+05      5.0657e+05      5.0545e+05
v  Local Time Step           0.001        0.023579       0.0011434       0.0015324


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69943      2.3735e+05          29.657          1.8028


 TIME FOR THE TIME STEP                9:        0.14073E+03

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


 INSTANT    0.100000000E+00   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.703898651E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442494763E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84247E+00 0.15822E+01
   Friction velocity        uet   :  0.44100E-02 0.13738E+02
   Friction velocity        uk    :  0.44157E-02 0.13738E+02
   Dimensionless distance   yplus :  0.10220E-02 0.71901E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        630
   Nb of faces within the viscous sub-layer     :      34764
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14370E+01      22   0.20008E-01   0.17374E+01 0.41106E+02 
c  Velocity[X]                                      0.50673E+00 
c  Velocity[Y]                                      0.72310E+00 
c  Velocity[Z]                                      0.50754E+00 
c  Pressure     0.15418E-01    1419   0.11708E+00   0.26579E+00 0.28918E+02 
c  k            0.15068E-01      18   0.49308E-03   0.32049E-03 0.67801E+02 
c  epsilon      0.84831E+02      11   0.88069E-03   0.11269E+05 0.23165E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.2319e-05                             6
a  epsilon               -0.041658                             7
a  Local Time Step      4.2278e-08                        219635


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.2182          3.3644         0.19499        0.050477
v  Velocity[Y]             -3.2095          4.6597         0.15105          0.1176
v  Velocity[Z]             -7.1492           4.804       -0.042299      0.00020107
v  ǁVelocityǁ            6.245e-05          8.0328         0.55849         0.93216
v  Pressure                -4117.3            9346          6331.9          5217.6
v  k                    2.3434e-09          0.4663       0.0012799        0.003726
v  epsilon              9.3784e-06            9513           2.087          1.2745
v  TurbVisc             7.8676e-14         0.37455        0.032147        0.009397
v  CourantNb            6.5041e-05          1060.4          3.0984          1.2024
v  FourierNb              0.034743      2.3653e+05          26.201         0.59517
v  total_pressure       4.9588e+05      5.0935e+05      5.0633e+05      5.0522e+05
v  Local Time Step           0.001        0.025937       0.0011592       0.0015462


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57333      2.3748e+05            29.3          1.7976


 TIME FOR THE TIME STEP               10:        0.13482E+03

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


 INSTANT    0.110000000E+00   TIME STEP NUMBER              11
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.793299489E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442498440E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83566E+00 0.15584E+01
   Friction velocity        uet   :  0.44258E-02 0.14332E+02
   Friction velocity        uk    :  0.44231E-02 0.14332E+02
   Dimensionless distance   yplus :  0.11043E-02 0.72392E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        634
   Nb of faces within the viscous sub-layer     :      34744
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14382E+01      25   0.20396E-01   0.16529E+01 0.39872E+02 
c  Velocity[X]                                      0.48148E+00 
c  Velocity[Y]                                      0.69824E+00 
c  Velocity[Z]                                      0.47322E+00 
c  Pressure     0.13891E-01    1565   0.10235E+00   0.23778E+00 0.17145E+02 
c  k            0.15259E-01      16   0.51145E-03   0.33952E-03 0.69433E+02 
c  epsilon      0.85180E+02      12   0.87325E-03   0.22521E+05 0.31437E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.1977e-05                             7
a  epsilon                -0.50864                            12
a  Local Time Step      4.2278e-08                        218729


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0941          3.5208         0.20159        0.050402
v  Velocity[Y]             -3.5526          4.4458         0.14957         0.11765
v  Velocity[Z]             -7.4469          4.8461       -0.042391      0.00010478
v  ǁVelocityǁ           0.00011252          8.3398         0.57171         0.93452
v  Pressure                -4017.8          9114.9          6181.7          5090.9
v  k                    2.2466e-09         0.46493       0.0013407       0.0037966
v  epsilon              9.8375e-06          9344.4          2.3659          1.3103
v  TurbVisc             1.0074e-13         0.35536        0.029349       0.0088298
v  CourantNb            4.3672e-05            1228          3.2038          1.2107
v  FourierNb              0.034705      2.3653e+05          25.854         0.58446
v  total_pressure       4.9598e+05      5.0911e+05      5.0618e+05      5.0509e+05
v  Local Time Step           0.001        0.028531       0.0011754       0.0015617


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51419      2.3737e+05          29.058          1.7951


 TIME FOR THE TIME STEP               11:        0.14422E+03

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


 INSTANT    0.120000000E+00   TIME STEP NUMBER              12
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.141521228E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442482191E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.82506E+00 0.15648E+01
   Friction velocity        uet   :  0.31648E-02 0.14524E+02
   Friction velocity        uk    :  0.31817E-02 0.14524E+02
   Dimensionless distance   yplus :  0.12542E-02 0.72859E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        629
   Nb of faces within the viscous sub-layer     :      34708
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14398E+01      27   0.20941E-01   0.15463E+01 0.38365E+02 
c  Velocity[X]                                      0.43937E+00 
c  Velocity[Y]                                      0.67133E+00 
c  Velocity[Z]                                      0.43559E+00 
c  Pressure     0.13056E-01    1229   0.93856E-01   0.22030E+00 0.61444E+01 
c  k            0.15443E-01      14   0.37432E-03   0.28327E-03 0.63043E+02 
c  epsilon      0.87693E+02      10   0.67124E-03   0.16512E+05 0.26534E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -3.252e-05                             9
a  epsilon               -0.043112                            11
a  Local Time Step      4.2278e-08                        217769


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -0.99088           3.391         0.20832        0.050326
v  Velocity[Y]             -3.8928          4.2937         0.14853         0.11764
v  Velocity[Z]             -7.4894          5.0323       -0.042509     -4.7787e-06
v  ǁVelocityǁ           0.00018207          8.3096         0.58467         0.93673
v  Pressure                -3797.1          9078.3          6128.8          5064.7
v  k                    2.1826e-09          0.4755       0.0013917       0.0038613
v  epsilon              1.2758e-05          9606.4          2.4827          1.3458
v  TurbVisc              1.417e-13           0.337        0.026788       0.0083336
v  CourantNb            0.00013483          1342.8          3.3118          1.2184
v  FourierNb              0.034656      2.3653e+05          25.549         0.57493
v  total_pressure        4.962e+05      5.0908e+05      5.0613e+05      5.0506e+05
v  Local Time Step           0.001        0.031384       0.0011924       0.0015785


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59266      2.3706e+05          28.861          1.7933


 TIME FOR THE TIME STEP               12:        0.12196E+03

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


 INSTANT    0.130000000E+00   TIME STEP NUMBER              13
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.553954633E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442516560E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88960E+00 0.15828E+01
   Friction velocity        uet   :  0.47724E-02 0.14619E+02
   Friction velocity        uk    :  0.47861E-02 0.14619E+02
   Dimensionless distance   yplus :  0.15245E-02 0.73314E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        619
   Nb of faces within the viscous sub-layer     :      34662
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14428E+01      24   0.20961E-01   0.14834E+01 0.37365E+02 
c  Velocity[X]                                      0.41088E+00 
c  Velocity[Y]                                      0.65013E+00 
c  Velocity[Z]                                      0.42238E+00 
c  Pressure     0.12806E-01    1034   0.90119E-01   0.21358E+00 0.44714E+01 
c  k            0.15604E-01      14   0.33942E-03   0.30586E-03 0.64682E+02 
c  epsilon      0.91257E+02      12   0.78451E-03   0.12302E+05 0.22258E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.4097e-05                             8
a  epsilon               -0.044568                            10
a  Local Time Step      4.2278e-08                        216866


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.0664           3.221         0.21493         0.05025
v  Velocity[Y]             -3.9877          4.1235         0.14817         0.11763
v  Velocity[Z]             -7.3466          5.1841        -0.04259     -8.0711e-05
v  ǁVelocityǁ           0.00036853          8.1044         0.59702         0.93894
v  Pressure                -3573.5          9097.3          6112.1          5069.2
v  k                    2.1443e-09         0.48208       0.0014607       0.0039207
v  epsilon              1.4822e-05          9857.3          2.7479          1.3812
v  TurbVisc             2.0696e-13         0.32046        0.024673       0.0079201
v  CourantNb             0.0008049          1345.2          3.4229          1.2255
v  FourierNb              0.034634      2.3653e+05          25.311         0.56762
v  total_pressure       4.9643e+05       5.091e+05      5.0611e+05      5.0507e+05
v  Local Time Step           0.001        0.034523       0.0012101       0.0015962


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6689      2.3674e+05          28.734          1.7931


 TIME FOR THE TIME STEP               13:        0.10111E+03

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


 INSTANT    0.140000000E+00   TIME STEP NUMBER              14
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.261106332E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442521881E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89517E+00 0.15981E+01
   Friction velocity        uet   :  0.71087E-02 0.13728E+02
   Friction velocity        uk    :  0.71018E-02 0.13728E+02
   Dimensionless distance   yplus :  0.17517E-02 0.73702E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        620
   Nb of faces within the viscous sub-layer     :      34609
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14465E+01      22   0.21804E-01   0.13969E+01 0.36095E+02 
c  Velocity[X]                                      0.37254E+00 
c  Velocity[Y]                                      0.61433E+00 
c  Velocity[Z]                                      0.41000E+00 
c  Pressure     0.12366E-01    1044   0.85135E-01   0.20318E+00 0.41735E+01 
c  k            0.15750E-01      13   0.32428E-03   0.26149E-03 0.59282E+02 
c  epsilon      0.93298E+02      11   0.52964E-03   0.10332E+05 0.20025E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.4595e-05                             8
a  epsilon                 -1.1701                             7
a  Local Time Step      4.2278e-08                        215877


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1095          3.1724         0.22142        0.050211
v  Velocity[Y]             -3.9141          4.0319         0.14829         0.11764
v  Velocity[Z]             -7.2968          5.3049       -0.042673     -0.00012661
v  ǁVelocityǁ           0.00012572          8.0425         0.60881          0.9412
v  Pressure                -3499.1            9099          6088.5          5064.8
v  k                    2.1434e-09         0.49096       0.0015216       0.0039756
v  epsilon              1.5958e-05           10097           2.881          1.4183
v  TurbVisc             2.8811e-13         0.30415        0.022666       0.0075534
v  CourantNb                     0            1191          3.5239          1.2321
v  FourierNb              0.034602      2.3653e+05          25.079         0.56083
v  total_pressure        4.965e+05       5.091e+05      5.0609e+05      5.0506e+05
v  Local Time Step           0.001        0.037975       0.0012285       0.0016145


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53545      2.3683e+05          28.603          1.7929


 TIME FOR THE TIME STEP               14:        0.11584E+03

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


 INSTANT    0.150000000E+00   TIME STEP NUMBER              15
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.304453872E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442558594E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.82798E+00 0.15996E+01
   Friction velocity        uet   :  0.31661E-02 0.14904E+02
   Friction velocity        uk    :  0.31756E-02 0.14904E+02
   Dimensionless distance   yplus :  0.19018E-02 0.74202E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        621
   Nb of faces within the viscous sub-layer     :      34542
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14503E+01      24   0.22704E-01   0.12977E+01 0.34654E+02 
c  Velocity[X]                                      0.33074E+00 
c  Velocity[Y]                                      0.57769E+00 
c  Velocity[Z]                                      0.38925E+00 
c  Pressure     0.12440E-01    1037   0.83471E-01   0.20143E+00 0.47507E+01 
c  k            0.15868E-01      18   0.33404E-03   0.27921E-03 0.60806E+02 
c  epsilon      0.92281E+02       9   0.34178E-03   0.95682E+04 0.19105E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.6669e-05                             9
a  epsilon               -0.054071                             6
a  Local Time Step      4.2278e-08                        214902


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1094          3.1385         0.22757        0.050167
v  Velocity[Y]             -4.0008          3.9572         0.14908         0.11769
v  Velocity[Z]             -7.2642          5.3663       -0.042622     -0.00017517
v  ǁVelocityǁ            0.0002018          7.9838         0.61986         0.94339
v  Pressure                -3475.3          9064.8          6051.1          5042.5
v  k                    2.3162e-09         0.48003       0.0015903       0.0040287
v  epsilon              1.6794e-05          9933.4          3.0491            1.46
v  TurbVisc             2.5328e-13         0.28927        0.020903       0.0072373
v  CourantNb            8.1774e-05          1041.3          3.6238          1.2383
v  FourierNb              0.034578      2.3653e+05          24.879         0.55526
v  total_pressure       4.9652e+05      5.0906e+05      5.0605e+05      5.0504e+05
v  Local Time Step           0.001        0.041772       0.0012471       0.0016333


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64458      2.3675e+05          28.503          1.7935


 TIME FOR THE TIME STEP               15:        0.11599E+03

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


 INSTANT    0.160000000E+00   TIME STEP NUMBER              16
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.838530193E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442552986E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.78115E+00 0.15987E+01
   Friction velocity        uet   :  0.38093E-02 0.15263E+02
   Friction velocity        uk    :  0.38213E-02 0.15263E+02
   Dimensionless distance   yplus :  0.19476E-02 0.74640E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        630
   Nb of faces within the viscous sub-layer     :      34458
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14537E+01      23   0.23327E-01   0.11989E+01 0.33209E+02 
c  Velocity[X]                                      0.29674E+00 
c  Velocity[Y]                                      0.53508E+00 
c  Velocity[Z]                                      0.36709E+00 
c  Pressure     0.12837E-01    1377   0.84089E-01   0.20474E+00 0.53501E+01 
c  k            0.15970E-01      12   0.37450E-03   0.29272E-03 0.61370E+02 
c  epsilon      0.90823E+02       9   0.49552E-03   0.12682E+05 0.21654E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.9023e-05                             8
a  epsilon               -0.054554                             7
a  Local Time Step      4.2278e-08                        214110


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.1849          3.1812         0.23306        0.050124
v  Velocity[Y]             -4.0008           3.954         0.15032         0.11773
v  Velocity[Z]             -7.1166          5.4196       -0.042715     -0.00020707
v  ǁVelocityǁ           0.00012897          7.8136         0.62986         0.94536
v  Pressure                -3467.2          9017.1          6005.7          5011.3
v  k                    2.3962e-09         0.47844       0.0016545       0.0040786
v  epsilon              2.0016e-05          9897.5          3.2673           1.495
v  TurbVisc              1.834e-13         0.27611        0.019389       0.0069699
v  CourantNb            0.00029104          1049.5          3.7216          1.2439
v  FourierNb                0.0345      2.3653e+05          24.707         0.55103
v  total_pressure       4.9653e+05      5.0902e+05      5.0601e+05      5.0501e+05
v  Local Time Step           0.001         0.04595       0.0012654       0.0016526


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47621      2.3669e+05          28.428          1.7949


 TIME FOR THE TIME STEP               16:        0.12919E+03

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


 INSTANT    0.170000000E+00   TIME STEP NUMBER              17
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.272344366E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442474964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76629E+00 0.15744E+01
   Friction velocity        uet   :  0.58906E-02 0.14082E+02
   Friction velocity        uk    :  0.58850E-02 0.14082E+02
   Dimensionless distance   yplus :  0.17969E-02 0.74889E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        636
   Nb of faces within the viscous sub-layer     :      34399
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14568E+01      21   0.24097E-01   0.11142E+01 0.31921E+02 
c  Velocity[X]                                      0.26620E+00 
c  Velocity[Y]                                      0.50049E+00 
c  Velocity[Z]                                      0.34752E+00 
c  Pressure     0.13225E-01     840   0.80871E-01   0.20767E+00 0.34789E+01 
c  k            0.16061E-01      16   0.36004E-03   0.28934E-03 0.60755E+02 
c  epsilon      0.86882E+02      12   0.58191E-03   0.13015E+05 0.21721E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.1754e-05                             5
a  epsilon              -0.0059169                             4
a  Local Time Step      4.2278e-08                        213382


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.2585          3.2115         0.23778        0.050122
v  Velocity[Y]             -3.9039          3.9498         0.15185         0.11779
v  Velocity[Z]             -7.2494          5.4179       -0.042801     -0.00025326
v  ǁVelocityǁ           0.00019267           7.962         0.63855         0.94717
v  Pressure                -3457.7          8997.4            5987          5002.4
v  k                     2.622e-09         0.46204        0.001732       0.0041257
v  epsilon               2.456e-05          9412.7          3.5788          1.5372
v  TurbVisc             1.1075e-13          0.2642        0.018083       0.0067379
v  CourantNb            0.00094153          978.09          3.8111          1.2489
v  FourierNb              0.034469      2.3653e+05          24.568         0.54758
v  total_pressure       4.9654e+05        5.09e+05      5.0599e+05        5.05e+05
v  Local Time Step           0.001        0.050545       0.0012835       0.0016716


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56548      2.3665e+05          28.379          1.7965


 TIME FOR THE TIME STEP               17:        0.10521E+03

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


 INSTANT    0.180000000E+00   TIME STEP NUMBER              18
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.154125509E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442550865E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72187E+00 0.15670E+01
   Friction velocity        uet   :  0.42459E-02 0.11730E+02
   Friction velocity        uk    :  0.42407E-02 0.11730E+02
   Dimensionless distance   yplus :  0.14763E-02 0.75183E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        641
   Nb of faces within the viscous sub-layer     :      34326
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14603E+01      20   0.24089E-01   0.10311E+01 0.30603E+02 
c  Velocity[X]                                      0.23852E+00 
c  Velocity[Y]                                      0.46304E+00 
c  Velocity[Z]                                      0.32952E+00 
c  Pressure     0.12991E-01     892   0.75203E-01   0.19997E+00 0.25912E+01 
c  k            0.16144E-01      17   0.34687E-03   0.26582E-03 0.57887E+02 
c  epsilon      0.84803E+02      15   0.53600E-03   0.10601E+05 0.19449E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.9556e-05                             6
a  epsilon                -0.15204                             9
a  Local Time Step      4.2278e-08                        212507


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.319          3.2453         0.24179        0.050104
v  Velocity[Y]             -3.8314          3.9654          0.1533         0.11784
v  Velocity[Z]             -7.3411          5.4174       -0.043002     -0.00026873
v  ǁVelocityǁ            0.0001291          8.0386         0.64616         0.94888
v  Pressure                -3458.3          8996.9          5979.4          4999.5
v  k                    3.0701e-09         0.46088       0.0017874       0.0041675
v  epsilon              4.0885e-06          9398.7          3.7619          1.5674
v  TurbVisc             5.8187e-14         0.25161        0.016708       0.0065213
v  CourantNb            0.00037313          903.06          3.8895          1.2535
v  FourierNb              0.034399      2.3653e+05          24.407          0.5441
v  total_pressure       4.9654e+05        5.09e+05      5.0598e+05        5.05e+05
v  Local Time Step           0.001        0.055599       0.0013014       0.0016903


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4229      2.3664e+05          28.296          1.7977


 TIME FOR THE TIME STEP               18:        0.10564E+03

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


 INSTANT    0.190000000E+00   TIME STEP NUMBER              19
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.296469200E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442518709E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69449E+00 0.15538E+01
   Friction velocity        uet   :  0.39859E-02 0.11707E+02
   Friction velocity        uk    :  0.39825E-02 0.11707E+02
   Dimensionless distance   yplus :  0.14201E-02 0.75483E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        640
   Nb of faces within the viscous sub-layer     :      34261
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14634E+01      22   0.24565E-01   0.94157E+00 0.29204E+02 
c  Velocity[X]                                      0.21725E+00 
c  Velocity[Y]                                      0.41382E+00 
c  Velocity[Z]                                      0.31050E+00 
c  Pressure     0.12477E-01    1189   0.67896E-01   0.18857E+00 0.27968E+01 
c  k            0.16226E-01      14   0.24810E-03   0.25486E-03 0.56408E+02 
c  epsilon      0.83081E+02      10   0.58589E-03   0.10477E+05 0.19119E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.5472e-05                             6
a  epsilon                -0.03274                             4
a  Local Time Step      4.2278e-08                        211767


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.3773          3.2501         0.24503        0.050084
v  Velocity[Y]             -3.7926          4.0098         0.15447         0.11785
v  Velocity[Z]              -7.344          5.4124       -0.043319     -0.00027674
v  ǁVelocityǁ             0.000153          8.0458         0.65261         0.95044
v  Pressure                -3492.2          8976.5          5966.2          4988.9
v  k                    3.9187e-09         0.45611       0.0018443       0.0042072
v  epsilon              2.8375e-05          9198.8          3.9676          1.5999
v  TurbVisc             5.2814e-14         0.24007        0.015543       0.0063363
v  CourantNb            0.00058792            1009          3.9605          1.2577
v  FourierNb              0.034348      2.3653e+05          24.277          0.5412
v  total_pressure       4.9651e+05      5.0898e+05      5.0597e+05      5.0499e+05
v  Local Time Step           0.001        0.061159       0.0013185       0.0017068


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66975      2.3663e+05          28.238          1.7989


 TIME FOR THE TIME STEP               19:        0.11824E+03

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


 INSTANT    0.200000000E+00   TIME STEP NUMBER              20
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.211364565E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442520355E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72171E+00 0.15327E+01
   Friction velocity        uet   :  0.45028E-02 0.12196E+02
   Friction velocity        uk    :  0.44987E-02 0.12196E+02
   Dimensionless distance   yplus :  0.15562E-02 0.75762E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        647
   Nb of faces within the viscous sub-layer     :      34199
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14662E+01      20   0.25315E-01   0.87404E+00 0.28092E+02 
c  Velocity[X]                                      0.19863E+00 
c  Velocity[Y]                                      0.38517E+00 
c  Velocity[Z]                                      0.29024E+00 
c  Pressure     0.11585E-01     422   0.61423E-01   0.17237E+00 0.21790E+01 
c  k            0.16290E-01      16   0.30445E-03   0.22179E-03 0.52334E+02 
c  epsilon      0.80412E+02      10   0.59536E-03   0.88861E+04 0.17463E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -1.321e-05                             5
a  epsilon               -0.057751                             4
a  Local Time Step      4.2278e-08                        211046


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.3858          3.2726         0.24767        0.050088
v  Velocity[Y]             -3.6955          4.0268         0.15537         0.11791
v  Velocity[Z]             -6.8292          5.4198       -0.043787     -0.00025932
v  ǁVelocityǁ           0.00012616           7.544         0.65832         0.95186
v  Pressure                -3529.4          8980.3          5967.1          4989.5
v  k                    6.4092e-09         0.45076       0.0019069        0.004243
v  epsilon              3.1886e-05          8959.9          4.1759          1.6261
v  TurbVisc             6.0005e-14         0.22932        0.014526       0.0061778
v  CourantNb            0.00027445          1007.2          4.0188          1.2613
v  FourierNb              0.034265      2.3653e+05          24.167         0.53919
v  total_pressure       4.9647e+05      5.0898e+05      5.0597e+05      5.0499e+05
v  Local Time Step           0.001        0.067275       0.0013351       0.0017228


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59546       2.366e+05          28.186          1.8005


 TIME FOR THE TIME STEP               20:        0.81547E+02

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


 INSTANT    0.210000000E+00   TIME STEP NUMBER              21
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.282444707E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442515761E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.73598E+00 0.15238E+01
   Friction velocity        uet   :  0.51014E-02 0.13440E+02
   Friction velocity        uk    :  0.50968E-02 0.13440E+02
   Dimensionless distance   yplus :  0.17149E-02 0.76035E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        655
   Nb of faces within the viscous sub-layer     :      34132
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14690E+01      20   0.25799E-01   0.82082E+00 0.27145E+02 
c  Velocity[X]                                      0.18378E+00 
c  Velocity[Y]                                      0.36037E+00 
c  Velocity[Z]                                      0.27666E+00 
c  Pressure     0.11668E-01     786   0.60566E-01   0.17150E+00 0.21645E+01 
c  k            0.16363E-01      13   0.29449E-03   0.31051E-03 0.61769E+02 
c  epsilon      0.79719E+02      10   0.53191E-03   0.12137E+05 0.20090E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.1966e-05                             5
a  epsilon               -0.056337                             6
a  Local Time Step      4.2278e-08                        210310


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.4335          3.2716         0.24965        0.050079
v  Velocity[Y]             -3.6699          4.0233         0.15594         0.11802
v  Velocity[Z]             -7.0304          5.4081       -0.044411     -0.00022685
v  ǁVelocityǁ           0.00012374          7.7651         0.66332         0.95316
v  Pressure                -3610.9          8984.8          5968.4          4989.3
v  k                    7.1403e-09         0.45304        0.001964       0.0042779
v  epsilon              1.8262e-05            8959          4.3744          1.6593
v  TurbVisc             9.6459e-14         0.21882        0.013568       0.0060369
v  CourantNb              0.001992          1202.1          4.0689          1.2648
v  FourierNb               0.03421      2.3653e+05          24.058         0.53705
v  total_pressure       4.9639e+05      5.0898e+05      5.0597e+05      5.0499e+05
v  Local Time Step           0.001        0.074002       0.0013506       0.0017363


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62375      2.3679e+05          28.126          1.8018


 TIME FOR THE TIME STEP               21:        0.10466E+03

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


 INSTANT    0.220000000E+00   TIME STEP NUMBER              22
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.235353857E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442464563E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74659E+00 0.15242E+01
   Friction velocity        uet   :  0.76227E-02 0.13174E+02
   Friction velocity        uk    :  0.76176E-02 0.13174E+02
   Dimensionless distance   yplus :  0.16810E-02 0.76257E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        658
   Nb of faces within the viscous sub-layer     :      34114
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14715E+01      22   0.24911E-01   0.77151E+00 0.26253E+02 
c  Velocity[X]                                      0.17198E+00 
c  Velocity[Y]                                      0.33652E+00 
c  Velocity[Z]                                      0.26301E+00 
c  Pressure     0.11427E-01     853   0.58053E-01   0.16583E+00 0.21656E+01 
c  k            0.16379E-01      11   0.45815E-03   0.24163E-03 0.52539E+02 
c  epsilon      0.74374E+02       8   0.84639E-03   0.21432E+05 0.25306E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.6859e-05                             4
a  epsilon               -0.058343                             5
a  Local Time Step      4.2278e-08                        209563


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.482          3.2909         0.25112        0.050101
v  Velocity[Y]             -3.6736          4.0168         0.15628         0.11816
v  Velocity[Z]             -6.9126          5.4365       -0.045275     -0.00020938
v  ǁVelocityǁ           0.00013558          7.6485         0.66777          0.9544
v  Pressure                -3686.7          8987.6          5969.9          4989.6
v  k                    9.3408e-09         0.45441       0.0019923       0.0043047
v  epsilon              4.1133e-05            8995          4.3777          1.6655
v  TurbVisc             7.4111e-14          0.2094        0.012723       0.0059143
v  CourantNb             0.0010904          1141.6          4.1126           1.268
v  FourierNb              0.034111      2.3653e+05          23.966         0.53538
v  total_pressure       4.9631e+05      5.0899e+05      5.0597e+05      5.0499e+05
v  Local Time Step           0.001        0.081403       0.0013654       0.0017493


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68479      2.3714e+05          28.079          1.8033


 TIME FOR THE TIME STEP               22:        0.95604E+02

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


 INSTANT    0.230000000E+00   TIME STEP NUMBER              23
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.256854016E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442455418E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76811E+00 0.15149E+01
   Friction velocity        uet   :  0.48298E-02 0.12890E+02
   Friction velocity        uk    :  0.48454E-02 0.12890E+02
   Dimensionless distance   yplus :  0.15955E-02 0.76478E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        653
   Nb of faces within the viscous sub-layer     :      34072
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14741E+01      20   0.25200E-01   0.71468E+00 0.25241E+02 
c  Velocity[X]                                      0.15948E+00 
c  Velocity[Y]                                      0.30824E+00 
c  Velocity[Z]                                      0.24695E+00 
c  Pressure     0.11083E-01     498   0.55885E-01   0.15966E+00 0.22303E+01 
c  k            0.16432E-01      14   0.28011E-03   0.21088E-03 0.50483E+02 
c  epsilon      0.73749E+02      10   0.52257E-03   0.87381E+04 0.17421E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.2261e-05                             3
a  epsilon               -0.053578                             5
a  Local Time Step      4.2278e-08                        208918


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.5129           3.281         0.25219         0.05015
v  Velocity[Y]             -3.6608          4.0175         0.15626         0.11824
v  Velocity[Z]              -6.746          5.3726       -0.046225     -0.00022437
v  ǁVelocityǁ             0.000147          7.4976         0.67185          0.9556
v  Pressure                -3778.6          8990.8          5969.1          4992.6
v  k                    1.3481e-08         0.44715       0.0020491       0.0043322
v  epsilon              3.5402e-05          8804.4          4.5314          1.6913
v  TurbVisc             1.0409e-13         0.20127        0.012031       0.0058128
v  CourantNb                     0          1026.3          4.1493          1.2709
v  FourierNb              0.034069      2.3653e+05          23.895         0.53407
v  total_pressure       4.9622e+05      5.0899e+05      5.0597e+05      5.0499e+05
v  Local Time Step           0.001        0.089543       0.0013785       0.0017594


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82925      2.3719e+05          28.044           1.805


 TIME FOR THE TIME STEP               23:        0.76623E+02

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


 INSTANT    0.240000000E+00   TIME STEP NUMBER              24
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.280417641E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442521631E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75647E+00 0.14839E+01
   Friction velocity        uet   :  0.57753E-02 0.10540E+02
   Friction velocity        uk    :  0.57757E-02 0.10540E+02
   Dimensionless distance   yplus :  0.13449E-02 0.76709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        655
   Nb of faces within the viscous sub-layer     :      34036
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14768E+01      18   0.26053E-01   0.66933E+00 0.24381E+02 
c  Velocity[X]                                      0.14411E+00 
c  Velocity[Y]                                      0.29351E+00 
c  Velocity[Z]                                      0.23171E+00 
c  Pressure     0.11151E-01     932   0.54438E-01   0.15886E+00 0.24656E+01 
c  k            0.16474E-01      12   0.33060E-03   0.24745E-03 0.54515E+02 
c  epsilon      0.71133E+02      11   0.66311E-03   0.12421E+05 0.20675E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.0059e-05                             3
a  epsilon               -0.054827                             6
a  Local Time Step      4.2278e-08                        208249


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.5378          3.2847         0.25293        0.050191
v  Velocity[Y]             -3.6624          4.0162         0.15609         0.11832
v  Velocity[Z]             -6.6456          5.3616       -0.047363     -0.00024264
v  ǁVelocityǁ           0.00013099          7.3988         0.67557         0.95673
v  Pressure                -3870.9          8981.9          5954.9          4983.8
v  k                    1.6776e-08          0.4304       0.0020847       0.0043558
v  epsilon              5.3375e-05          8328.1          4.6981          1.7091
v  TurbVisc               1.44e-13         0.19249        0.011296       0.0057137
v  CourantNb             0.0012527          719.76          4.1808          1.2737
v  FourierNb              0.033971      2.3653e+05           23.81         0.53186
v  total_pressure       4.9613e+05      5.0898e+05      5.0595e+05      5.0498e+05
v  Local Time Step           0.001        0.098497       0.0013902       0.0017684


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85493      2.3723e+05          27.991          1.8056


 TIME FOR THE TIME STEP               24:        0.10242E+03

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


 INSTANT    0.250000000E+00   TIME STEP NUMBER              25
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.277135256E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442539036E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74661E+00 0.14593E+01
   Friction velocity        uet   :  0.38030E-02 0.95762E+01
   Friction velocity        uk    :  0.38689E-02 0.95762E+01
   Dimensionless distance   yplus :  0.98513E-03 0.76906E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        656
   Nb of faces within the viscous sub-layer     :      33995
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14791E+01      19   0.25382E-01   0.63693E+00 0.23752E+02 
c  Velocity[X]                                      0.13625E+00 
c  Velocity[Y]                                      0.27697E+00 
c  Velocity[Z]                                      0.22372E+00 
c  Pressure     0.10564E-01     516   0.50965E-01   0.14955E+00 0.20393E+01 
c  k            0.16514E-01      16   0.25482E-03   0.24024E-03 0.53489E+02 
c  epsilon      0.69495E+02      11   0.50076E-03   0.12336E+05 0.20460E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.2921e-05                             9
a  epsilon                -0.24774                            18
a  Local Time Step      4.2278e-08                        207646


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.5519          3.2774         0.25351        0.050199
v  Velocity[Y]             -3.6446          4.0248         0.15574         0.11842
v  Velocity[Z]             -6.5252          5.3297       -0.048626     -0.00031085
v  ǁVelocityǁ           6.8057e-05          7.2968         0.67906         0.95781
v  Pressure                -3962.3          8984.2          5953.1          4984.5
v  k                    1.4902e-08         0.42416       0.0021201       0.0043779
v  epsilon              5.9792e-05          8101.7          4.8444          1.7265
v  TurbVisc              1.428e-13          0.1839        0.010611       0.0056256
v  CourantNb            0.00035038          975.91          4.2123          1.2761
v  FourierNb              0.033888      2.3653e+05          23.729         0.52948
v  total_pressure       4.9604e+05      5.0898e+05      5.0595e+05      5.0498e+05
v  Local Time Step           0.001         0.10835       0.0014003        0.001776


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.80203      2.3751e+05          27.941          1.8056


 TIME FOR THE TIME STEP               25:        0.66163E+02

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


 INSTANT    0.260000000E+00   TIME STEP NUMBER              26
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.409788616E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442578059E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80559E+00 0.14556E+01
   Friction velocity        uet   :  0.42249E-02 0.90216E+01
   Friction velocity        uk    :  0.42246E-02 0.90216E+01
   Dimensionless distance   yplus :  0.70161E-03 0.77096E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        646
   Nb of faces within the viscous sub-layer     :      33967
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14814E+01      19   0.24597E-01   0.59273E+00 0.22889E+02 
c  Velocity[X]                                      0.12965E+00 
c  Velocity[Y]                                      0.25356E+00 
c  Velocity[Z]                                      0.20952E+00 
c  Pressure     0.10278E-01    1216   0.48866E-01   0.14479E+00 0.35109E+01 
c  k            0.16553E-01      13   0.23722E-03   0.16259E-03 0.44004E+02 
c  epsilon      0.69559E+02      10   0.45679E-03   0.78311E+04 0.16134E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.4673e-05                            10
a  epsilon                -0.19089                            13
a  Local Time Step      4.2278e-08                        207122


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6394          3.2744         0.25395        0.050209
v  Velocity[Y]             -3.6589          4.0303         0.15529         0.11852
v  Velocity[Z]             -6.5355          5.3017       -0.050008     -0.00034211
v  ǁVelocityǁ           0.00013857          7.3179          0.6822         0.95879
v  Pressure                -4054.4          8958.1          5921.6          4963.9
v  k                    2.2464e-08         0.42738       0.0021438       0.0043976
v  epsilon              1.5102e-05          8159.1          4.8988          1.7402
v  TurbVisc             1.7282e-13         0.17576       0.0099917       0.0055487
v  CourantNb             0.0013195            1169          4.2428          1.2783
v  FourierNb              0.033795      2.3653e+05          23.652         0.52692
v  total_pressure       4.9595e+05      5.0896e+05      5.0592e+05      5.0496e+05
v  Local Time Step           0.001         0.11918       0.0014088       0.0017816


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7607       2.377e+05          27.895          1.8052


 TIME FOR THE TIME STEP               26:        0.12452E+03

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


 INSTANT    0.270000000E+00   TIME STEP NUMBER              27
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.297254793E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442604376E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80594E+00 0.14511E+01
   Friction velocity        uet   :  0.73835E-02 0.81431E+01
   Friction velocity        uk    :  0.73722E-02 0.81431E+01
   Dimensionless distance   yplus :  0.62347E-03 0.77285E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        644
   Nb of faces within the viscous sub-layer     :      33945
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14835E+01      20   0.24913E-01   0.55427E+00 0.22082E+02 
c  Velocity[X]                                      0.12002E+00 
c  Velocity[Y]                                      0.23494E+00 
c  Velocity[Z]                                      0.19930E+00 
c  Pressure     0.10033E-01    1374   0.47711E-01   0.14083E+00 0.41051E+01 
c  k            0.16586E-01      12   0.19657E-03   0.14584E-03 0.41528E+02 
c  epsilon      0.69425E+02      10   0.33152E-03   0.67028E+04 0.14759E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1809e-05                             9
a  epsilon               -0.050738                            15
a  Local Time Step      4.2278e-08                        206445


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6472          3.2779         0.25446        0.050228
v  Velocity[Y]             -3.6484          4.0459         0.15473         0.11861
v  Velocity[Z]             -6.5623          5.2899       -0.051341     -0.00028337
v  ǁVelocityǁ            0.0001146          7.3445         0.68519         0.95971
v  Pressure                -4159.2          8930.9          5880.2          4938.1
v  k                    2.3956e-08         0.42402       0.0021692       0.0044156
v  epsilon              2.4706e-05          8076.2          5.0098          1.7523
v  TurbVisc             1.7649e-13         0.16801       0.0094323       0.0054808
v  CourantNb            0.00066415          1056.6          4.2687          1.2803
v  FourierNb              0.033722      2.3653e+05          23.582         0.52425
v  
  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7607       2.377e+05          27.895          1.8052


 TIME FOR THE TIME STEP               26:        0.10954E+03

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


 INSTANT    0.270000000E+00   TIME STEP NUMBER              27
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.297254793E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442604376E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80594E+00 0.14511E+01
   Friction velocity        uet   :  0.73835E-02 0.81431E+01
   Friction velocity        uk    :  0.73722E-02 0.81431E+01
   Dimensionless distance   yplus :  0.62347E-03 0.77285E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        644
   Nb of faces within the viscous sub-layer     :      33945
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14835E+01      20   0.24913E-01   0.55427E+00 0.22082E+02 
c  Velocity[X]                                      0.12002E+00 
c  Velocity[Y]                                      0.23494E+00 
c  Velocity[Z]                                      0.19930E+00 
c  Pressure     0.10033E-01    1374   0.47711E-01   0.14083E+00 0.41051E+01 
c  k            0.16586E-01      12   0.19657E-03   0.14584E-03 0.41528E+02 
c  epsilon      0.69425E+02      10   0.33152E-03   0.67028E+04 0.14759E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1809e-05                             9
a  epsilon          -  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0165e-05                             9
a  epsilon                 -0.1012                            17
a  Local Time Step      4.2278e-08                        205974


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6746           3.263         0.25491        0.050243
v  Velocity[Y]             -3.6821          4.0609         0.15415         0.11868
v  Velocity[Z]             -6.5787          5.2821       -0.052805     -0.00031884
v  ǁVelocityǁ           0.00024448          7.3738         0.68793         0.96058
v  Pressure                  -4237          8922.4          5870.4          4935.2
v  k                    2.5405e-08         0.40379       0.0021871       0.0044323
v  epsilon              3.8347e-05          7252.6          5.0224           1.756
v  TurbVisc             1.8015e-13         0.16061       0.0089209       0.0054201
v  CourantNb             0.0015699          1051.2          4.2944          1.2821
v  FourierNb              0.033624      2.3653e+05          23.518         0.52167
v  total_pressure       4.9576e+05      5.0892e+05      5.0587e+05      5.0494e+05
v  Local Time Step           0.001         0.13894       0.0014221       0.0017883


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67786      2.3758e+05          27.812          1.8037


 TIME FOR THE TIME STEP               28:        0.89649E+02

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


 INSTANT    0.290000000E+00   TIME STEP NUMBER              29
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.324633102E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442556017E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83932E+00 0.14490E+01
   Friction velocity        uet   :  0.45017E-02 0.71446E+01
   Friction velocity        uk    :  0.44997E-02 0.71446E+01
   Dimensionless distance   yplus :  0.79971E-03 0.77471E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        639
   Nb of faces within the viscous sub-layer     :      33887
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14865E+01      18   0.25058E-01   0.50576E+00 0.20997E+02 
c  Velocity[X]                                      0.10771E+00 
c  Velocity[Y]                                      0.21229E+00 
c  Velocity[Z]                                      0.18575E+00 
c  Pressure     0.98048E-02     674   0.46319E-01   0.13729E+00 0.19513E+01 
c  k            0.16539E-01      11   0.21280E-03   0.10992E-03 0.35885E+02 
c  epsilon      0.43543E+02      10   0.58603E-03   0.31842E+04 0.10988E+03 
------------------------------------------------------------------------  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0165e-05                             9
a  epsilon                 -0.1012                            17
a  Local Time Step      4.2278e-08                        205974


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6746           3.263         0.25491        0.050243
v  Velocity[Y]             -3.6821          4.0609         0.15415         0.11868
v  Velocity[Z]             -6.5787          5.2821       -0.052805     -0.00031884
v  ǁVelocityǁ           0.00024448          7.3738         0.68793         0.96058
v  Pressure                  -4237          8922.4          5870.4          4935.2
v  k                    2.5405e-08         0.40379       0.0021871       0.0044323
v  epsilon              3.8347e-05          7252.6          5.0224           1.756
v  TurbVisc             1.8015e-13         0.16061       0.0089209       0.0054201
v  CourantNb             0.0015699          1051.2          4.2944          1.2821
v  FourierNb              0.033624      2.3653e+05          23.518         0.52167
v  total_pressure       4.9576e+05      5.0892e+05      5.0587e+05      5.0494e+05
v  Local Time Step           0.001         0.13894       0.0014221       0.0017883


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67786      2.3758e+05          27.812          1.8037


 TIME FOR THE TIME STEP               28:        0.11388E+03

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


 INSTANT    0.290000000E+00   TIME STEP NUMBER              29
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.324633102E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442556017E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83932E+00 0.14490E+01
   Friction velocity        uet   :  0.45017E-02 0.71446E+01
   Friction velocity        uk    :  0.44997E-02 0.71446E+01
   Dimensionless distance   yplus :  0.799   Friction velocity        uet   :  0.25880E-02 0.69545E+01
   Friction velocity        uk    :  0.26990E-02 0.69545E+01
   Dimensionless distance   yplus :  0.87088E-03 0.77659E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        644
   Nb of faces within the viscous sub-layer     :      33876
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14880E+01      18   0.25306E-01   0.47248E+00 0.20243E+02 
c  Velocity[X]                                      0.10354E+00 
c  Velocity[Y]                                      0.18974E+00 
c  Velocity[Z]                                      0.17920E+00 
c  Pressure     0.96559E-02    1164   0.45144E-01   0.13472E+00 0.42273E+01 
c  k            0.16562E-01      10   0.20423E-03   0.11341E-03 0.36454E+02 
c  epsilon      0.43841E+02      13   0.69596E-03   0.82174E+04 0.17415E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.3701e-05                            11
a  epsilon                -0.13701                            19
a  Local Time Step      4.2278e-08                        205211


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6462          3.2748         0.25605        0.050275
v  Velocity[Y]             -3.7181          4.1103         0.15316         0.11868
v  Velocity[Z]             -6.6399          5.2718       -0.055745     -0.00037262
v  ǁVelocityǁ           0.00036818          7.4389         0.69292         0.96208
v  Pressure                -4381.2          8890.6          5826.7          4908.6
v  k                    2.7302e-08         0.40734       0.0022239       0.0044641
v  epsilon              2.3377e-05          7367.3           5.156          1.7772
v  TurbVisc             1.8507e-13          0.1469       0.0079801       0.0053153
v  CourantNb            0.00016434          821.41          4.3386          1.2853
v  FourierNb              0.033453      2.3653e+05          23.391         0.51519
v  total_pressure       4.9562e+05      5.0889e+05      5.0583e+05      5.0491e+05
v  Local Time Step           0.001         0.11858       0.0014286       0.0017916


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87257      2.3735e+05           27.73          1.8005


 TIME FOR THE TIME STEP               30:        0.12568E+03

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


 INSTANT    0.310000000E+00   TIME STEP NUMBER              31
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.241445126E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442591148E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                      Friction velocity        uet   :  0.25880E-02 0.69545E+01
   Friction velocity        uk    :  0.26990E-02 0.69545E+01
   Dimensionless distance   yplus :  0.87088E-03 0.77659E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        644
   Nb of faces within the viscous sub-layer     :      33876
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14880E+01      18   0.25306E-01   0.47248E+00 0.20243E+02 
c  Velocity[X]                                      0.10354E+00 
c  Velocity[Y]                                      0.18974E+00 
c  Velocity[Z]                                      0.17920E+00 
c  Pressure     0.96559E-02    1164   0.45144E-01   0.13472E+00 0.42273E+01 
c  k            0.16562E-01      10   0.20423E-03   0.11341E-03 0.36454E+02 
c  epsilon      0.43841E+02      13   0.69596E-03   0.82174E+04 0.17415E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.3701e-05                            11
a  epsilon                -0.13701                            19
a  Local Time Step      4.2278e-08                        205211


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6462          3.2748         0.25605        0.050275
v  Velocity[Y]             -3.7181          4.1103         0.15316         0.11868
v  Velocity[Z]             -6.6399          5.2718       -0.055745     -0.00037262
v  ǁVelocityǁ           0.00036818          7.4389         0.69292         0.96208
v  Pressure                -4381.2          8890.6          5826.7          4908.6
v  k                    2.7302e-08         0.40734       0.0022239       0.0044641
v  epsilon              2.3377e-05          7367.3           5.156          1.7772
v  TurbVisc             1.8507e-13          0.1469       0.0079801       0.0053153
v  CourantNb            0.00016434          821.41          4.3386          1.2853
v  FourierNb              0.033453      2.3653e+05          23.391         0.51519
v  total_pressure       4.9562e+05      5.0889e+05      5.0583e+05      5.0491e+05
v  Local Time Step           0.001         0.11858       0.0014286       0.0017916


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87257      2.3735e+05           27.73          1.8005


 TIME FOR THE TIME STEP               30:        0.10487E+03

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


 INSTANT    0.310000000E+00   TIME S TIME FOR THE TIME STEP               31:        0.78682E+02

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


 INSTANT    0.320000000E+00   TIME STEP NUMBER              32
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.511443676E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442608173E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85802E+00 0.14540E+01
   Friction velocity        uet   :  0.56086E-02 0.66589E+01
   Friction velocity        uk    :  0.56000E-02 0.66589E+01
   Dimensionless distance   yplus :  0.84967E-03 0.77871E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        638
   Nb of faces within the viscous sub-layer     :      33839
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14893E+01      16   0.25516E-01   0.44679E+00 0.19636E+02 
c  Velocity[X]                                      0.10173E+00 
c  Velocity[Y]                                      0.17778E+00 
c  Velocity[Z]                                      0.16728E+00 
c  Pressure     0.94572E-02     629   0.42981E-01   0.13134E+00 0.15586E+01 
c  k            0.16602E-01      10   0.20746E-03   0.12787E-03 0.38504E+02 
c  epsilon      0.44181E+02       9   0.61311E-03   0.65613E+04 0.15485E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.9652e-06                            11
a  epsilon               -0.063441                            21
a  Local Time Step      4.2278e-08                        204687


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6362          3.2796         0.25733        0.050246
v  Velocity[Y]             -3.8999          4.1633         0.15252         0.11866
v  Velocity[Z]             -6.6761          5.2398       -0.058546     -0.00036595
v  ǁVelocityǁ           0.00031351          7.4724         0.69716         0.96328
v  Pressure                -4462.2          8896.1          5821.3          4909.2
v  k                    2.8273e-08         0.40813        0.002247       0.0044926
v  epsilon              5.0584e-05          7404.5          5.2316          1.7957
v  TurbVisc             1.9143e-13         0.13367       0.0071631       0.0052289
v  CourantNb            0.00066153          629.57          4.3727          1.2881
v  FourierNb              0.033276      2.3653e+05          23.275         0.50778
v  total_pressure       4.9554e+05       5.089e+05      5.0582e+05      5.0491e+05
v  Local Time Step           0.001         0.13048       0.0014294       0.0017948


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

   criterion               minimum         maximum        set mean    spatial mean
   - TIME FOR THE TIME STEP               31:        0.79337E+02

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


 INSTANT    0.320000000E+00   TIME STEP NUMBER              32
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.511443676E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442608173E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85802E+00 0.14540E+01
   Friction velocity        uet   :  0.56086E-02 0.66589E+01
   Friction velocity        uk    :  0.56000E-02 0.66589E+01
   Dimensionless distance   yplus :  0.84967E-03 0.77871E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        638
   Nb of faces within the viscous sub-layer     :      33839
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14893E+01      16   0.25516E-01   0.44679E+00 0.19636E+02 
c  Velocity[X]                                      0.10173E+00 
c  Velocity[Y]                                      0.17778E+00 
c  Velocity[Z]                                      0.16728E+00 
c  Pressure     0.94572E-02     629   0.42981E-01   0.13134E+00 0.15586E+01 
c  k            0.16602E-01      10   0.20746E-03   0.12787E-03 0.38504E+02 
c  epsilon      0.44181E+02       9   0.61311E-03   0.65613E+04 0.15485E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.9652e-06                            11
a  epsilon               -0.063441                            21
a  Local Time Step      4.2278e-08                        204687


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  ------------
   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6429          3.2806         0.25807        0.050211
v  Velocity[Y]             -4.0451          4.1743         0.15234         0.11867
v  Velocity[Z]             -6.6809          5.2894       -0.059897     -0.00039659
v  ǁVelocityǁ             0.000366          7.4738         0.69912         0.96389
v  Pressure                -4474.6          8899.5          5817.8          4909.3
v  k                    2.8617e-08         0.40992        0.002257        0.004506
v  epsilon              3.4231e-06          7468.1          5.2451          1.8029
v  TurbVisc             1.9385e-13         0.12808       0.0068247       0.0051933
v  CourantNb            0.00085032          741.71          4.3875          1.2894
v  FourierNb              0.033196      2.3653e+05          23.225         0.50434
v  total_pressure       4.9553e+05       5.089e+05      5.0582e+05      5.0491e+05
v  Local Time Step           0.001         0.14353       0.0014287       0.0017973


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77413      2.3727e+05          27.613          1.7937


 TIME FOR THE TIME STEP               33:        0.75605E+02

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


 INSTANT    0.340000000E+00   TIME STEP NUMBER              34
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.308272146E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442595304E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87128E+00 0.14633E+01
   Friction velocity        uet   :  0.53291E-02 0.70002E+01
   Friction velocity        uk    :  0.53210E-02 0.70002E+01
   Dimensionless distance   yplus :  0.89323E-03 0.77912E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        629
   Nb of faces within the viscous sub-layer     :      33763
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14900E+01      17   0.25446E-01   0.41104E+00 0.18779E+02 
c  Velocity[X]                                      0.94130E-01 
c  Velocity[Y]                                      0.15975E+00 
c  Velocity[Z]                                      0.15716E+00 
c  Pressure     0.91562E-02     860   0.40960E-01   0.12578E+00 0.19913E+01 
c  k            0.16638E-01      10   0.19639E-03   0.11983E-03 0.37162E+02 
c  epsilon      0.44509E+02      10   0.53266E-03   0.42971E+04 0.12412E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.7332e-05                            10
a  epsilon                -0
   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6429          3.2806         0.25807        0.050211
v  Velocity[Y]             -4.0451          4.1743         0.15234         0.11867
v  Velocity[Z]             -6.6809          5.2894       -0.059897     -0.00039659
v  ǁVelocityǁ             0.000366          7.4738         0.69912         0.96389
v  Pressure                -4474.6          8899.5          5817.8          4909.3
v  k                    2.8617e-08         0.40992        0.002257        0.004506
v  epsilon              3.4231e-06          7468.1          5.2451          1.8029
v  TurbVisc             1.9385e-13         0.12808       0.0068247       0.0051933
v  CourantNb            0.00085032          741.71          4.3875          1.2894
v  FourierNb              0.033196      2.3653e+05          23.225         0.50434
v  total_pressure       4.9553e+05       5.089e+05      5.0582e+05      5.0491e+05
v  Local Time Step           0.001         0.14353       0.0014287       0.0017973


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77413      2.3727e+05          27.613          1.7937


 TIME FOR THE TIME STEP               33:        0.71524E+02

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


 INSTANT    0.340000000E+00   TIME STEP NUMBER              34
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.308272146E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442595304E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87128E+00 0.14633E+01
   Friction velocity        uet   :  0.53291E-02 0.70002E+01
   Friction velocity        uk    :  0.53210E-02 0.70002E+01
   Dimensionless distance   yplus :  0.89323E-03 0.77912E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        629
   Nb of faces within the viscous sub-layer     :      33763
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
         Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14898E+01      16   0.25306E-01   0.40448E+00 0.18616E+02 
c  Velocity[X]                                      0.95779E-01 
c  Velocity[Y]                                      0.15936E+00 
c  Velocity[Z]                                      0.14934E+00 
c  Pressure     0.91018E-02     425   0.40320E-01   0.12470E+00 0.13036E+01 
c  k            0.16658E-01      10   0.20356E-03   0.12017E-03 0.37263E+02 
c  epsilon      0.44806E+02      10   0.70072E-03   0.45992E+04 0.12771E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.7091e-06                             8
a  epsilon                -0.08179                            15
a  Local Time Step      4.2278e-08                        204606


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6517          3.2942          0.2594         0.05012
v  Velocity[Y]             -4.0433          4.2358         0.15247         0.11873
v  Velocity[Z]             -6.7327          5.2505       -0.062292     -0.00033174
v  ǁVelocityǁ           0.00034668          7.5239          0.7026         0.96499
v  Pressure                -4519.8          8891.9          5800.6          4898.8
v  k                    2.8722e-08         0.41098       0.0022855       0.0045335
v  epsilon              7.3261e-06            7512          5.3463          1.8263
v  TurbVisc             1.9755e-13         0.11771       0.0062201       0.0051297
v  CourantNb            9.2265e-05          586.22          4.4077           1.292
v  FourierNb               0.03299      2.3653e+05          23.132         0.49762
v  total_pressure       4.9548e+05      5.0889e+05       5.058e+05       5.049e+05
v  Local Time Step           0.001         0.15756       0.0014255        0.001804


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91255      2.3712e+05           27.54          1.7897


 TIME FOR THE TIME STEP               35:        0.68522E+02

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


 INSTANT    0.360000000E+00   TIME STEP NUMBER              36
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.388193643E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442483273E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89240E+00 0.14615E+01
   Friction velocity        uet   :  0.10372E-01 0.66579E+01
   Friction velocity        uk    :  0.10345E-01 0.66579E+01
   Dimensionless distance   yplus :  0.80677E-03 0.77857E+01
   -------------   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14898E+01      16   0.25306E-01   0.40448E+00 0.18616E+02 
c  Velocity[X]                                      0.95779E-01 
c  Velocity[Y]                                      0.15936E+00 
c  Velocity[Z]                                      0.14934E+00 
c  Pressure     0.91018E-02     425   0.40320E-01   0.12470E+00 0.13036E+01 
c  k            0.16658E-01      10   0.20356E-03   0.12017E-03 0.37263E+02 
c  epsilon      0.44806E+02      10   0.70072E-03   0.45992E+04 0.12771E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.7091e-06                             8
a  epsilon                -0.08179                            15
a  Local Time Step      4.2278e-08                        204606


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6517          3.2942          0.2594         0.05012
v  Velocity[Y]             -4.0433          4.2358         0.15247         0.11873
v  Velocity[Z]             -6.7327          5.2505       -0.062292     -0.00033174
v  ǁVelocityǁ           0.00034668          7.5239          0.7026         0.96499
v  Pressure                -4519.8          8891.9          5800.6          4898.8
v  k                    2.8722e-08         0.41098       0.0022855       0.0045335
v  epsilon              7.3261e-06            7512          5.3463          1.8263
v  TurbVisc             1.9755e-13         0.11771       0.0062201       0.0051297
v  CourantNb            9.2265e-05          586.22          4.4077           1.292
v  FourierNb               0.03299      2.3653e+05          23.132         0.49762
v  total_pressure       4.9548e+05      5.0889e+05       5.058e+05       5.049e+05
v  Local Time Step           0.001         0.15756       0.0014255        0.001804


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91255      2.3712e+05           27.54          1.7897


 TIME FOR THE TIME STEP               35:        0.78119E+02

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


 INSTANT    0.360000000E+00   TIME STEP NUMBER              36
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
-------------------------------------------------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.120226099E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442470058E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89780E+00 0.14637E+01
   Friction velocity        uet   :  0.79066E-02 0.66581E+01
   Friction velocity        uk    :  0.78866E-02 0.66581E+01
   Dimensionless distance   yplus :  0.73084E-03 0.77779E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        628
   Nb of faces within the viscous sub-layer     :      33657
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14894E+01      16   0.25343E-01   0.38398E+00 0.18103E+02 
c  Velocity[X]                                      0.90249E-01 
c  Velocity[Y]                                      0.14764E+00 
c  Velocity[Z]                                      0.14610E+00 
c  Pressure     0.88987E-02    1050   0.38770E-01   0.12011E+00 0.26830E+01 
c  k            0.16688E-01       9   0.15187E-03   0.95387E-04 0.33153E+02 
c  epsilon      0.45109E+02       9   0.33905E-03   0.23377E+04 0.90753E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0718e-05                             8
a  epsilon               -0.056953                            12
a  Local Time Step      4.2278e-08                        204862


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6634          3.2934         0.26075        0.050094
v  Velocity[Y]             -4.1866          4.2533         0.15303         0.11879
v  Velocity[Z]             -6.7085          5.2512       -0.064363     -0.00029312
v  ǁVelocityǁ           0.00021783          7.5004         0.70581         0.96609
v  Pressure                  -4525          8932.6          5829.9          4924.7
v  k                    2.8193e-08         0.41162       0.0023029       0.0045573
v  epsilon              1.1919e-05          7536.5          5.3833          1.8406
v  TurbVisc             1.9192e-13         0.11253       0.0057003       0.0050776
v  CourantNb             0.0017484          676.34          4.4224          1.2945
v  FourierNb              0.032778      2.3653e+05          23.045         0.49075
v  total_pressure       4.9548e+05      5.0893e+05      5.0583e+05      5.0492e+05
v  Local Time Step           0.001         0.15758       0.0014195       0.0018115


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.93131      2.3721e+05          27.467          1.7853


 TIME FOR THE TIME STEP               37:        0.96327E+02

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


 INSTANT    0.380000000E+00   TIME STEP NU---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.120226099E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442470058E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89780E+00 0.14637E+01
   Friction velocity        uet   :  0.79066E-02 0.66581E+01
   Friction velocity        uk    :  0.78866E-02 0.66581E+01
   Dimensionless distance   yplus :  0.73084E-03 0.77779E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        628
   Nb of faces within the viscous sub-layer     :      33657
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14894E+01      16   0.25343E-01   0.38398E+00 0.18103E+02 
c  Velocity[X]                                      0.90249E-01 
c  Velocity[Y]                                      0.14764E+00 
c  Velocity[Z]                                      0.14610E+00 
c  Pressure     0.88987E-02    1050   0.38770E-01   0.12011E+00 0.26830E+01 
c  k            0.16688E-01       9   0.15187E-03   0.95387E-04 0.33153E+02 
c  epsilon      0.45109E+02       9   0.33905E-03   0.23377E+04 0.90753E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0718e-05                             8
a  epsilon               -0.056953                            12
a  Local Time Step      4.2278e-08                        204862


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6634          3.2934         0.26075        0.050094
v  Velocity[Y]             -4.1866          4.2533         0.15303         0.11879
v  Velocity[Z]             -6.7085          5.2512       -0.064363     -0.00029312
v  ǁVelocityǁ           0.00021783          7.5004         0.70581         0.96v  Velocity[Z]             -6.7087          5.2382       -0.065312     -0.00028628
v  ǁVelocityǁ           0.00030652          7.5027         0.70741         0.96666
v  Pressure                -4544.3          8939.2          5829.9            4925
v  k                    2.8076e-08          0.4123       0.0023169       0.0045694
v  epsilon              3.0019e-05          7563.6          5.4261          1.8497
v  TurbVisc              1.897e-13         0.11253        0.005471       0.0050547
v  CourantNb             0.0009919          705.48           4.429          1.2958
v  FourierNb              0.032686      2.3653e+05          23.005         0.48739
v  total_pressure       4.9546e+05      5.0894e+05      5.0583e+05      5.0493e+05
v  Local Time Step           0.001         0.15758       0.0014159       0.0018133


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90812      2.3724e+05          27.434          1.7831


 TIME FOR THE TIME STEP               38:        0.99810E+02

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


 INSTANT    0.390000000E+00   TIME STEP NUMBER              39
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.379625793E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442434525E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88166E+00 0.14671E+01
   Friction velocity        uet   :  0.77748E-02 0.61289E+01
   Friction velocity        uk    :  0.77724E-02 0.61289E+01
   Dimensionless distance   yplus :  0.73966E-03 0.77517E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        630
   Nb of faces within the viscous sub-layer     :      33581
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14887E+01      17   0.26012E-01   0.37614E+00 0.17906E+02 
c  Velocity[X]                                      0.88516E-01 
c  Velocity[Y]                                      0.14790E+00 
c  Velocity[Z]                                      0.13973E+00 
c  Pressure     0.90976E-02     802   0.38635E-01   0.12076E+00 0.13388E+01 
c  k            0.16714E-01      10   0.20064E-03   0.79478E-04 0.29925E+02 
c  epsilon      0.45259E+02       9   0.62878E-03   0.27601E+04 0.97819E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.7278e-05                             9
a  epsilon               -0.093764                            11
a  Local Time Step      4.2278e-08                        205190


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v v  Velocity[Z]             -6.7087          5.2382       -0.065312     -0.00028628
v  ǁVelocityǁ           0.00030652          7.5027         0.70741         0.96666
v  Pressure                -4544.3          8939.2          5829.9            4925
v  k                    2.8076e-08          0.4123       0.0023169       0.0045694
v  epsilon              3.0019e-05          7563.6          5.4261          1.8497
v  TurbVisc              1.897e-13         0.11253        0.005471       0.0050547
v  CourantNb             0.0009919          705.48           4.429          1.2958
v  FourierNb              0.032686      2.3653e+05          23.005         0.48739
v  total_pressure       4.9546e+05      5.0894e+05      5.0583e+05      5.0493e+05
v  Local Time Step           0.001         0.15758       0.0014159       0.0018133


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90812      2.3724e+05          27.434          1.7831


 TIME FOR THE TIME STEP               38:        0.78586E+02

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


 INSTANT    0.390000000E+00   TIME STEP NUMBER              39
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.379625793E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442434525E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88166E+00 0.14671E+01
   Friction velocity        uet   :  0.77748E-02 0.61289E+01
   Friction velocity        uk    :  0.77724E-02 0.61289E+01
   Dimensionless distance   yplus :  0.73966E-03 0.77517E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        630
   Nb of faces within the viscous sub-layer     :      33581
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14887E+01      17   0.26012E-01   0.37614E+00 0.17906E+02 
c  Veloci-----------------------------------------------------------------------------
c  Velocity     0.14882E+01      16   0.26318E-01   0.36703E+00 0.17681E+02 
c  Velocity[X]                                      0.88647E-01 
c  Velocity[Y]                                      0.14014E+00 
c  Velocity[Z]                                      0.13824E+00 
c  Pressure     0.90150E-02     723   0.38115E-01   0.11906E+00 0.23249E+01 
c  k            0.16726E-01      10   0.14743E-03   0.75860E-04 0.29060E+02 
c  epsilon      0.45269E+02      12   0.34818E-03   0.23744E+04 0.90781E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.6358e-05                            12
a  epsilon                -0.12347                            19
a  Local Time Step      4.2278e-08                        205522


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6779          3.2834         0.26255         0.04998
v  Velocity[Y]             -4.2119          4.3067         0.15443         0.11878
v  Velocity[Z]             -6.7425          5.1933       -0.066883      -0.0002709
v  ǁVelocityǁ           0.00022723          7.5386         0.71062         0.96783
v  Pressure                -4540.3          8970.6          5852.1          4943.9
v  k                    2.8398e-08         0.41288        0.002335       0.0045905
v  epsilon              4.4394e-05          7591.1          5.5043          1.8636
v  TurbVisc             1.9056e-13         0.11253       0.0050395       0.0050129
v  CourantNb                     0          814.85          4.4439          1.2981
v  FourierNb              0.032478      2.3653e+05          22.925         0.48058
v  total_pressure       4.9546e+05      5.0897e+05      5.0585e+05      5.0494e+05
v  Local Time Step           0.001         0.15255        0.001408       0.0018197


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72656      2.3734e+05          27.369          1.7787


 TIME FOR THE TIME STEP               40:        0.93276E+02

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


 INSTANT    0.410000000E+00   TIME STEP NUMBER              41
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.204890502E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442430341E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89707E+00 0.14680E+01
   Friction velocity        uet   :  0.10235E-01 0.51607E+01
   Friction velocity        uk    :  0.10218E-01 0.51607E+01
   Dimensionless distance   yplus :  0.65851E-03 0.76871E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        638
   Nb of faces within the viscous sub-layer     :      33540
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      ------------------------------------------------------------------------------------------------
c  Velocity     0.14882E+01      16   0.26318E-01   0.36703E+00 0.17681E+02 
c  Velocity[X]                                      0.88647E-01 
c  Velocity[Y]                                      0.14014E+00 
c  Velocity[Z]                                      0.13824E+00 
c  Pressure     0.90150E-02     723   0.38115E-01   0.11906E+00 0.23249E+01 
c  k            0.16726E-01      10   0.14743E-03   0.75860E-04 0.29060E+02 
c  epsilon      0.45269E+02      12   0.34818E-03   0.23744E+04 0.90781E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.6358e-05                            12
a  epsilon                -0.12347                            19
a  Local Time Step      4.2278e-08                        205522


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6779          3.2834         0.26255         0.04998
v  Velocity[Y]             -4.2119          4.3067         0.15443         0.11878
v  Velocity[Z]             -6.7425          5.1933       -0.066883      -0.0002709
v  ǁVelocityǁ           0.00022723          7.5386         0.71062         0.96783
v  Pressure                -4540.3          8970.6          5852.1          4943.9
v  k                    2.8398e-08         0.41288        0.002335       0.0045905
v  epsilon              4.4394e-05          7591.1          5.5043          1.8636
v  TurbVisc             1.9056e-13         0.11253       0.0050395       0.0050129
v  CourantNb                     0          814.85          4.4439          1.2981
v  FourierNb              0.032478      2.3653e+05          22.925         0.48058
v  total_pressure       4.9546e+05      5.0897e+05      5.0585e+05      5.0494e+05
v  Local Time Step           0.001         0.15255        0.001408       0.0018197


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72656      2.3734e+05          27.369          1.7787


 TIME FOR THE TIME STEP               40:        0.90839E+02

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


 INSTANT    0.410000000E+00   TIME STEP NUMBER              41
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.204890502E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442430341E+00
Free inlet               13         Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442438824E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88553E+00 0.14678E+01
   Friction velocity        uet   :  0.56164E-02 0.45023E+01
   Friction velocity        uk    :  0.56069E-02 0.45023E+01
   Dimensionless distance   yplus :  0.55269E-03 0.76443E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        642
   Nb of faces within the viscous sub-layer     :      33508
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14877E+01      17   0.25662E-01   0.36420E+00 0.17516E+02 
c  Velocity[X]                                      0.87701E-01 
c  Velocity[Y]                                      0.14460E+00 
c  Velocity[Z]                                      0.13190E+00 
c  Pressure     0.98222E-02     521   0.41124E-01   0.12860E+00 0.11054E+01 
c  k            0.16749E-01       9   0.16995E-03   0.73592E-04 0.28604E+02 
c  epsilon      0.45466E+02       8   0.31476E-03   0.21866E+04 0.86642E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.2223e-05                            10
a  epsilon                -0.13284                            19
a  Local Time Step      4.2278e-08                        206218


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6937          3.2889         0.26373        0.049873
v  Velocity[Y]             -4.3351          4.3015         0.15544          0.1188
v  Velocity[Z]             -6.7138          5.2429       -0.068179     -0.00026269
v  ǁVelocityǁ           0.00027546          7.5165         0.71393         0.96896
v  Pressure                -4561.2          8981.3          5852.8          4947.3
v  k                    2.8844e-08         0.41292       0.0023511       0.0046098
v  epsilon              5.1391e-05          7598.6          5.5657          1.8763
v  TurbVisc              1.942e-13         0.11253       0.0046497        0.004976
v  CourantNb             0.0011987          1008.6            4.46          1.3004
v  FourierNb               0.03229      2.3653e+05          22.851         0.47377
v  total_pressure       4.9544e+05      5.0898e+05      5.0585e+05      5.0495e+05
v  Local Time Step           0.001         0.17297       0.0013993       0.0018211


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81007      2.3754e+05          27.311          1.7742


 TIME FOR THE TIME STEP               42:        0.87255E+02

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


 INSTANT    0.430000000E+00   TIME STEP NUMBER              43
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2 Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442438824E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88553E+00 0.14678E+01
   Friction velocity        uet   :  0.56164E-02 0.45023E+01
   Friction velocity        uk    :  0.56069E-02 0.45023E+01
   Dimensionless distance   yplus :  0.55269E-03 0.76443E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        642
   Nb of faces within the viscous sub-layer     :      33508
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14877E+01      17   0.25662E-01   0.36420E+00 0.17516E+02 
c  Velocity[X]                                      0.87701E-01 
c  Velocity[Y]                                      0.14460E+00 
c  Velocity[Z]                                      0.13190E+00 
c  Pressure     0.98222E-02     521   0.41124E-01   0.12860E+00 0.11054E+01 
c  k            0.16749E-01       9   0.16995E-03   0.73592E-04 0.28604E+02 
c  epsilon      0.45466E+02       8   0.31476E-03   0.21866E+04 0.86642E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.2223e-05                            10
a  epsilon                -0.13284                            19
a  Local Time Step      4.2278e-08                        206218


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.6937          3.2889         0.26373        0.049873
v  Velocity[Y]             -4.3351          4.3015         0.15544          0.1188
v  Velocity[Z]             -6.7138          5.2429       -0.068179     -0.00026269
v  ǁVelocityǁ           0.00027546          7.5165         0.71393         0.96896
v  Pressure                -4561.2          8981.3          5852.8          4947.3
v  k                    2.8844e-08         0.41292       0.0023511       0.0046098
v  epsilon              5.1391e-05          7598.6          5.5657          1.8763
v  TurbVisc              1.942e-13         0.11253       0.0046497        0.00497v  epsilon              4.9251e-05          7602.8          5.5477          1.8785
v  TurbVisc             1.9583e-13         0.11253       0.0044882       0.0049598
v  CourantNb             0.0015231          936.06          4.4676          1.3015
v  FourierNb               0.03221      2.3653e+05          22.821         0.47057
v  total_pressure       4.9545e+05      5.0898e+05      5.0585e+05      5.0495e+05
v  Local Time Step           0.001           0.173        0.001395       0.0018204


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88627      2.3747e+05          27.288          1.7721


 TIME FOR THE TIME STEP               43:        0.73675E+02

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


 INSTANT    0.440000000E+00   TIME STEP NUMBER              44
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.459969282E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442412080E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88914E+00 0.14664E+01
   Friction velocity        uet   :  0.41275E-02 0.46914E+01
   Friction velocity        uk    :  0.41206E-02 0.46914E+01
   Dimensionless distance   yplus :  0.30231E-03 0.75534E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        647
   Nb of faces within the viscous sub-layer     :      33467
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14872E+01      17   0.26474E-01   0.33581E+00 0.16885E+02 
c  Velocity[X]                                      0.83346E-01 
c  Velocity[Y]                                      0.12812E+00 
c  Velocity[Z]                                      0.12435E+00 
c  Pressure     0.87324E-02     687   0.36890E-01   0.11446E+00 0.16102E+01 
c  k            0.16763E-01      11   0.15078E-03   0.64437E-04 0.26224E+02 
c  epsilon      0.45555E+02       9   0.55239E-03   0.23290E+04 0.88946E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.4063e-05                            13
a  epsilon                -0.13541                            19
a  Local Time Step      4.2278e-08                        207050


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7055          3.2945         0.26489        0.049776
v  Velocity[Y]             -4.2557          4.2383         0.15639         0.11885
v  Velocity[Z]             -6.7235           5.256       -0.069325     -0.00020476
v  ǁVelocityǁ           0.00025256          7.5299         0.71751         0.97016
v v  epsilon              4.9251e-05          7602.8          5.5477          1.8785
v  TurbVisc             1.9583e-13         0.11253       0.0044882       0.0049598
v  CourantNb             0.0015231          936.06          4.4676          1.3015
v  FourierNb               0.03221      2.3653e+05          22.821         0.47057
v  total_pressure       4.9545e+05      5.0898e+05      5.0585e+05      5.0495e+05
v  Local Time Step           0.001           0.173        0.001395       0.0018204


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88627      2.3747e+05          27.288          1.7721


 TIME FOR THE TIME STEP               43:        0.82200E+02

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


 INSTANT    0.440000000E+00   TIME STEP NUMBER              44
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.459969282E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442412080E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88914E+00 0.14664E+01
   Friction velocity        uet   :  0.41275E-02 0.46914E+01
   Friction velocity        uk    :  0.41206E-02 0.46914E+01
   Dimensionless distance   yplus :  0.30231E-03 0.75534E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        647
   Nb of faces within the viscous sub-layer     :      33467
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14872E+01      17   0.26474E-01   0.33581E+00 0.16885E+02 
c  Velocity[X]                                      0.83346E-01 
c  Velocity[Y]                                      0.12812E+00 
c  Velocity[Z]                                      0.12435E+00 
c  Pressure     0.87324E-02     687   0.36890E-01   0.11446E+00 0.16102E+01 
c  k            0.1676c  Velocity[Z]                                      0.12350E+00 
c  Pressure     0.85529E-02     534   0.35496E-01   0.11182E+00 0.10968E+01 
c  k            0.16770E-01      14   0.16486E-03   0.82229E-04 0.30419E+02 
c  epsilon      0.45505E+02       9   0.46640E-03   0.32178E+04 0.10500E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.7036e-05                             9
a  epsilon               -0.070743                            12
a  Local Time Step      4.2278e-08                        207554


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7094            3.29         0.26543         0.04975
v  Velocity[Y]             -4.3584          4.1877         0.15663         0.11886
v  Velocity[Z]              -6.734          5.2691       -0.070002     -0.00018976
v  ǁVelocityǁ           0.00025898          7.5329         0.71932         0.97078
v  Pressure                -4567.2          9003.8          5865.7          4959.4
v  k                    7.4035e-09         0.41324       0.0023644       0.0046336
v  epsilon              4.2524e-05          7612.7          5.6017          1.8898
v  TurbVisc             1.9577e-13         0.11253       0.0041662       0.0049265
v  CourantNb             0.0012193          864.95          4.4872          1.3036
v  FourierNb              0.032064      2.3653e+05          22.761         0.46507
v  total_pressure       4.9543e+05        5.09e+05      5.0587e+05      5.0496e+05
v  Local Time Step           0.001         0.17305       0.0013879       0.0018231


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.86475      2.3739e+05          27.248          1.7687


 TIME FOR THE TIME STEP               45:        0.84043E+02

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


 INSTANT    0.460000000E+00   TIME STEP NUMBER              46
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.278858299E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442343035E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.90432E+00 0.14690E+01
   Friction velocity        uet   :  0.44534E-02 0.46765E+01
   Friction velocity        uk    :  0.44459E-02 0.46765E+01
   Dimensionless distance   yplus :  0.34218E-03 0.74706E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        648
   Nb of faces within the viscous sub-layer     :      33432
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14871E+01      16   0.255c  Velocity[Z]                                      0.12350E+00 
c  Pressure     0.85529E-02     534   0.35496E-01   0.11182E+00 0.10968E+01 
c  k            0.16770E-01      14   0.16486E-03   0.82229E-04 0.30419E+02 
c  epsilon      0.45505E+02       9   0.46640E-03   0.32178E+04 0.10500E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.7036e-05                             9
a  epsilon               -0.070743                            12
a  Local Time Step      4.2278e-08                        207554


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7094            3.29         0.26543         0.04975
v  Velocity[Y]             -4.3584          4.1877         0.15663         0.11886
v  Velocity[Z]              -6.734          5.2691       -0.070002     -0.00018976
v  ǁVelocityǁ           0.00025898          7.5329         0.71932         0.97078
v  Pressure                -4567.2          9003.8          5865.7          4959.4
v  k                    7.4035e-09         0.41324       0.0023644       0.0046336
v  epsilon              4.2524e-05          7612.7          5.6017          1.8898
v  TurbVisc             1.9577e-13         0.11253       0.0041662       0.0049265
v  CourantNb             0.0012193          864.95          4.4872          1.3036
v  FourierNb              0.032064      2.3653e+05          22.761         0.46507
v  total_pressure       4.9543e+05        5.09e+05      5.0587e+05      5.0496e+05
v  Local Time Step           0.001         0.17305       0.0013879       0.0018231


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.86475      2.3739e+05          27.248          1.7687


 TIME FOR THE TIME STEP               45:        0.91864E+02

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


 INSTANT    0.460000000E+00   TIME STEP NUMBER              46
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.278858299E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442343035E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
------------------------------------Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88985E+00 0.14695E+01
   Friction velocity        uet   :  0.46295E-02 0.47360E+01
   Friction velocity        uk    :  0.46276E-02 0.47360E+01
   Dimensionless distance   yplus :  0.28788E-03 0.74352E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        643
   Nb of faces within the viscous sub-layer     :      33413
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14874E+01      17   0.26521E-01   0.30519E+00 0.16115E+02 
c  Velocity[X]                                      0.77261E-01 
c  Velocity[Y]                                      0.11015E+00 
c  Velocity[Z]                                      0.11778E+00 
c  Pressure     0.83101E-02     723   0.34331E-01   0.10913E+00 0.12568E+01 
c  k            0.16781E-01       8   0.10723E-03   0.46777E-04 0.22884E+02 
c  epsilon      0.45599E+02       7   0.20024E-03   0.73482E+03 0.50187E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -1.633e-05                             7
a  epsilon               -0.074634                            13
a  Local Time Step      4.2278e-08                        208615


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7344          3.3217         0.26646        0.049714
v  Velocity[Y]             -4.3107          4.1415          0.1569         0.11893
v  Velocity[Z]             -6.7627          5.2531       -0.071342     -0.00024616
v  ǁVelocityǁ           0.00019035            7.58          0.7229         0.97218
v  Pressure                -4549.1          9050.4          5901.7          4989.5
v  k                    3.0042e-09         0.41357       0.0023649       0.0046452
v  epsilon              5.3564e-06          7626.2          5.5723          1.8944
v  TurbVisc             1.9808e-13         0.11253         0.00389        0.004897
v  CourantNb             0.0018547          766.33           4.506          1.3056
v  FourierNb              0.031951      2.3653e+05          22.708         0.46041
v  total_pressure       4.9545e+05      5.0905e+05       5.059e+05      5.0499e+05
v  Local Time Step           0.001          0.1731       0.0013813       0.0018284


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72748       2.373e+05          27.214          1.7661


 TIME FOR THE TIME STEP               47:        0.10254E+03

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


 INSTANT    0.480000000E+00   TIME STEP NUMBER              48
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.341952854E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3 Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88985E+00 0.14695E+01
   Friction velocity        uet   :  0.46295E-02 0.47360E+01
   Friction velocity        uk    :  0.46276E-02 0.47360E+01
   Dimensionless distance   yplus :  0.28788E-03 0.74352E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        643
   Nb of faces within the viscous sub-layer     :      33413
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14874E+01      17   0.26521E-01   0.30519E+00 0.16115E+02 
c  Velocity[X]                                      0.77261E-01 
c  Velocity[Y]                                      0.11015E+00 
c  Velocity[Z]                                      0.11778E+00 
c  Pressure     0.83101E-02     723   0.34331E-01   0.10913E+00 0.12568E+01 
c  k            0.16781E-01       8   0.10723E-03   0.46777E-04 0.22884E+02 
c  epsilon      0.45599E+02       7   0.20024E-03   0.73482E+03 0.50187E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -1.633e-05                             7
a  epsilon               -0.074634                            13
a  Local Time Step      4.2278e-08                        208615


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7344          3.3217         0.26646        0.049714
v  Velocity[Y]             -4.3107          4.1415          0.1569         0.11893
v  Velocity[Z]             -6.7627          5.2531       -0.071342     -0.00024616
v  ǁVelocityǁ           0.00019035            7.58          0.7229         0.97218
v  Pressure                -4549.1          9050.4          5901.7          4989.5
v  k                    3.0042e-09         0.41357       0.0023649       0.0046452
v  epsilon              5.3564e-06          7626.2          5.5723          1.8944
v  TurbVisc             1.9808e-13         0.11253         0.00389        0.004897
v  CourantNb             0.0018547          766.33           4.506          1.3056
v  FourierNb              0.031951      2.3653e+05          22.708         0.46041
v  total_pressure       4.9545e+05      5.0905e+05       5.059e+05      5.0499e+0v  FourierNb              0.031921      2.3653e+05          22.685         0.45829
v  total_pressure       4.9544e+05      5.0905e+05       5.059e+05      5.0499e+05
v  Local Time Step           0.001         0.17313       0.0013783       0.0018289


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68072      2.3741e+05          27.201           1.765


 TIME FOR THE TIME STEP               48:        0.87153E+02

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


 INSTANT    0.490000000E+00   TIME STEP NUMBER              49
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.333661976E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442394455E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89594E+00 0.14675E+01
   Friction velocity        uet   :  0.51310E-02 0.42966E+01
   Friction velocity        uk    :  0.51289E-02 0.42966E+01
   Dimensionless distance   yplus :  0.18521E-03 0.73831E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        649
   Nb of faces within the viscous sub-layer     :      33371
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14879E+01      15   0.25894E-01   0.28234E+00 0.15490E+02 
c  Velocity[X]                                      0.70803E-01 
c  Velocity[Y]                                      0.10139E+00 
c  Velocity[Z]                                      0.11015E+00 
c  Pressure     0.81018E-02     763   0.33089E-01   0.10599E+00 0.17707E+01 
c  k            0.16788E-01      11   0.11098E-03   0.54874E-04 0.24863E+02 
c  epsilon      0.45671E+02       8   0.48445E-03   0.22810E+04 0.88126E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.7326e-05                            10
a  epsilon               -0.077834                            18
a  Local Time Step      4.2278e-08                        209588


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7544          3.3159         0.26738        0.049627
v  Velocity[Y]             -4.3467          4.1647         0.15667         0.11897
v  Velocity[Z]             -6.7548          5.2306       -0.072775     -0.00026056
v  ǁVelocityǁ           0.00023251          7.5745         0.72648         0.97366
v  Pressure                -4547.8          9069.9          5914.2          5000.8
v  k                    2.9132e-08         0.41262       0.0023759       0.0046557
v  epsilon              6.6095e-05          7602.6          5.6709          1.9007
v v  FourierNb              0.031921      2.3653e+05          22.685         0.45829
v  total_pressure       4.9544e+05      5.0905e+05       5.059e+05      5.0499e+05
v  Local Time Step           0.001         0.17313       0.0013783       0.0018289


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68072      2.3741e+05          27.201           1.765


 TIME FOR THE TIME STEP               48:        0.84751E+02

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


 INSTANT    0.490000000E+00   TIME STEP NUMBER              49
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.333661976E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442394455E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89594E+00 0.14675E+01
   Friction velocity        uet   :  0.51310E-02 0.42966E+01
   Friction velocity        uk    :  0.51289E-02 0.42966E+01
   Dimensionless distance   yplus :  0.18521E-03 0.73831E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        649
   Nb of faces within the viscous sub-layer     :      33371
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14879E+01      15   0.25894E-01   0.28234E+00 0.15490E+02 
c  Velocity[X]                                      0.70803E-01 
c  Velocity[Y]                                      0.10139E+00 
c  Velocity[Z]                                      0.11015E+00 
c  Pressure     0.81018E-02     763   0.33089E-01   0.10599E+00 0.17707E+01 
c  k            0.16788E-01      11   0.11098E-03   0.54874E-04 0.24863E+02 
c  epsilon      0.45671E+02       8   0.48445E-03   0.22810E+04 0.88126E+02 
-----------------------------------------------------------------------------
  
  

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

   field-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.2075e-05                            10
a  epsilon               -0.080969                            18
a  Local Time Step      4.2278e-08                        210199


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7619          3.3286         0.26782        0.049593
v  Velocity[Y]             -4.2706           4.168         0.15643         0.11899
v  Velocity[Z]             -6.7556          5.2337       -0.073548     -0.00030467
v  ǁVelocityǁ           0.00024665          7.5808         0.72827         0.97438
v  Pressure                  -4555          9079.1          5913.7          5001.2
v  k                    1.9064e-08         0.41353        0.002384        0.004661
v  epsilon               8.808e-05          7635.8          5.7412          1.9056
v  TurbVisc             1.9712e-13         0.11253       0.0035299       0.0048569
v  CourantNb             0.0006912          836.66          4.5323          1.3087
v  FourierNb              0.031936      2.3653e+05           22.64         0.45406
v  total_pressure       4.9544e+05      5.0908e+05      5.0591e+05        5.05e+05
v  Local Time Step           0.001         0.17318       0.0013719       0.0018323


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78362      2.3737e+05          27.173          1.7628


 TIME FOR THE TIME STEP               50:        0.73435E+02

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


 INSTANT    0.510000000E+00   TIME STEP NUMBER              51
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.165712159E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442479869E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.90150E+00 0.14697E+01
   Friction velocity        uet   :  0.49070E-02 0.44773E+01
   Friction velocity        uk    :  0.49719E-02 0.44773E+01
   Dimensionless distance   yplus :  0.57131E-03 0.73544E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        656
   Nb of faces within the viscous sub-layer     :      33319
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14890E+01      16   0.25717E-01   0.26903E+00 0.15129E+02 
c  Velocity[X]                                      0.70340E-01 
c  Velocity[Y]                                      0.93974E-01 
c  Velocity[Z]                                      0.10471E+00 
c  Pressure     0.77793E-02     365   0.31435E-01   0.10176E+00 0.7-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.2075e-05                            10
a  epsilon               -0.080969                            18
a  Local Time Step      4.2278e-08                        210199


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7619          3.3286         0.26782        0.049593
v  Velocity[Y]             -4.2706           4.168         0.15643         0.11899
v  Velocity[Z]             -6.7556          5.2337       -0.073548     -0.00030467
v  ǁVelocityǁ           0.00024665          7.5808         0.72827         0.97438
v  Pressure                  -4555          9079.1          5913.7          5001.2
v  k                    1.9064e-08         0.41353        0.002384        0.004661
v  epsilon               8.808e-05          7635.8          5.7412          1.9056
v  TurbVisc             1.9712e-13         0.11253       0.0035299       0.0048569
v  CourantNb             0.0006912          836.66          4.5323          1.3087
v  FourierNb              0.031936      2.3653e+05           22.64         0.45406
v  total_pressure       4.9544e+05      5.0908e+05      5.0591e+05        5.05e+05
v  Local Time Step           0.001         0.17318       0.0013719       0.0018323


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78362      2.3737e+05          27.173          1.7628


 TIME FOR THE TIME STEP               50:        0.71269E+02

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


 INSTANT    0.510000000E+00   TIME STEP NUMBER              51
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.165712159E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442479869E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88664E+00 0.14693E+01
   Friction velocity        uet   :  0.85978E-02 0.38092E+01
   Friction velocity        uk    :  0.85814E-02 0.38092E+01
   Dimensionless distance   yplus :  0.48606E-03 0.73502E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        656
   Nb of faces within the viscous sub-layer     :      33300
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14895E+01      16   0.25720E-01   0.26136E+00 0.14930E+02 
c  Velocity[X]                                      0.65818E-01 
c  Velocity[Y]                                      0.92519E-01 
c  Velocity[Z]                                      0.10303E+00 
c  Pressure     0.76893E-02     416   0.31072E-01   0.10031E+00 0.78390E+00 
c  k            0.16807E-01      10   0.13644E-03   0.47842E-04 0.23267E+02 
c  epsilon      0.45811E+02       9   0.54032E-03   0.24806E+04 0.91388E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.9753e-05                             8
a  epsilon               -0.087273                            16
a  Local Time Step      4.2278e-08                        211238


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7728          3.3468          0.2687        0.049501
v  Velocity[Y]             -4.3095          4.1813         0.15577         0.11901
v  Velocity[Z]             -6.7544          5.2099        -0.07503     -0.00041592
v  ǁVelocityǁ           0.00013141          7.5887         0.73192         0.97588
v  Pressure                -4547.7          9097.1          5910.5          5002.9
v  k                    4.5773e-09         0.41369       0.0023969       0.0046717
v  epsilon              7.8894e-05          7644.6          5.7717           1.915
v  TurbVisc             1.9336e-13         0.11253       0.0032877       0.0048319
v  CourantNb              0.001055          966.01          4.5511          1.3108
v  FourierNb               0.03204      2.3653e+05          22.594         0.44978
v  total_pressure       4.9545e+05       5.091e+05      5.0591e+05        5.05e+05
v  Local Time Step           0.001         0.17321       0.0013652       0.0018326


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0072       2.375e+05          27.145          1.7606


 TIME FOR THE TIME STEP               52:        0.63996E+02

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


 INSTANT    0.530000000E+00   TIME STEP NUMBER              53
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.276065512E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442575027E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.00------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88664E+00 0.14693E+01
   Friction velocity        uet   :  0.85978E-02 0.38092E+01
   Friction velocity        uk    :  0.85814E-02 0.38092E+01
   Dimensionless distance   yplus :  0.48606E-03 0.73502E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        656
   Nb of faces within the viscous sub-layer     :      33300
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14895E+01      16   0.25720E-01   0.26136E+00 0.14930E+02 
c  Velocity[X]                                      0.65818E-01 
c  Velocity[Y]                                      0.92519E-01 
c  Velocity[Z]                                      0.10303E+00 
c  Pressure     0.76893E-02     416   0.31072E-01   0.10031E+00 0.78390E+00 
c  k            0.16807E-01      10   0.13644E-03   0.47842E-04 0.23267E+02 
c  epsilon      0.45811E+02       9   0.54032E-03   0.24806E+04 0.91388E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.9753e-05                             8
a  epsilon               -0.087273                            16
a  Local Time Step      4.2278e-08                        211238


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7728          3.3468          0.2687        0.049501
v  Velocity[Y]             -4.3095          4.1813         0.15577         0.11901
v  Velocity[Z]             -6.7544          5.2099        -0.07503     -0.00041592
v  ǁVelocityǁ           0.00013141          7.5887         0.73192         0.97588
v  Pressure                -4547.7          9097.1          5910.5          5002.9
v  k                    4.5773e-09         0.41369       0.0023969       0.0046717
v  epsilon              7.8894e-05          7644.6          5.7717           1.915
v  TurbVisc             1.9336e-13         0.11253       0.0032877       0.0048319
v  CourantNb              0.001055          966.01          4.5511          1.3108
v  FourierNb               0.03204      2.3653e+05          22.594         0.44978
v  total_pressure       4.9545e+05       5.091e+05      5.0591e+05        5.05e+05
v  Local Time Step           0.001         0.17321       0.0013652       0.0018326


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  ------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99515      2.3715e+05          27.132          1.7596


 TIME FOR THE TIME STEP               53:        0.91168E+02

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


 INSTANT    0.540000000E+00   TIME STEP NUMBER              54
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.467276480E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442547595E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87136E+00 0.14702E+01
   Friction velocity        uet   :  0.96647E-02 0.50286E+01
   Friction velocity        uk    :  0.96605E-02 0.50286E+01
   Dimensionless distance   yplus :  0.11375E-03 0.73662E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        663
   Nb of faces within the viscous sub-layer     :      33282
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14905E+01      17   0.25418E-01   0.24877E+00 0.14555E+02 
c  Velocity[X]                                      0.61056E-01 
c  Velocity[Y]                                      0.88564E-01 
c  Velocity[Z]                                      0.99148E-01 
c  Pressure     0.75962E-02     321   0.30787E-01   0.99192E-01 0.70377E+00 
c  k            0.16815E-01      10   0.10729E-03   0.56248E-04 0.25159E+02 
c  epsilon      0.45969E+02       8   0.33265E-03   0.18161E+04 0.77828E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.4886e-05                            10
a  epsilon               -0.071531                            18
a  Local Time Step      4.2278e-08                        212269


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7816          3.3498         0.26938        0.049457
v  Velocity[Y]             -4.1431          4.2159         0.15495         0.11904
v  Velocity[Z]             -6.7197           5.241       -0.076518     -0.00039324
v  ǁVelocityǁ           7.4907e-05          7.5604         0.73549         0.97718
v  Pressure                -4542.6          9092.2          5890.3          4988.1
v  k                     2.897e-08         0.41432       0.0024089       0.0046796
v  epsilon              6.8975e-05          7669.3          5.8607          1.9201
v  TurbVisc             1.9774e-13          1.9697       0.0031006       0.0048143
v  CourantNb             0.0009897          811.81           4.569          1.3129
v  FourierNb              0.032109      2.3653e+05          22.556          0.4458
v  total_pressure       4.9546e+05      5.0909e+05      5.0589e+
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99515      2.3715e+05          27.132          1.7596


 TIME FOR THE TIME STEP               53:        0.86700E+02

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


 INSTANT    0.540000000E+00   TIME STEP NUMBER              54
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.467276480E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442547595E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87136E+00 0.14702E+01
   Friction velocity        uet   :  0.96647E-02 0.50286E+01
   Friction velocity        uk    :  0.96605E-02 0.50286E+01
   Dimensionless distance   yplus :  0.11375E-03 0.73662E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        663
   Nb of faces within the viscous sub-layer     :      33282
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14905E+01      17   0.25418E-01   0.24877E+00 0.14555E+02 
c  Velocity[X]                                      0.61056E-01 
c  Velocity[Y]                                      0.88564E-01 
c  Velocity[Z]                                      0.99148E-01 
c  Pressure     0.75962E-02     321   0.30787E-01   0.99192E-01 0.70377E+00 
c  k            0.16815E-01      10   0.10729E-03   0.56248E-04 0.25159E+02 
c  epsilon      0.45969E+02       8   0.33265E-03   0.18161E+04 0.77828E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.4886e-05                            10
a  epsilon               -0.071531                            18
a  Local Time Step      4.2278e-08a  k                   -2.0644e-05                            10
a  epsilon               -0.057536                            13
a  Local Time Step      4.2278e-08                        212729


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7921          3.3405         0.26975        0.049453
v  Velocity[Y]             -4.3425          4.2345         0.15454         0.11904
v  Velocity[Z]             -6.7068           5.234       -0.077222     -0.00036788
v  ǁVelocityǁ           5.8133e-05           7.545         0.73729         0.97777
v  Pressure                -4534.6          9100.1          5888.4          4988.3
v  k                    2.9019e-08         0.41364       0.0024114       0.0046835
v  epsilon              6.5485e-05          7645.5          5.8506          1.9238
v  TurbVisc             1.9556e-13         0.11253       0.0030055       0.0047988
v  CourantNb            0.00050692          606.23          4.5778          1.3139
v  FourierNb              0.032171      2.3653e+05          22.538         0.44384
v  total_pressure       4.9547e+05       5.091e+05      5.0589e+05      5.0499e+05
v  Local Time Step           0.001         0.17324        0.001355       0.0018298


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85662      2.3714e+05          27.116          1.7578


 TIME FOR THE TIME STEP               55:        0.80289E+02

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


 INSTANT    0.560000000E+00   TIME STEP NUMBER              56
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.373608914E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442535248E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.86639E+00 0.14684E+01
   Friction velocity        uet   :  0.51872E-02 0.37135E+01
   Friction velocity        uk    :  0.51867E-02 0.37135E+01
   Dimensionless distance   yplus :  0.44903E-03 0.73980E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        666
   Nb of faces within the viscous sub-layer     :      33271
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14912E+01      16   0.25381E-01   0.24427E+00 0.14429E+02 
c  Velocity[X]                                      0.58455E-01 
c  Velocity[Y]                                      0.88984E-01 
c  Velocity[Z]                                      0.96833E-01 
c  Pressure     0.74760E-02     329   0.29996E-01   0.97453E-01 0.67311E+00 
c  k            0.16824E-01       9   0.11870E-03   0.56486E-04 0.25190E+02 
c  epsilon      0.46020E+02       8   0.28221E-03   0.15268E+04 0.71252E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -------------------------a  k                   -2.0644e-05                            10
a  epsilon               -0.057536                            13
a  Local Time Step      4.2278e-08                        212729


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7921          3.3405         0.26975        0.049453
v  Velocity[Y]             -4.3425          4.2345         0.15454         0.11904
v  Velocity[Z]             -6.7068           5.234       -0.077222     -0.00036788
v  ǁVelocityǁ           5.8133e-05           7.545         0.73729         0.97777
v  Pressure                -4534.6          9100.1          5888.4          4988.3
v  k                    2.9019e-08         0.41364       0.0024114       0.0046835
v  epsilon              6.5485e-05          7645.5          5.8506          1.9238
v  TurbVisc             1.9556e-13         0.11253       0.0030055       0.0047988
v  CourantNb            0.00050692          606.23          4.5778          1.3139
v  FourierNb              0.032171      2.3653e+05          22.538         0.44384
v  total_pressure       4.9547e+05       5.091e+05      5.0589e+05      5.0499e+05
v  Local Time Step           0.001         0.17324        0.001355       0.0018298


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85662      2.3714e+05          27.116          1.7578


 TIME FOR THE TIME STEP               55:        0.76906E+02

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


 INSTANT    0.560000000E+00   TIME STEP NUMBER              56
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.373608914E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442535248E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.86639E+00 0.14684E+01
   Friction velocity        uet   :  0.51872E-02 0.37135E+01
   Friction velocity        uk    :  0.51867E-02 0.37135E+01
   Dimensionless distance   yplus :  0.44903E-03 0.73980E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   Dimensionless distance   yplus :  0.21774E-03 0.74177E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        664
   Nb of faces within the viscous sub-layer     :      33255
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14914E+01      16   0.25823E-01   0.23928E+00 0.14274E+02 
c  Velocity[X]                                      0.60153E-01 
c  Velocity[Y]                                      0.87168E-01 
c  Velocity[Z]                                      0.91961E-01 
c  Pressure     0.74092E-02     488   0.29832E-01   0.96462E-01 0.70619E+00 
c  k            0.16827E-01      11   0.11716E-03   0.43252E-04 0.22073E+02 
c  epsilon      0.46090E+02       9   0.27383E-03   0.11200E+04 0.61034E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.8332e-05                            10
a  epsilon               -0.044966                            13
a  Local Time Step      4.2278e-08                        213690


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7997          3.3446         0.27045        0.049447
v  Velocity[Y]             -4.1452          4.2499         0.15372         0.11902
v  Velocity[Z]             -6.6802          5.2203       -0.078513     -0.00036301
v  ǁVelocityǁ           5.4966e-05          7.4895         0.74076         0.97893
v  Pressure                  -4506          9112.3          5887.1          4989.4
v  k                    2.9809e-08         0.41378       0.0024178       0.0046898
v  epsilon              6.0074e-05          7651.4          5.8592          1.9268
v  TurbVisc             1.9957e-13         0.11253        0.002838       0.0047759
v  CourantNb            0.00070539          814.19          4.5951          1.3159
v  FourierNb              0.032328      2.3653e+05          22.506         0.43984
v  total_pressure       4.9549e+05      5.0911e+05      5.0589e+05      5.0499e+05
v  Local Time Step           0.001         0.17325        0.001348       0.0018246


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0323      2.3734e+05          27.101          1.7558


 TIME FOR THE TIME STEP               57:        0.80110E+02

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


 INSTANT    0.580000000E+00   TIME STEP NUMBER              58
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.306643125E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442501405E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at    Dimensionless distance   yplus :  0.21774E-03 0.74177E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        664
   Nb of faces within the viscous sub-layer     :      33255
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14914E+01      16   0.25823E-01   0.23928E+00 0.14274E+02 
c  Velocity[X]                                      0.60153E-01 
c  Velocity[Y]                                      0.87168E-01 
c  Velocity[Z]                                      0.91961E-01 
c  Pressure     0.74092E-02     488   0.29832E-01   0.96462E-01 0.70619E+00 
c  k            0.16827E-01      11   0.11716E-03   0.43252E-04 0.22073E+02 
c  epsilon      0.46090E+02       9   0.27383E-03   0.11200E+04 0.61034E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.8332e-05                            10
a  epsilon               -0.044966                            13
a  Local Time Step      4.2278e-08                        213690


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7997          3.3446         0.27045        0.049447
v  Velocity[Y]             -4.1452          4.2499         0.15372         0.11902
v  Velocity[Z]             -6.6802          5.2203       -0.078513     -0.00036301
v  ǁVelocityǁ           5.4966e-05          7.4895         0.74076         0.97893
v  Pressure                  -4506          9112.3          5887.1          4989.4
v  k                    2.9809e-08         0.41378       0.0024178       0.0046898
v  epsilon              6.0074e-05          7651.4          5.8592          1.9268
v  TurbVisc             1.9957e-13         0.11253        0.002838       0.0047759
v  CourantNb            0.00070539          814.19          4.5951          1.3159
v  FourierNb              0.032328      2.3653e+05          22.506         0.43984
v  total_pressure       4.9549e+05      5.0911e+05      5.0589e+05      5.0499e+05
v  Local Time Step           0.001         0.17325        0.001348       0.0018246


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0323      2.3734e+05          27.101          1.7558


 TIME FOR THE TIME STEP               57:        0.80914E+02

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


 INSTANT    0.580000000E+00   TIME STEP NUMBER              58
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMAT INSTANT    0.590000000E+00   TIME STEP NUMBER              59
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.415956249E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442529486E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.79414E+00 0.14718E+01
   Friction velocity        uet   :  0.60173E-02 0.42102E+01
   Friction velocity        uk    :  0.60168E-02 0.42102E+01
   Dimensionless distance   yplus :  0.44237E-03 0.74521E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        666
   Nb of faces within the viscous sub-layer     :      33234
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14919E+01      20   0.25233E-01   0.23441E+00 0.14129E+02 
c  Velocity[X]                                      0.54750E-01 
c  Velocity[Y]                                      0.86253E-01 
c  Velocity[Z]                                      0.93404E-01 
c  Pressure     0.75834E-02     424   0.30548E-01   0.98791E-01 0.67075E+00 
c  k            0.16839E-01      10   0.11395E-03   0.54507E-04 0.24802E+02 
c  epsilon      0.46231E+02       8   0.30018E-03   0.33311E+04 0.10499E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.2481e-06                             8
a  epsilon               -0.044393                             9
a  Local Time Step      4.2278e-08                        214572


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8127          3.3438         0.27092        0.049434
v  Velocity[Y]             -4.1442          4.2533          0.1528         0.11903
v  Velocity[Z]             -6.6934          5.2265       -0.079802     -0.00044695
v  ǁVelocityǁ           0.00022397          7.4853         0.74392         0.98008
v  Pressure                -4464.8          9120.7          5886.1          4990.4
v  k                    1.2529e-08          0.4142        0.002429        0.004697
v  epsilon              5.7344e-05          7668.7           5.886          1.9333
v  TurbVisc             1.9752e-13         0.11253       0.0026446       0.0047542
v  CourantNb            0.00062111          799.65          4.6126          1.3179
v  FourierNb              0.032577      2.3653e+05          22.467         0.43611
v  total_pressure       4.9554e+05      5.0912e+05      5.0589e+05      5.0499e+05
v  Local Time Step           0.001         0.17326       0.0013412       0.0018206


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0103      2.3733e+0 INSTANT    0.590000000E+00   TIME STEP NUMBER              59
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.415956249E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442529486E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.79414E+00 0.14718E+01
   Friction velocity        uet   :  0.60173E-02 0.42102E+01
   Friction velocity        uk    :  0.60168E-02 0.42102E+01
   Dimensionless distance   yplus :  0.44237E-03 0.74521E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        666
   Nb of faces within the viscous sub-layer     :      33234
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14919E+01      20   0.25233E-01   0.23441E+00 0.14129E+02 
c  Velocity[X]                                      0.54750E-01 
c  Velocity[Y]                                      0.86253E-01 
c  Velocity[Z]                                      0.93404E-01 
c  Pressure     0.75834E-02     424   0.30548E-01   0.98791E-01 0.67075E+00 
c  k            0.16839E-01      10   0.11395E-03   0.54507E-04 0.24802E+02 
c  epsilon      0.46231E+02       8   0.30018E-03   0.33311E+04 0.10499E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.2481e-06                             8
a  epsilon               -0.044393                             9
a  Local Time Step      4.2278e-08                        214572


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8127          3.3438         0.27092        0.04943-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8201          3.3456         0.27109        0.049435
v  Velocity[Y]             -4.1257          4.2557         0.15242         0.11902
v  Velocity[Z]             -6.6606          5.3493       -0.080429     -0.00050958
v  ǁVelocityǁ           3.4933e-05          7.4735         0.74538         0.98062
v  Pressure                -4449.8          9122.7          5883.6          4989.9
v  k                    2.9637e-08         0.41326        0.002441       0.0047014
v  epsilon              4.3139e-05          7649.4          5.9458          1.9381
v  TurbVisc             1.9777e-13         0.11253       0.0025715       0.0047445
v  CourantNb               0.00117           468.9          4.6187          1.3188
v  FourierNb              0.032664      2.3653e+05          22.452         0.43434
v  total_pressure       4.9555e+05      5.0912e+05      5.0588e+05      5.0499e+05
v  Local Time Step           0.001         0.17326       0.0013376       0.0018189


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88981        2.37e+05          27.071          1.7531


 TIME FOR THE TIME STEP               60:        0.93515E+02

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


 INSTANT    0.610000000E+00   TIME STEP NUMBER              61
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.420770680E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442638534E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.81498E+00 0.14700E+01
   Friction velocity        uet   :  0.78612E-02 0.40197E+01
   Friction velocity        uk    :  0.78603E-02 0.40197E+01
   Dimensionless distance   yplus :  0.44688E-03 0.74805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        669
   Nb of faces within the viscous sub-layer     :      33203
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14926E+01      16   0.25490E-01   0.22568E+00 0.13835E+02 
c  Velocity[X]                                      0.55220E-01 
c  Velocity[Y]                                      0.83978E-01 
c  Velocity[Z]                                      0.86483E-01 
c  Pressure     0.75250E-02     780   0.30138E-01   0.97581E-01 0.29269E+01 
c  k            0.16847E-01      10   0.14045E-03   0.67429E-04 0.27484E+02 
c  epsilon      0.46380E+02       9   0.28429E-03   0.21848E+04 0.84752E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012759                            10
a  epsilon                -0.24934                            15
a  Local Time Step      4.2278e-08             -  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8201          3.3456         0.27109        0.049435
v  Velocity[Y]             -4.1257          4.2557         0.15242         0.11902
v  Velocity[Z]             -6.6606          5.3493       -0.080429     -0.00050958
v  ǁVelocityǁ           3.4933e-05          7.4735         0.74538         0.98062
v  Pressure                -4449.8          9122.7          5883.6          4989.9
v  k                    2.9637e-08         0.41326        0.002441       0.0047014
v  epsilon              4.3139e-05          7649.4          5.9458          1.9381
v  TurbVisc             1.9777e-13         0.11253       0.0025715       0.0047445
v  CourantNb               0.00117           468.9          4.6187          1.3188
v  FourierNb              0.032664      2.3653e+05          22.452         0.43434
v  total_pressure       4.9555e+05      5.0912e+05      5.0588e+05      5.0499e+05
v  Local Time Step           0.001         0.17326       0.0013376       0.0018189


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88981        2.37e+05          27.071          1.7531


 TIME FOR THE TIME STEP               60:        0.10073E+03

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


 INSTANT    0.610000000E+00   TIME STEP NUMBER              61
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.420770680E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442638534E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.81498E+00 0.14700E+01
   Friction velocity        uet   :  0.78612E-02 0.40197E+01
   Friction velocity        uk    :  0.78603E-02 0.40197E+01
   Dimensionless distance   yplus :  0.44688E-03 0.74805E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        669
   Nb of faces within the viscous sub-layer     :      33203
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14925E+01      16   0.25477E-01   0.22675E+00 0.13860E+02 
c  Velocity[X]                                      0.56672E-01 
c  Velocity[Y]                                      0.81578E-01 
c  Velocity[Z]                                      0.88501E-01 
c  Pressure     0.75763E-02     946   0.30358E-01   0.97978E-01 0.28351E+01 
c  k            0.16849E-01       9   0.11161E-03   0.51060E-04 0.23846E+02 
c  epsilon      0.46303E+02       8   0.27250E-03   0.11624E+04 0.61797E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.2558e-05                             8
a  epsilon                -0.07043                            12
a  Local Time Step      4.2278e-08                        215735


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.824          3.3287         0.27126        0.049419
v  Velocity[Y]             -4.0147          4.2506         0.15171         0.11906
v  Velocity[Z]             -6.6618          5.3297       -0.081452     -0.00045655
v  ǁVelocityǁ            5.832e-05          7.4508         0.74796         0.98148
v  Pressure                -4477.3            9069          5831.3          4948.8
v  k                    3.0786e-08         0.41383         0.00245       0.0047074
v  epsilon              4.1867e-06          7659.4          5.9577          1.9412
v  TurbVisc             2.0481e-13         0.11253       0.0024238       0.0047247
v  CourantNb            0.00029858          742.09          4.6343          1.3205
v  FourierNb              0.032911      2.3653e+05          22.422         0.43126
v  total_pressure       4.9552e+05      5.0907e+05      5.0583e+05      5.0495e+05
v  Local Time Step           0.001         0.17326       0.0013311       0.0018183


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83723      2.3727e+05          27.056          1.7518


 TIME FOR THE TIME STEP               62:        0.10759E+03

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


 INSTANT    0.630000000E+00   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.341542519E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442506476E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80691E+00 0.14692E+01
   Friction velocity        uet   :  0.83286E-02 0.36608E+01
   Friction velocity        uk    :  0.83138E-02 0.36608E+01
   Dimensionless distance   yplus :  0.17942E-03 0.75010E+01
   ------------------------------------------------------
   Nb of reversal o------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14925E+01      16   0.25477E-01   0.22675E+00 0.13860E+02 
c  Velocity[X]                                      0.56672E-01 
c  Velocity[Y]                                      0.81578E-01 
c  Velocity[Z]                                      0.88501E-01 
c  Pressure     0.75763E-02     946   0.30358E-01   0.97978E-01 0.28351E+01 
c  k            0.16849E-01       9   0.11161E-03   0.51060E-04 0.23846E+02 
c  epsilon      0.46303E+02       8   0.27250E-03   0.11624E+04 0.61797E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.2558e-05                             8
a  epsilon                -0.07043                            12
a  Local Time Step      4.2278e-08                        215735


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -1.824          3.3287         0.27126        0.049419
v  Velocity[Y]             -4.0147          4.2506         0.15171         0.11906
v  Velocity[Z]             -6.6618          5.3297       -0.081452     -0.00045655
v  ǁVelocityǁ            5.832e-05          7.4508         0.74796         0.98148
v  Pressure                -4477.3            9069          5831.3          4948.8
v  k                    3.0786e-08         0.41383         0.00245       0.0047074
v  epsilon              4.1867e-06          7659.4          5.9577          1.9412
v  TurbVisc             2.0481e-13         0.11253       0.0024238       0.0047247
v  CourantNb            0.00029858          742.09          4.6343          1.3205
v  FourierNb              0.032911      2.3653e+05          22.422         0.43126
v  total_pressure       4.9552e+05      5.0907e+05      5.0583e+05      5.0495e+05
v  Local Time Step           0.001         0.17326       0.0013311       0.0018183


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83723      2.3727e+05          27.056          1.7518


 TIME FOR THE TIME STEP               62:        0.11417E+03

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


 INSTANT    0.630000000E+00   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46 Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.256977214E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442535900E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.79882E+00 0.14665E+01
   Friction velocity        uet   :  0.31163E-02 0.31684E+01
   Friction velocity        uk    :  0.31154E-02 0.31684E+01
   Dimensionless distance   yplus :  0.32015E-03 0.75024E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        672
   Nb of faces within the viscous sub-layer     :      33179
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14925E+01      15   0.26240E-01   0.22022E+00 0.13638E+02 
c  Velocity[X]                                      0.57075E-01 
c  Velocity[Y]                                      0.75729E-01 
c  Velocity[Z]                                      0.87412E-01 
c  Pressure     0.75544E-02     375   0.29548E-01   0.97138E-01 0.62634E+00 
c  k            0.16850E-01       9   0.93698E-04   0.38703E-04 0.20830E+02 
c  epsilon      0.46188E+02       7   0.25272E-03   0.10563E+04 0.58992E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.4619e-06                             9
a  epsilon               -0.053933                            13
a  Local Time Step      4.2278e-08                        216481


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8354          3.3378         0.27141        0.049423
v  Velocity[Y]             -4.2784          4.2671         0.15104         0.11907
v  Velocity[Z]             -6.6511          5.4877       -0.082511     -0.00043312
v  ǁVelocityǁ           1.8995e-05          7.4459         0.75035         0.98227
v  Pressure                -4456.6          9072.2            5831          4950.2
v  k                    3.1838e-08         0.41204       0.0024567       0.0047121
v  epsilon              5.6778e-05          7609.2          5.9538          1.9429
v  TurbVisc             2.2069e-13         0.11253       0.0022982       0.0047069
v  CourantNb            0.00030906          588.85          4.6429           1.322
v  FourierNb              0.033014      2.3653e+05          22.395         0.42828
v  total_pressure       4.9554e+05      5.0907e+05      5.0583e+05      5.0495e+05
v  Local Time Step           0.001         0.17326       0.0013247       0.0018182


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0303      2.3712e+05          27.038          1.7503


 TIME FOR THE TIME STEP               64:        0.75077E+02

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


 INSTANT    0.650000000E+00   TIME STEP NUMBER              65
 ==========================================Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.256977214E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442535900E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.79882E+00 0.14665E+01
   Friction velocity        uet   :  0.31163E-02 0.31684E+01
   Friction velocity        uk    :  0.31154E-02 0.31684E+01
   Dimensionless distance   yplus :  0.32015E-03 0.75024E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        672
   Nb of faces within the viscous sub-layer     :      33179
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14925E+01      15   0.26240E-01   0.22022E+00 0.13638E+02 
c  Velocity[X]                                      0.57075E-01 
c  Velocity[Y]                                      0.75729E-01 
c  Velocity[Z]                                      0.87412E-01 
c  Pressure     0.75544E-02     375   0.29548E-01   0.97138E-01 0.62634E+00 
c  k            0.16850E-01       9   0.93698E-04   0.38703E-04 0.20830E+02 
c  epsilon      0.46188E+02       7   0.25272E-03   0.10563E+04 0.58992E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.4619e-06                             9
a  epsilon               -0.053933                            13
a  Local Time Step      4.2278e-08                        216481


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8354          3.3378         0.27141        0.049423
v  Velocity[Y]             -4.2784          4.2671         0.15104         0.11907
v  Velocity[Z]             -6.6511          5.4877       -0.082511     -0.00043312
v  ǁVelocityǁ           1.8995e-05          7.4459         0.75035         0.98v  Velocity[Z]             -6.6628          5.5876       -0.082949     -0.00043798
v  ǁVelocityǁ           5.4033e-05          7.3969         0.75149         0.98267
v  Pressure                -4459.6          9071.6          5830.9          4950.7
v  k                    3.0932e-08         0.41339       0.0024581       0.0047149
v  epsilon              5.8034e-05          7641.3          5.9219          1.9444
v  TurbVisc             2.2671e-13         0.11253       0.0022415       0.0046982
v  CourantNb            0.00010278          739.38          4.6484          1.3228
v  FourierNb              0.033017      2.3653e+05          22.383         0.42689
v  total_pressure       4.9554e+05      5.0907e+05      5.0583e+05      5.0495e+05
v  Local Time Step           0.001         0.17326       0.0013215       0.0018178


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9739      2.3727e+05          27.032          1.7496


 TIME FOR THE TIME STEP               65:        0.85203E+02

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


 INSTANT    0.660000000E+00   TIME STEP NUMBER              66
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.390242324E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442551067E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80442E+00 0.14661E+01
   Friction velocity        uet   :  0.57231E-02 0.60803E+01
   Friction velocity        uk    :  0.57226E-02 0.60803E+01
   Dimensionless distance   yplus :  0.33999E-03 0.75218E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        660
   Nb of faces within the viscous sub-layer     :      33164
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14928E+01      15   0.25173E-01   0.22334E+00 0.13725E+02 
c  Velocity[X]                                      0.55512E-01 
c  Velocity[Y]                                      0.78278E-01 
c  Velocity[Z]                                      0.89550E-01 
c  Pressure     0.76903E-02     432   0.30404E-01   0.99487E-01 0.66443E+00 
c  k            0.16853E-01       8   0.10031E-03   0.37639E-04 0.20536E+02 
c  epsilon      0.46187E+02       7   0.26664E-03   0.13447E+04 0.66621E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.4899e-05                             9
a  epsilon               -0.052424                            16
a  Local Time Step      4.2278e-08                        217132


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v v  Velocity[Z]             -6.6628          5.5876       -0.082949     -0.00043798
v  ǁVelocityǁ           5.4033e-05          7.3969         0.75149         0.98267
v  Pressure                -4459.6          9071.6          5830.9          4950.7
v  k                    3.0932e-08         0.41339       0.0024581       0.0047149
v  epsilon              5.8034e-05          7641.3          5.9219          1.9444
v  TurbVisc             2.2671e-13         0.11253       0.0022415       0.0046982
v  CourantNb            0.00010278          739.38          4.6484          1.3228
v  FourierNb              0.033017      2.3653e+05          22.383         0.42689
v  total_pressure       4.9554e+05      5.0907e+05      5.0583e+05      5.0495e+05
v  Local Time Step           0.001         0.17326       0.0013215       0.0018178


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9739      2.3727e+05          27.032          1.7496


 TIME FOR THE TIME STEP               65:        0.84744E+02

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


 INSTANT    0.660000000E+00   TIME STEP NUMBER              66
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.390242324E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442551067E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80442E+00 0.14661E+01
   Friction velocity        uet   :  0.57231E-02 0.60803E+01
   Friction velocity        uk    :  0.57226E-02 0.60803E+01
   Dimensionless distance   yplus :  0.33999E-03 0.75218E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        660
   Nb of faces within the viscous sub-layer     :      33164
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14928E+01      15   0.25173E-01   0.22334E+00 0.13725E+02 
c  Veloci-----------------------------------------------------------------------------
c  Velocity     0.14930E+01      17   0.26063E-01   0.21330E+00 0.13415E+02 
c  Velocity[X]                                      0.53300E-01 
c  Velocity[Y]                                      0.75459E-01 
c  Velocity[Z]                                      0.84542E-01 
c  Pressure     0.78216E-02     397   0.30453E-01   0.10096E+00 0.57694E+00 
c  k            0.16851E-01       8   0.12009E-03   0.41398E-04 0.21555E+02 
c  epsilon      0.46104E+02       7   0.27572E-03   0.16423E+04 0.73860E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.7175e-05                            10
a  epsilon               -0.066332                            18
a  Local Time Step      4.2278e-08                        217486


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8336          3.3354         0.27159        0.049373
v  Velocity[Y]             -4.1536          4.2716         0.15011         0.11907
v  Velocity[Z]             -6.6374          5.4701       -0.083918     -0.00048636
v  ǁVelocityǁ           0.00011716           7.391         0.75379         0.98341
v  Pressure                -4451.8          9073.7          5829.4          4949.9
v  k                     3.073e-08         0.41263       0.0024634       0.0047187
v  epsilon              5.7657e-05            7616          5.9018          1.9442
v  TurbVisc             2.3161e-13         0.11253        0.002137       0.0046822
v  CourantNb             0.0011405          1011.9          4.6646          1.3241
v  FourierNb              0.032987      2.3653e+05           22.36         0.42412
v  total_pressure       4.9555e+05      5.0907e+05      5.0583e+05      5.0495e+05
v  Local Time Step           0.001         0.17326       0.0013151       0.0018162


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97786      2.3754e+05          27.025          1.7483


 TIME FOR THE TIME STEP               67:        0.63985E+02

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


 INSTANT    0.680000000E+00   TIME STEP NUMBER              68
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.444011391E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442601286E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.77939E+00 0.14617E+01
   Friction velocity        uet   :  0.19320E-02 0.44632E+01
   Friction velocity        uk    :  0.19316E-02 0.44632E+01
   Dimensionless distance   yplus :  0.56950E-03 0.75294E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        652
   Nb of faces within the viscous sub-layer     :      33163
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      ------------------------------------------------------------------------------------------------
c  Velocity     0.14930E+01      17   0.26063E-01   0.21330E+00 0.13415E+02 
c  Velocity[X]                                      0.53300E-01 
c  Velocity[Y]                                      0.75459E-01 
c  Velocity[Z]                                      0.84542E-01 
c  Pressure     0.78216E-02     397   0.30453E-01   0.10096E+00 0.57694E+00 
c  k            0.16851E-01       8   0.12009E-03   0.41398E-04 0.21555E+02 
c  epsilon      0.46104E+02       7   0.27572E-03   0.16423E+04 0.73860E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.7175e-05                            10
a  epsilon               -0.066332                            18
a  Local Time Step      4.2278e-08                        217486


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8336          3.3354         0.27159        0.049373
v  Velocity[Y]             -4.1536          4.2716         0.15011         0.11907
v  Velocity[Z]             -6.6374          5.4701       -0.083918     -0.00048636
v  ǁVelocityǁ           0.00011716           7.391         0.75379         0.98341
v  Pressure                -4451.8          9073.7          5829.4          4949.9
v  k                     3.073e-08         0.41263       0.0024634       0.0047187
v  epsilon              5.7657e-05            7616          5.9018          1.9442
v  TurbVisc             2.3161e-13         0.11253        0.002137       0.0046822
v  CourantNb             0.0011405          1011.9          4.6646          1.3241
v  FourierNb              0.032987      2.3653e+05           22.36         0.42412
v  total_pressure       4.9555e+05      5.0907e+05      5.0583e+05      5.0495e+05
v  Local Time Step           0.001         0.17326       0.0013151       0.0018162


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97786      2.3754e+05          27.025          1.7483


 TIME FOR THE TIME STEP               67:        0.78321E+02

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


 INSTANT    0.680000000E+00   TIME STEP NUMBER              68
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.444011391E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442601286E+00
Free inlet               13         Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442452397E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.77271E+00 0.14643E+01
   Friction velocity        uet   :  0.52281E-02 0.40338E+01
   Friction velocity        uk    :  0.52189E-02 0.40338E+01
   Dimensionless distance   yplus :  0.49078E-03 0.75271E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        644
   Nb of faces within the viscous sub-layer     :      33150
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14928E+01      17   0.25948E-01   0.21887E+00 0.13610E+02 
c  Velocity[X]                                      0.56730E-01 
c  Velocity[Y]                                      0.73186E-01 
c  Velocity[Z]                                      0.88955E-01 
c  Pressure     0.78787E-02     403   0.31080E-01   0.10194E+00 0.59779E+00 
c  k            0.16849E-01       8   0.11376E-03   0.36103E-04 0.20037E+02 
c  epsilon      0.46089E+02       7   0.22741E-03   0.15049E+04 0.70544E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.1652e-05                            10
a  epsilon                -0.21812                            19
a  Local Time Step      4.2278e-08                        218164


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8351          3.3409         0.27166         0.04933
v  Velocity[Y]             -4.1329          4.2658         0.14942         0.11902
v  Velocity[Z]             -6.5949          5.1822       -0.084687     -0.00036645
v  ǁVelocityǁ           5.6607e-05          7.4059         0.75583         0.98394
v  Pressure                -4455.6            9051          5803.8            4930
v  k                    3.0068e-08         0.41205       0.0024746       0.0047218
v  epsilon              5.2333e-05          7599.2           5.938          1.9455
v  TurbVisc             2.3167e-13         0.33475       0.0020298       0.0046664
v  CourantNb                     0          582.64          4.6696          1.3253
v  FourierNb               0.03301      2.3653e+05          22.338         0.42152
v  total_pressure       4.9554e+05      5.0905e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17325       0.0013098        0.001812


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.033      2.3711e+05          27.007          1.7468


 TIME FOR THE TIME STEP               69:        0.65389E+02

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


 INSTANT    0.700000000E+00   TIME STEP NUMBER              70
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2 Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442452397E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.77271E+00 0.14643E+01
   Friction velocity        uet   :  0.52281E-02 0.40338E+01
   Friction velocity        uk    :  0.52189E-02 0.40338E+01
   Dimensionless distance   yplus :  0.49078E-03 0.75271E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        644
   Nb of faces within the viscous sub-layer     :      33150
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14928E+01      17   0.25948E-01   0.21887E+00 0.13610E+02 
c  Velocity[X]                                      0.56730E-01 
c  Velocity[Y]                                      0.73186E-01 
c  Velocity[Z]                                      0.88955E-01 
c  Pressure     0.78787E-02     403   0.31080E-01   0.10194E+00 0.59779E+00 
c  k            0.16849E-01       8   0.11376E-03   0.36103E-04 0.20037E+02 
c  epsilon      0.46089E+02       7   0.22741E-03   0.15049E+04 0.70544E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.1652e-05                            10
a  epsilon                -0.21812                            19
a  Local Time Step      4.2278e-08                        218164


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8351          3.3409         0.27166         0.04933
v  Velocity[Y]             -4.1329          4.2658         0.14942         0.11902
v  Velocity[Z]             -6.5949          5.1822       -0.084687     -0.00036645
v  ǁVelocityǁ           5.6607e-05          7.4059         0.75583         0.98394
v  Pressure                -4455.6            9051          5803.8            4930
v  k                    3.0068e-08         0.41205       0.0024746       0.0047218
v  epsilon              5.2333e-05          7599.2           5.938          1.9455
v  TurbVisc             2.3167e-13         0.33475       0.0020298       0.004666v  epsilon              5.0898e-05          7579.9          5.9204          1.9453
v  TurbVisc             2.3247e-13         0.11253       0.0019792       0.0046578
v  CourantNb            1.1963e-06          445.01          4.6766          1.3259
v  FourierNb              0.032991      2.3653e+05          22.327         0.42055
v  total_pressure       4.9555e+05      5.0905e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17325       0.0013072        0.001813


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0274      2.3697e+05          27.004          1.7464


 TIME FOR THE TIME STEP               70:        0.65031E+02

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


 INSTANT    0.710000000E+00   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.272947133E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442459213E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74676E+00 0.14621E+01
   Friction velocity        uet   :  0.13577E-02 0.38629E+01
   Friction velocity        uk    :  0.13574E-02 0.38629E+01
   Dimensionless distance   yplus :  0.37564E-03 0.74892E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        639
   Nb of faces within the viscous sub-layer     :      33139
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14928E+01      15   0.25847E-01   0.21068E+00 0.13355E+02 
c  Velocity[X]                                      0.54243E-01 
c  Velocity[Y]                                      0.72934E-01 
c  Velocity[Z]                                      0.83498E-01 
c  Pressure     0.75815E-02     412   0.29677E-01   0.98013E-01 0.55555E+00 
c  k            0.16842E-01      10   0.84493E-04   0.30186E-04 0.17998E+02 
c  epsilon      0.45796E+02       8   0.27854E-03   0.87788E+03 0.53925E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.8937e-05                            11
a  epsilon                 -0.1654                            16
a  Local Time Step      4.2278e-08                        218843


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8399          3.3252         0.27154        0.049246
v  Velocity[Y]             -4.1337          4.2401         0.14879           0.119
v  Velocity[Z]             -6.5554          5.1866       -0.085478     -0.00030315
v  ǁVelocityǁ           8.5757e-05          7.3819         0.75774         0.98438
v v  epsilon              5.0898e-05          7579.9          5.9204          1.9453
v  TurbVisc             2.3247e-13         0.11253       0.0019792       0.0046578
v  CourantNb            1.1963e-06          445.01          4.6766          1.3259
v  FourierNb              0.032991      2.3653e+05          22.327         0.42055
v  total_pressure       4.9555e+05      5.0905e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17325       0.0013072        0.001813


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0274      2.3697e+05          27.004          1.7464


 TIME FOR THE TIME STEP               70:        0.75222E+02

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


 INSTANT    0.710000000E+00   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.272947133E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442459213E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74676E+00 0.14621E+01
   Friction velocity        uet   :  0.13577E-02 0.38629E+01
   Friction velocity        uk    :  0.13574E-02 0.38629E+01
   Dimensionless distance   yplus :  0.37564E-03 0.74892E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        639
   Nb of faces within the viscous sub-layer     :      33139
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14928E+01      15   0.25847E-01   0.21068E+00 0.13355E+02 
c  Velocity[X]                                      0.54243E-01 
c  Velocity[Y]                                      0.72934E-01 
c  Velocity[Z]                                      0.83498E-01 
c  Pressure     0.75815E-02     412   0.29677E-01   0.98013E-01 0.55555E+00 
c  k            0.16842E-01      10   0.84493E-04   0.30186E-04 0.17998E+02 
c  epsilon      0.45796E+02       8   0.27854E-03   0.87788E+03 0.53925E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.8937e-05                            11
a  epsilon                 -0.1654                            16
a  Local Time Step      4.2278e-08                        218843


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8399          3.3252         0.27154        0.049246
v  Velocity[Y]             -4.1337          4.2401         0.14879           0.119
v  Velocity[Z]             -6.5554          5.1866       -0.085478     -0.00030315
v  ǁVelocityǁ           8.5757e-05          7.3819         0.75774         0.98438
v  Pressure                -4446.4          9053.8            5805          4930.9
v  k                    2.9862e-08         0.41173       0.0024812        0.004724
v  epsilon              4.7591e-05          7583.2          5.9191          1.9439
v  TurbVisc             2.3294e-13         0.11253        0.001934       0.0046502
v  CourantNb             9.943e-05          738.04          4.6818          1.3264
v  FourierNb              0.032979      2.3653e+05          22.318         0.41919
v  total_pressure       4.9555e+05      5.0905e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17325       0.0013044        0.001811


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97895      2.3727e+05          26.999          1.7456


 TIME FOR THE TIME STEP               71:        0.65892E+02

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


 INSTANT    0.720000000E+00   TIME STEP NUMBER              72
 ==============================Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442452397E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.77271E+00 0.14643E+01
   Friction velocity        uet   :  0.52281E-02 0.40338E+01
   Friction velocity        uk    :  0.52189E-02 0.40338E+01
   Dimensionless distance   yplus :  0.49078E-03 0.75271E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        644
   Nb of faces within the viscous sub-layer     :      33150
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14928E+01      17   0.25948E-01   0.21887E+00 0.13610E+02 
c  Velocity[X]                                      0.56730E-01 
c  Velocity[Y]                                      0.73186E-01 
c  Velocity[Z]                                      0.88955E-01 
c  Pressure     0.78787E-02     403   0.31080E-01   0.10194E+00 0.59779E+00 
c  k            0.16849E-01       8   0.11376E-03   0.36103E-04 0.20037E+02 
c  epsilon      0.46089E+02       7   0.22741E-03   0.15049E+04 0.70544E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     ic  Velocity[Z]                                      0.84020E-01 
c  Pressure     0.74265E-02     336   0.29304E-01   0.95920E-01 0.54255E+00 
c  k            0.16842E-01       9   0.92392E-04   0.25956E-04 0.16928E+02 
c  epsilon      0.45712E+02       8   0.25247E-03   0.10335E+04 0.58700E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.2772e-05                            11
a  epsilon                -0.12223                            17
a  Local Time Step      4.2278e-08                        219108


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8411          3.3043         0.27143        0.049206
v  Velocity[Y]             -4.0607          4.2505         0.14847         0.11899
v  Velocity[Z]             -6.5448          5.2342       -0.085853     -0.00027819
v  ǁVelocityǁ           0.00011212          7.3429         0.75865         0.98456
v  Pressure                -4429.1            9055          5805.7          4931.3
v  k                    2.0495e-08         0.41009       0.0024858        0.004725
v  epsilon              4.6143e-05          7543.3          5.9073          1.9448
v  TurbVisc             2.3302e-13         0.11253       0.0018896       0.0046427
v  CourantNb            0.00049955          414.07          4.6834          1.3269
v  FourierNb              0.032986      2.3653e+05          22.308         0.41842
v  total_pressure       4.9557e+05      5.0905e+05      5.0581e+05      5.0493e+05
v  Local Time Step           0.001         0.17325       0.0013021       0.0018135


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.033      2.3694e+05          26.991          1.7453


 TIME FOR THE TIME STEP               72:        0.66253E+02

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


 INSTANT    0.730000000E+00   TIME STEP NUMBER              73
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.574857754E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442402602E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
------------------------------------Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75406E+00 0.14573E+01
   Friction velocity        uet   :  0.59577E-02 0.41184E+01
   Friction velocity        uk    :  0.59568E-02 0.41184E+01
   Dimensionless distance   yplus :  0.52551E-03 0.74535E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        638
   Nb of faces within the viscous sub-layer     :      33129
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14928E+01      17   0.25968E-01   0.21272E+00 0.13409E+02 
c  Velocity[X]                                      0.53581E-01 
c  Velocity[Y]                                      0.76693E-01 
c  Velocity[Z]                                      0.82447E-01 
c  Pressure     0.75246E-02     304   0.29388E-01   0.96750E-01 0.51408E+00 
c  k            0.16837E-01       8   0.11333E-03   0.31737E-04 0.18845E+02 
c  epsilon      0.45537E+02       7   0.26061E-03   0.91311E+03 0.55343E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.4795e-05                             9
a  epsilon                -0.15132                            14
a  Local Time Step      4.2278e-08                        219808


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

   field  v  epsilon              5.0898e-05          7579.9          5.9204          1.9453
v  TurbVisc             2.3247e-13         0.11253       0.0019792       0.0046578
v  CourantNb            1.1963e-06          445.01          4.6766          1.3259
v  FourierNb              0.032991      2.3653e+05          22.327         0.42055
v  total_pressure       4.9555e+05      5.0905e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17325       0.0013072        0.001813


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0274      2.3697e+05          27.004          1.7464


 TIME FOR THE TIME STEP               70:        0.68791E+02

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


 INSTANT    0.710000000E+00   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.272947133E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442459213E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uFree surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75406E+00 0.14573E+01
   Friction velocity        uet   :  0.59577E-02 0.41184E+01
   Friction velocity        uk    :  0.59568E-02 0.41184E+01
   Dimensionless distance   yplus :  0.52551E-03 0.74535E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        638
   Nb of faces within the viscous sub-layer     :      33129
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14928E+01      17   0.25968E-01   0.21272E+00 0.13409E+02 
c  Velocity[X]                                      0.53581E-01 
c  Velocity[Y]                                      0.76693E-01 
c  Velocity[Z]                                      0.82447E-01 
c  Pressure     0.75246E-02     304   0.29388E-01   0.96750E-01 0.51408E+00 
c  k            0.16837E-01       8   0.11333E-03   0.31737E-04 0.18845E+02 
c  epsilon      0.45537E+02       7   0.26061E-03   0.91311E+03 0.55343E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.4795e-05                             9
a  epsilon                -0.15132                            14
a  Local Time Step      4.2278e-08                        219808


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8549          3.3179         0.27116        0.049117
v  Velocity[Y]             -4.0243          4.2171         0.14787         0.11892
v  Velocity[Z]             -6.5426          5.3546       -0.086585     -0.00026107
v  ǁVelocityǁ           0.00010453          7.3471         0.76038           0.985
v  Pressure                -4412.8          9072.3          5819.2            4942
v  k                    4.6828e-09         0.40993       0.0024923       0.0047254
v  epsilon              2.3822e-05          7531.2          5.8926          1.9426
v  TurbVisc             2.3153e-13         0.11253       0.0018034       0.0046282
v  CourantNb            0.00067577          650.73          4.6926          1.3278
v  FourierNb              0.032957      2.3653e+05           22.29         0.41655
v  total_pressure       4.9559e+05      5.0907e+05      5.0582e+05      5.0494e+0v  FourierNb               0.03297      2.3653e+05          22.282         0.41582
v  total_pressure        4.956e+05      5.0907e+05      5.0582e+05      5.0494e+05
v  Local Time Step           0.001         0.17325       0.0012957       0.0018173


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83824      2.3697e+05          26.975          1.7441


 TIME FOR THE TIME STEP               75:        0.69091E+02

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


 INSTANT    0.760000000E+00   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.444529167E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442416384E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74220E+00 0.14554E+01
   Friction velocity        uet   :  0.68724E-02 0.51919E+01
   Friction velocity        uk    :  0.68704E-02 0.51919E+01
   Dimensionless distance   yplus :  0.51734E-03 0.74675E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        628
   Nb of faces within the viscous sub-layer     :      33121
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14927E+01      14   0.25893E-01   0.20479E+00 0.13153E+02 
c  Velocity[X]                                      0.56276E-01 
c  Velocity[Y]                                      0.69201E-01 
c  Velocity[Z]                                      0.79308E-01 
c  Pressure     0.74199E-02     589   0.29084E-01   0.94950E-01 0.74667E+00 
c  k            0.16835E-01       9   0.89506E-04   0.34061E-04 0.19518E+02 
c  epsilon      0.45578E+02       7   0.23316E-03   0.10040E+04 0.58039E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.5282e-06                             8
a  epsilon               -0.098703                            13
a  Local Time Step      4.2278e-08                        220477


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8514          3.3702         0.27103        0.049079
v  Velocity[Y]             -4.0854          4.2087         0.14728         0.11889
v  Velocity[Z]             -6.5327          5.3259       -0.087377     -0.00026092
v  ǁVelocityǁ           0.00022915          7.3748         0.76222         0.98534
v  Pressure                -4411.9          9080.3          5821.9          4942.8
v  k                     3.189e-09         0.40941       0.0025015       0.0047264
v  epsilon              1.2156e-05          7516.1          5.8948          1.9434
v v  FourierNb               0.03297      2.3653e+05          22.282         0.41582
v  total_pressure        4.956e+05      5.0907e+05      5.0582e+05      5.0494e+05
v  Local Time Step           0.001         0.17325       0.0012957       0.0018173


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83824      2.3697e+05          26.975          1.7441


 TIME FOR THE TIME STEP               75:        0.65009E+02

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


 INSTANT    0.760000000E+00   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.444529167E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442416384E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74220E+00 0.14554E+01
   Friction velocity        uet   :  0.68724E-02 0.51919E+01
   Friction velocity        uk    :  0.68704E-02 0.51919E+01
   Dimensionless distance   yplus :  0.51734E-03 0.74675E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        628
   Nb of faces within the viscous sub-layer     :      33121
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14927E+01      14   0.25893E-01   0.20479E+00 0.13153E+02 
c  Velocity[X]                                      0.56276E-01 
c  Velocity[Y]                                      0.69201E-01 
c  Velocity[Z]                                      0.79308E-01 
c  Pressure     0.74199E-02     589   0.29084E-01   0.94950E-01 0.74667E+00 
c  k            0.16835E-01       9   0.89506E-04   0.34061E-04 0.19518E+02 
c  epsilon      0.45578E+02       7   0.23316E-03   0.10040E+04 0.58039E+02 
-----------------------------------------------------------------------------
  
  

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

   field-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -7.654e-06                             7
a  epsilon                -0.13897                            16
a  Local Time Step      4.2278e-08                        220830


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8539           3.346         0.27094        0.049068
v  Velocity[Y]             -4.0901          4.1874         0.14694         0.11884
v  Velocity[Z]             -6.5371          5.2248       -0.087799     -0.00025426
v  ǁVelocityǁ           0.00022389          7.3576         0.76316         0.98555
v  Pressure                -4408.4          9081.3          5823.2          4947.2
v  k                    4.4165e-09         0.40988       0.0025049       0.0047269
v  epsilon              1.7386e-05          7527.7          5.8752           1.943
v  TurbVisc             2.3278e-13         0.11253       0.0016828       0.0046073
v  CourantNb             0.0017389          665.45          4.7025          1.3291
v  FourierNb              0.032966      2.3653e+05          22.265         0.41473
v  total_pressure       4.9559e+05      5.0908e+05      5.0582e+05      5.0495e+05
v  Local Time Step           0.001         0.17325       0.0012923       0.0018222


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7528       2.372e+05          26.968          1.7439


 TIME FOR THE TIME STEP               77:        0.69420E+02

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


 INSTANT    0.780000000E+00   TIME STEP NUMBER              78
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75406E+00 0.14573E+01
   Friction velocity        uet   :  0.59577E-02 0.41184E+01
   Friction velocity        uk    :  0.59568E-02 0.41184E+01
   Dimensionless distance   yplus :  0.52551E-03 0.74535E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        638
   Nb of faces within the viscous sub-layer     :      33129
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14928E+01      17   0.25968E-01   0.21272E+00 0.13409E+02 
c  Velocity[X]                                      0.53581E-01 
c  Velocity[Y]                                      0.76693E-01 
c  Velocity[Z]                                      0.82447E-01 
c  Pressure     0.75246E-02     304   0.29388E-01   0.96750E-01 0.51408E+00 
c  k            0.16837E-01       8   0.11333E-03   0.31737E-04 0.18845E+02 
c  epsilon      0.45537E+02       7   0.26061E-03   0.91311E+03 0.55343E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.4795e-05                             9
a  epsilon                -0.15132                            14
a  Local Time Step      4.2278e-08              -----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -7.654e-06                             7
a  epsilon                -0.13897                            16
a  Local Time Step      4.2278e-08                        220830


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8539           3.346         0.27094        0.049068
v  Velocity[Y]             -4.0901          4.1874         0.14694         0.11884
v  Velocity[Z]             -6.5371          5.2248       -0.087799     -0.00025426
v  ǁVelocityǁ           0.00022389          7.3576         0.76316         0.98555
v  Pressure                -4408.4          9081.3          5823.2          4947.2
v  k                    4.4165e-09         0.40988       0.0025049       0.0047269
v  epsilon              1.7386e-05          7527.7          5.8752           1.943
v  TurbVisc             2.3278e-13         0.11253       0.0016828       0.0046073
v  CourantNb             0.0017389          665.45          4.7025          1.3291
v  FourierNb              0.032966      2.3653e+05          22.265         0.41473
v  total_pressure       4.9559e+05      5.0908e+05      5.0582e+05      5.0495e+05
v  Local Time Step           0.001         0.17325       0.0012923       0.0018222


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7528       2.372e+05          26.968          1.7439


 TIME FOR THE TIME STEP               77:        0.67348E+02

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


 INSTANT    0.780000000E+00   TIME STEP NUMBER              78
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.202320345E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442439502E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76426E+00 0.14556E+01
   Friction velocity        uet   :  0.83185E-02 0.42551E+01
   Friction velocity        uk    :  0.83032E-02 0.42551E+01
   Dimensionless distance   yplus :  0.35862E-03 0.74777E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        622
   Nb of faces within the viscous sub-layer     :      33103
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14926E+01      15   0.25897E-01   0.20576E+00 0.13151E+02 
c  Velocity[X]                                      0.55520E-01 
c  Velocity[Y]                                      0.71814E-01 
c  Velocity[Z]                                      0.78424E-01 
c  Pressure     0.77850E-02     548   0.31258E-01   0.10072E+00 0.64169E+00 
c  k            0.16826E-01       8   0.12736E-03   0.59843E-04 0.25911E+02 
c  epsilon      0.45588E+02       8   0.30680E-03   0.15062E+04 0.71132E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.3187e-06                             6
a  epsilon               -0.092777                            16
a  Local Time Step      4.2278e-08                        221471


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8635          3.3682         0.27085        0.049026
v  Velocitv  FourierNb               0.03297      2.3653e+05          22.282         0.41582
v  total_pressure        4.956e+05      5.0907e+05      5.0582e+05      5.0494e+05
v  Local Time Step           0.001         0.17325       0.0012957       0.0018173


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83824      2.3697e+05          26.975          1.7441


 TIME FOR THE TIME STEP               75:        0.67342E+02

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


 INSTANT    0.760000000E+00   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.444529167E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442416384E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74220E+00 0.14554E+01
   Friction velocity        uet   :  0.68724E-02 0.51919E+01
   Friction velocity        uk    :  0.68704E-02 0.51919E+01
   Dimensionless distance   yplus :  0.51734E-03 0.74675E+01
   ------------------------------------------------------
   Nb o------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76426E+00 0.14556E+01
   Friction velocity        uet   :  0.83185E-02 0.42551E+01
   Friction velocity        uk    :  0.83032E-02 0.42551E+01
   Dimensionless distance   yplus :  0.35862E-03 0.74777E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        622
   Nb of faces within the viscous sub-layer     :      33103
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14926E+01      15   0.25897E-01   0.20576E+00 0.13151E+02 
c  Velocity[X]                                      0.55520E-01 
c  Velocity[Y]                                      0.71814E-01 
c  Velocity[Z]                                      0.78424E-01 
c  Pressure     0.77850E-02     548   0.31258E-01   0.10072E+00 0.64169E+00 
c  k            0.16826E-01       8   0.12736E-03   0.59843E-04 0.25911E+02 
c  epsilon      0.45588E+02       8   0.30680E-03   0.15062E+04 0.71132E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.3187e-06                             6
a  epsilon               -0.092777                            16
a  Local Time Step      4.2278e-08                        221471


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8635          3.3682         0.27085        0.049026
v  Velocity[Y]             -4.1138          4.1623         0.14634         0.11879
v  Velocity[Z]              -6.484          5.2192       -0.088703     -0.00030541
v  ǁVelocityǁ           0.00025492          7.3275         0.76504         0.98588
v  Pressure                -4426.9          9083.3          5825.6          4945.9
v  k                    6.1999e-09         0.41001       0.0025138       0.0047265
v  epsilon              1.7226e-05          7527.7          5.8883          1.9411
v  TurbVisc             2.3335e-13         0.11253       0.0016156       0.0045944
v  CourantNb            0.00092352          533.74          4.7121          1.3299
v  FourierNb              0.032976      2.3653e+05          22.253         0.41407
v  total_pressure       4.9557e+05      5.0908e+05      5.0583e+05      5.0495e+05
v  Local Time Step           0.001         0.17325       0.0012896       0.0018294


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  ------------
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6478      2.3703e+05          26.962          1.7436


 TIME FOR THE TIME STEP               80:        0.69444E+02

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


 INSTANT    0.810000000E+00   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.269091850E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442487125E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68951E+00 0.14564E+01
   Friction velocity        uet   :  0.63768E-02 0.42644E+01
   Friction velocity        uk    :  0.63651E-02 0.42644E+01
   Dimensionless distance   yplus :  0.39505E-03 0.75157E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        625
   Nb of faces within the viscous sub-layer     :      33109
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14926E+01      16   0.25676E-01   0.19712E+00 0.12873E+02 
c  Velocity[X]                                      0.54799E-01 
c  Velocity[Y]                                      0.67497E-01 
c  Velocity[Z]                                      0.74829E-01 
c  Pressure     0.76841E-02     349   0.30796E-01   0.99097E-01 0.58336E+00 
c  k            0.16822E-01      10   0.10935E-03   0.43056E-04 0.21992E+02 
c  epsilon      0.45616E+02       9   0.28785E-03   0.15499E+04 0.72220E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0628e-05                             8
a  epsilon                -0.54219                            17
a  Local Time Step      4.2278e-08                        222041


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8709          3.3457         0.27077        0.048962
v  Velocity[Y]             -4.3423          4.1459         0.14561         0.11869
v  Velocity[Z]             -6.5273          5.4007        -0.08952     -0.00035073
v  ǁVelocityǁ            0.0002935          7.3346          0.7669         0.98616
v  Pressure                -4429.1          9086.9          5824.9          4945.5
v  k                    8.4803e-09         0.41026         0.00252       0.0047256
v  epsilon              2.4209e-05          7531.9           5.886          1.9387
v  TurbVisc             2.3463e-13         0.11253       0.0015474       0.0045814
v  CourantNb            0.00062689          831.14          4.7219          1.3307
v  FourierNb              0.032989      2.3653e+05           22.24         0.41282
v  total_pressure       4.9557e+05      5.0909e+05      5.0582e+
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6478      2.3703e+05          26.962          1.7436


 TIME FOR THE TIME STEP               80:        0.65300E+02

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


 INSTANT    0.810000000E+00   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.269091850E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442487125E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68951E+00 0.14564E+01
   Friction velocity        uet   :  0.63768E-02 0.42644E+01
   Friction velocity        uk    :  0.63651E-02 0.42644E+01
   Dimensionless distance   yplus :  0.39505E-03 0.75157E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        625
   Nb of faces within the viscous sub-layer     :      33109
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14926E+01      16   0.25676E-01   0.19712E+00 0.12873E+02 
c  Velocity[X]                                      0.54799E-01 
c  Velocity[Y]                                      0.67497E-01 
c  Velocity[Z]                                      0.74829E-01 
c  Pressure     0.76841E-02     349   0.30796E-01   0.99097E-01 0.58336E+00 
c  k            0.16822E-01      10   0.10935E-03   0.43056E-04 0.21992E+02 
c  epsilon      0.45616E+02       9   0.28785E-03   0.15499E+04 0.72220E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0628e-05                             8
a  epsilon                -0.54219                            17
a  Local Time Step      4.2278e-08a  k                   -9.1022e-06                             8
a  epsilon               -0.050311                            11
a  Local Time Step      4.2278e-08                        222294


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8757          3.3369         0.27079        0.048956
v  Velocity[Y]             -4.2796           4.124         0.14522         0.11864
v  Velocity[Z]             -6.5165           5.494       -0.090008      -0.0004072
v  ǁVelocityǁ           0.00022078          7.3304         0.76792         0.98631
v  Pressure                -4422.8          9088.5          5824.4          4946.1
v  k                    8.3519e-09         0.40819       0.0025269       0.0047254
v  epsilon              2.2507e-05          7481.3           5.914          1.9413
v  TurbVisc             2.3653e-13         0.11253       0.0015128       0.0045751
v  CourantNb              0.004231          670.74          4.7271          1.3311
v  FourierNb              0.032991      2.3653e+05          22.233         0.41243
v  total_pressure       4.9558e+05      5.0909e+05      5.0582e+05      5.0495e+05
v  Local Time Step           0.001         0.17326       0.0012855        0.001832


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40921       2.372e+05           26.96          1.7435


 TIME FOR THE TIME STEP               82:        0.62261E+02

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


 INSTANT    0.830000000E+00   TIME STEP NUMBER              83
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth w------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76426E+00 0.14556E+01
   Friction velocity        uet   :  0.83185E-02 0.42551E+01
   Friction velocity        uk    :  0.83032E-02 0.42551E+01
   Dimensionless distance   yplus :  0.35862E-03 0.74777E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        622
   Nb of faces within the viscous sub-layer     :      33103
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14926E+01      15   0.25897E-01   0.20576E+00 0.13151E+02 
c  Velocity[X]                                      0.55520E-01 
c  Velocity[Y]                                      0.71814E-01 
c  Velocity[Z]                                      0.78424E-01 
c  Pressure     0.77850E-02     548   0.31258E-01   0.10072E+00 0.64169E+00 
c  k            0.16826E-01       8   0.12736E-03   0.59843E-04 0.25911E+02 
c  epsilon      0.45588E+02       8   0.30680E-03   0.15062E+04 0.71132E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.3187e-06                             6
a  epsilon               -0.092777                            16
a  Local Time Step      4.2278e-08                        221471


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8635          3.3682         0.27085  a  k                   -9.1022e-06                             8
a  epsilon               -0.050311                            11
a  Local Time Step      4.2278e-08                        222294


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8757          3.3369         0.27079        0.048956
v  Velocity[Y]             -4.2796           4.124         0.14522         0.11864
v  Velocity[Z]             -6.5165           5.494       -0.090008      -0.0004072
v  ǁVelocityǁ           0.00022078          7.3304         0.76792         0.98631
v  Pressure                -4422.8          9088.5          5824.4          4946.1
v  k                    8.3519e-09         0.40819       0.0025269       0.0047254
v  epsilon              2.2507e-05          7481.3           5.914          1.9413
v  TurbVisc             2.3653e-13         0.11253       0.0015128       0.0045751
v  CourantNb              0.004231          670.74          4.7271          1.3311
v  FourierNb              0.032991      2.3653e+05          22.233         0.41243
v  total_pressure       4.9558e+05      5.0909e+05      5.0582e+05      5.0495e+05
v  Local Time Step           0.001         0.17326       0.0012855        0.001832


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40921       2.372e+05           26.96          1.7435


 TIME FOR THE TIME STEP               82:        0.64156E+02

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


 INSTANT    0.830000000E+00   TIME STEP NUMBER              83
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.277537311E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442497709E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74453E+00 0.14538E+01
   Friction velocity        uet   :  0.64322E-02 0.42704E+01
   Friction velocity        uk    :  0.64203E-02 0.42704E+01
   Dimensionless distance   yplus :  0.40110E-03 0.75333E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   Dimensionless distance   yplus :  0.10406E-03 0.75499E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        617
   Nb of faces within the viscous sub-layer     :      33118
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14926E+01      15   0.25154E-01   0.19506E+00 0.12831E+02 
c  Velocity[X]                                      0.53078E-01 
c  Velocity[Y]                                      0.69691E-01 
c  Velocity[Z]                                      0.72289E-01 
c  Pressure     0.78211E-02     416   0.31553E-01   0.10076E+00 0.63437E+00 
c  k            0.16822E-01       9   0.11273E-03   0.39483E-04 0.21005E+02 
c  epsilon      0.45469E+02       9   0.31388E-03   0.12454E+04 0.64812E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0405e-05                             9
a  epsilon                -0.48203                            14
a  Local Time Step      4.2278e-08                        222789


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8794          3.3497         0.27099        0.048976
v  Velocity[Y]             -4.0715          4.1143         0.14442         0.11854
v  Velocity[Z]             -6.5186          5.4573       -0.090915     -0.00041305
v  ǁVelocityǁ           0.00020764          7.3443         0.76986         0.98655
v  Pressure                -4453.3          9088.5          5821.8    
   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6478      2.3703e+05          26.962          1.7436


 TIME FOR THE TIME STEP               80:        0.65629E+02

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


 INSTANT    0.810000000E+00   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.269091850E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442487125E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68951E+00 0.14564E+01
   Friction velocity        uet   :  0.63768E-02 0.42644E+01
   Friction velocity        uk    :  0.63651E-02 0.42644E+01
   Dimensionless distance   yplus :  0.39505E-03 0.75157E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        625
   Nb of faces within the viscous sub-layer     :      33109
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
------------------------------------------------------------   Dimensionless distance   yplus :  0.10406E-03 0.75499E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        617
   Nb of faces within the viscous sub-layer     :      33118
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14926E+01      15   0.25154E-01   0.19506E+00 0.12831E+02 
c  Velocity[X]                                      0.53078E-01 
c  Velocity[Y]                                      0.69691E-01 
c  Velocity[Z]                                      0.72289E-01 
c  Pressure     0.78211E-02     416   0.31553E-01   0.10076E+00 0.63437E+00 
c  k            0.16822E-01       9   0.11273E-03   0.39483E-04 0.21005E+02 
c  epsilon      0.45469E+02       9   0.31388E-03   0.12454E+04 0.64812E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0405e-05                             9
a  epsilon                -0.48203                            14
a  Local Time Step      4.2278e-08                        222789


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8794          3.3497         0.27099        0.048976
v  Velocity[Y]             -4.0715          4.1143         0.14442         0.11854
v  Velocity[Z]             -6.5186          5.4573       -0.090915     -0.00041305
v  ǁVelocityǁ           0.00020764          7.3443         0.76986         0.98655
v  Pressure                -4453.3          9088.5          5821.8            4946
v  k                    1.6895e-08         0.40794       0.0025321       0.0047243
v  epsilon              3.5494e-05          7473.9          5.8999          1.9392
v  TurbVisc             2.3529e-13         0.11253        0.001443       0.0045627
v  CourantNb             0.0021729          500.31          4.7377          1.3318
v  FourierNb              0.033006      2.3653e+05           22.22         0.41171
v  total_pressure       4.9555e+05      5.0909e+05      5.0582e+05      5.0495e+05
v  Local Time Step           0.001         0.17326       0.0012832       0.0018352


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68387      2.3703e+05          26.958          1.7435


 TIME FOR THE TIME STEP               84:        0.67062E+02

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


 INSTANT    0.850000000E+00   TIME STEP NUMBER              85
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMAT INSTANT    0.860000000E+00   TIME STEP NUMBER              86
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.404651063E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442577352E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74686E+00 0.14520E+01
   Friction velocity        uet   :  0.90071E-02 0.65135E+01
   Friction velocity        uk    :  0.89875E-02 0.65135E+01
   Dimensionless distance   yplus :  0.54025E-03 0.75566E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        615
   Nb of faces within the viscous sub-layer     :      33113
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14925E+01      15   0.26054E-01   0.19965E+00 0.12987E+02 
c  Velocity[X]                                      0.55668E-01 
c  Velocity[Y]                                      0.69883E-01 
c  Velocity[Z]                                      0.74095E-01 
c  Pressure     0.76001E-02     267   0.30239E-01   0.97820E-01 0.51993E+00 
c  k            0.16822E-01      11   0.14133E-03   0.54000E-04 0.24442E+02 
c  epsilon      0.45499E+02      11   0.69650E-03   0.43310E+04 0.12060E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0889e-05                             7
a  epsilon               -0.058479                            12
a  Local Time Step      4.2278e-08                        223246


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8881          3.3752         0.27127        0.048991
v  Velocity[Y]             -4.2307          4.0781         0.14367         0.11849
v  Velocity[Z]             -6.5164          5.1724       -0.091651     -0.00047133
v  ǁVelocityǁ            0.0002302          7.3743         0.77183         0.98674
v  Pressure                -4462.6          9091.1          5820.8          4944.9
v  k                    1.8609e-08         0.40796       0.0025379       0.0047248
v  epsilon              3.6464e-05          7479.4          5.8882          1.9408
v  TurbVisc             2.4564e-13         0.11253        0.001378       0.0045511
v  CourantNb             0.0020173          466.67          4.7504          1.3327
v  FourierNb              0.033024      2.3653e+05          22.208         0.41106
v  total_pressure       4.9554e+05      5.0909e+05      5.0582e+05      5.0494e+05
v  Local Time Step           0.001         0.17326       0.0012811       0.0018388


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.95548        2.37e+0 INSTANT    0.860000000E+00   TIME STEP NUMBER              86
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.404651063E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442577352E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74686E+00 0.14520E+01
   Friction velocity        uet   :  0.90071E-02 0.65135E+01
   Friction velocity        uk    :  0.89875E-02 0.65135E+01
   Dimensionless distance   yplus :  0.54025E-03 0.75566E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        615
   Nb of faces within the viscous sub-layer     :      33113
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14925E+01      15   0.26054E-01   0.19965E+00 0.12987E+02 
c  Velocity[X]                                      0.55668E-01 
c  Velocity[Y]                                      0.69883E-01 
c  Velocity[Z]                                      0.74095E-01 
c  Pressure     0.76001E-02     267   0.30239E-01   0.97820E-01 0.51993E+00 
c  k            0.16822E-01      11   0.14133E-03   0.54000E-04 0.24442E+02 
c  epsilon      0.45499E+02      11   0.69650E-03   0.43310E+04 0.12060E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0889e-05                             7
a  epsilon               -0.058479                            12
a  Local Time Step      4.2278e-08                        223246


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8881          3.3752         0.27127        0.04899-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8859          3.3641         0.27145        0.048995
v  Velocity[Y]             -4.1439          4.0654         0.14322         0.11847
v  Velocity[Z]             -6.5179          5.4445       -0.091901     -0.00045397
v  ǁVelocityǁ           0.00025708          7.3384         0.77279         0.98679
v  Pressure                -4490.7          9073.9          5803.7          4930.6
v  k                    2.0525e-08         0.40804       0.0025439       0.0047245
v  epsilon              3.2851e-05            7474          5.9468          1.9396
v  TurbVisc              2.307e-13         0.11253       0.0013459       0.0045455
v  CourantNb             0.0020473          916.73          4.7585          1.3332
v  FourierNb              0.033051      2.3653e+05          22.203         0.41056
v  total_pressure       4.9551e+05      5.0907e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17327       0.0012798       0.0018398


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0331      2.3745e+05          26.961          1.7437


 TIME FOR THE TIME STEP               87:        0.75254E+02

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


 INSTANT    0.880000000E+00   TIME STEP NUMBER              88
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.110575231E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442545003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.0000   Dimensionless distance   yplus :  0.10406E-03 0.75499E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        617
   Nb of faces within the viscous sub-layer     :      33118
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14926E+01      15   0.25154E-01   0.19506E+00 0.12831E+02 
c  Velocity[X]                                      0.53078E-01 
c  Velocity[Y]                                      0.69691E-01 
c  Velocity[Z]                                      0.72289E-01 
c  Pressure     0.78211E-02     416   0.31553E-01   0.10076E+00 0.63437E+00 
c  k            0.16822E-01       9   0.11273E-03   0.39483E-04 0.21005E+02 
c  epsilon      0.45469E+02       9   0.31388E-03   0.12454E+04 0.64812E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0405e-05                             9
a  epsilon                -0.48203                            14
a  Local Time Step      4.2278e-08                        222789


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8794          3.3497         0.27099        0.048976
v  Velocity[Y]             -4.0715          4.1143         0.14442         0.11854
v  Velocity[Z]             -6.5186          5.4573       -0.090915     -0.00041305
v  ǁVelocityǁ           0.00020764          7.3443         0.76986         0.98655
v  Pressure                -4453.3          9088.5          5821.8         -  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8859          3.3641         0.27145        0.048995
v  Velocity[Y]             -4.1439          4.0654         0.14322         0.11847
v  Velocity[Z]             -6.5179          5.4445       -0.091901     -0.00045397
v  ǁVelocityǁ           0.00025708          7.3384         0.77279         0.98679
v  Pressure                -4490.7          9073.9          5803.7          4930.6
v  k                    2.0525e-08         0.40804       0.0025439       0.0047245
v  epsilon              3.2851e-05            7474          5.9468          1.9396
v  TurbVisc              2.307e-13         0.11253       0.0013459       0.0045455
v  CourantNb             0.0020473          916.73          4.7585          1.3332
v  FourierNb              0.033051      2.3653e+05          22.203         0.41056
v  total_pressure       4.9551e+05      5.0907e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17327       0.0012798       0.0018398


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0331      2.3745e+05          26.961          1.7437


 TIME FOR THE TIME STEP               87:        0.76721E+02

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


 INSTANT    0.880000000E+00   TIME STEP NUMBER              88
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.110575231E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442545003E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74898E+00 0.14515E+01
   Friction velocity        uet   :  0.12573E-01 0.41490E+01
   Friction velocity        uk    :  0.12571E-01 0.41490E+01
   Dimensionless distance   yplus :  0.44552E-03 0.75740E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        611
   Nb of faces within the viscous sub-layer     :      33116
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14920E+01      15   0.25597E-01   0.18929E+00 0.12654E+02 
c  Velocity[X]                                      0.54734E-01 
c  Velocity[Y]                                      0.66182E-01 
c  Velocity[Z]                                      0.68372E-01 
c  Pressure     0.73493E-02     301   0.28976E-01   0.95588E-01 0.51314E+00 
c  k            0.16822E-01      12   0.11968E-03   0.48845E-04 0.23147E+02 
c  epsilon      0.45646E+02      10   0.42367E-03   0.22091E+04 0.86140E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -1.126e-05                             9
a  epsilon               -0.055196                            10
a  Local Time Step      4.2278e-08                        223881


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8897          3.3687         0.27185        0.048977
v  Velocity[Y]             -4.2687           4.056         0.14243         0.11843
v  Velocity[Z]             -6.5247          5.2357       -0.092487     -0.00045297
v  ǁVelocityǁ            0.0002312          7.3798         0.77456         0.98686
v  Pressure                -4487.5          9074.3          5803.1          4931.6
v  k                    2.1923e-08         0.40886       0.0025445       0.0047239
v  epsilon              3.5296e-05          7499.3          5.9177          1.9391
v  TurbVisc             2.3621e-13         0.11253        0.001289       0.0045351
v  CourantNb             0.0015345          582.45          4.7684           1.334
v  FourierNb              0.033091  INSTANT    0.860000000E+00   TIME STEP NUMBER              86
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.404651063E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442577352E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74686E+00 0.14520E+01
   Friction velocity        uet   :  0.90071E-02 0.65135E+01
   Friction velocity        uk    :  0.89875E-02 0.65135E+01
   Dimensionless distance   yplus :  0.54025E-03 0.75566E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        615
   Nb of faces within the viscous sub-layer     :      33113
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14925E+01      15   0.26054E-01   0.19965E+00 0.12987E+02 
c  Velocity[X]                                     ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14920E+01      15   0.25597E-01   0.18929E+00 0.12654E+02 
c  Velocity[X]                                      0.54734E-01 
c  Velocity[Y]                                      0.66182E-01 
c  Velocity[Z]                                      0.68372E-01 
c  Pressure     0.73493E-02     301   0.28976E-01   0.95588E-01 0.51314E+00 
c  k            0.16822E-01      12   0.11968E-03   0.48845E-04 0.23147E+02 
c  epsilon      0.45646E+02      10   0.42367E-03   0.22091E+04 0.86140E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -1.126e-05                             9
a  epsilon               -0.055196                            10
a  Local Time Step      4.2278e-08                        223881


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8897          3.3687         0.27185        0.048977
v  Velocity[Y]             -4.2687           4.056         0.14243         0.11843
v  Velocity[Z]             -6.5247          5.2357       -0.092487     -0.00045297
v  ǁVelocityǁ            0.0002312          7.3798         0.77456         0.98686
v  Pressure                -4487.5          9074.3          5803.1          4931.6
v  k                    2.1923e-08         0.40886       0.0025445       0.0047239
v  epsilon              3.5296e-05          7499.3          5.9177          1.9391
v  TurbVisc             2.3621e-13         0.11253        0.001289       0.0045351
v  CourantNb             0.0015345          582.45          4.7684           1.334
v  FourierNb              0.033091      2.3653e+05          22.193         0.40987
v  total_pressure       4.9551e+05      5.0907e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17327       0.0012778       0.0018418


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0331      2.3711e+05          26.961          1.7438


 TIME FOR THE TIME STEP               89:        0.64615E+02

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


 INSTANT    0.900000000E+00   TIME STEP NUMBER              90
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46 Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.263192359E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442505393E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74542E+00 0.14516E+01
   Friction velocity        uet   :  0.56452E-02 0.30672E+01
   Friction velocity        uk    :  0.56348E-02 0.30672E+01
   Dimensionless distance   yplus :  0.38104E-03 0.75823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        609
   Nb of faces within the viscous sub-layer     :      33106
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14917E+01      16   0.26350E-01   0.18520E+00 0.12511E+02 
c  Velocity[X]                                      0.52946E-01 
c  Velocity[Y]                                      0.65585E-01 
c  Velocity[Z]                                      0.66665E-01 
c  Pressure     0.71041E-02     377   0.28155E-01   0.92630E-01 0.56439E+00 
c  k            0.16821E-01       9   0.15406E-03   0.33495E-04 0.19260E+02 
c  epsilon      0.45708E+02       9   0.99275E-03   0.28264E+04 0.97162E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1119e-05                             8
a  epsilon               -0.051134                            12
a  Local Time Step      4.2278e-08                        224307


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8858          3.4009         0.27217        0.049001
v  Velocity[Y]             -4.1554          4.0555         0.14163         0.11843
v  Velocity[Z]             -6.4986          5.1979       -0.093139     -0.00047163
v  ǁVelocityǁ           0.00018376          7.3895         0.77627         0.98694
v  Pressure                -4500.8          9076.4          5801.7          4931.4
v  k                    2.8406e-08         0.40789       0.0025501       0.0047237
v  epsilon              4.1061e-05          7471.7          5.9507          1.9407
v  TurbVisc             2.3681e-13         0.11253       0.0012299        0.004525
v  CourantNb            0.00041609          799.56            4.78          1.3347
v  FourierNb              0.033136      2.3653e+05          22.182         0.40863
v  total_pressure        4.955e+05      5.0908e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17327       0.0012753        0.001839


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98962      2.3733e+05          26.962          1.7433


 TIME FOR THE TIME STEP               91:        0.63359E+02

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


 INSTANT    0.920000000E+00   TIME STEP NUMBER              92
 ==========================================Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.263192359E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442505393E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74542E+00 0.14516E+01
   Friction velocity        uet   :  0.56452E-02 0.30672E+01
   Friction velocity        uk    :  0.56348E-02 0.30672E+01
   Dimensionless distance   yplus :  0.38104E-03 0.75823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        609
   Nb of faces within the viscous sub-layer     :      33106
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14917E+01      16   0.26350E-01   0.18520E+00 0.12511E+02 
c  Velocity[X]                                      0.52946E-01 
c  Velocity[Y]                                      0.65585E-01 
c  Velocity[Z]                                      0.66665E-01 
c  Pressure     0.71041E-02     377   0.28155E-01   0.92630E-01 0.56439E+00 
c  k            0.16821E-01       9   0.15406E-03   0.33495E-04 0.19260E+02 
c  epsilon      0.45708E+02       9   0.99275E-03   0.28264E+04 0.97162E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1119e-05                             8
a  epsilon               -0.051134                            12
a  Local Time Step      4.2278e-08                        224307


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8858          3.4009         0.27217        0.049001
v  Velocity[Y]             -4.1554          4.0555         0.14163         0.11843
v  Velocity[Z]             -6.4986          5.1979       -0.093139     -0.00047163
v  ǁVelocityǁ           0.00018376          7.3895         0.77627         0.98v  Velocity[Z]             -6.4712          5.2024       -0.093416     -0.00048771
v  ǁVelocityǁ           0.00017193          7.3557         0.77705           0.987
v  Pressure                -4496.4            9076          5801.8          4932.3
v  k                    2.8207e-08         0.40736       0.0025503       0.0047235
v  epsilon              4.8182e-05            7464          5.9384          1.9407
v  TurbVisc             2.3721e-13         0.11253       0.0012007       0.0045202
v  CourantNb             0.0020909          532.08          4.7841          1.3351
v  FourierNb              0.033159      2.3653e+05          22.178         0.40817
v  total_pressure        4.955e+05      5.0908e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17327       0.0012746        0.001838


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98662      2.3706e+05          26.962          1.7432


 TIME FOR THE TIME STEP               92:        0.80256E+02

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


 INSTANT    0.930000000E+00   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.271946848E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442486135E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.77089E+00 0.14532E+01
   Friction velocity        uet   :  0.64584E-02 0.42035E+01
   Friction velocity        uk    :  0.64464E-02 0.42035E+01
   Dimensionless distance   yplus :  0.26588E-03 0.75788E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        607
   Nb of faces within the viscous sub-layer     :      33094
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14915E+01      16   0.25514E-01   0.19028E+00 0.12714E+02 
c  Velocity[X]                                      0.54699E-01 
c  Velocity[Y]                                      0.67745E-01 
c  Velocity[Z]                                      0.67838E-01 
c  Pressure     0.71429E-02     314   0.28188E-01   0.93198E-01 0.51152E+00 
c  k            0.16822E-01      10   0.11508E-03   0.31332E-04 0.18637E+02 
c  epsilon      0.45632E+02       8   0.37773E-03   0.19172E+04 0.80248E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1727e-05                             7
a  epsilon               -0.063006                            14
a  Local Time Step      4.2278e-08                        224631


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v v  Velocity[Z]             -6.4712          5.2024       -0.093416     -0.00048771
v  ǁVelocityǁ           0.00017193          7.3557         0.77705           0.987
v  Pressure                -4496.4            9076          5801.8          4932.3
v  k                    2.8207e-08         0.40736       0.0025503       0.0047235
v  epsilon              4.8182e-05            7464          5.9384          1.9407
v  TurbVisc             2.3721e-13         0.11253       0.0012007       0.0045202
v  CourantNb             0.0020909          532.08          4.7841          1.3351
v  FourierNb              0.033159      2.3653e+05          22.178         0.40817
v  total_pressure        4.955e+05      5.0908e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17327       0.0012746        0.001838


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98662      2.3706e+05          26.962          1.7432


 TIME FOR THE TIME STEP               92:        0.76464E+02

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


 INSTANT    0.930000000E+00   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.271946848E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442486135E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.77089E+00 0.14532E+01
   Friction velocity        uet   :  0.64584E-02 0.42035E+01
   Friction velocity        uk    :  0.64464E-02 0.42035E+01
   Dimensionless distance   yplus :  0.26588E-03 0.75788E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        607
   Nb of faces within the viscous sub-layer     :      33094
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14915E+01      16   0.25514E-01   0.19028E+00 0.12714E+02 
c  Velocity[X]                                      0.54699E-01 
c  Velocity[Y]                                      0.67745E-01 
c  Velocity[Z]                                      0.67838E-01 
c  Pressure     0.71429E-02     314   0.28188E-01   0.93198E-01 0.51152E+00 
c  k            0.16822E-01      10   0.11508E-03   0.31332E-04 0.18637E+02 
c  epsilon      0.45632E+02       8   0.37773E-03   0.19172E+04 0.80248E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1727e-05                             7
a  epsilon               -0.063006                            14
a  Local Time Step      4.2278e-08                        224631


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8761          3.3637         0.27259        0.049003
v  Velocity[Y]             -4.1244          4.0509          0.1411         0.11843
v  Velocity[Z]             -6.5241          5.2191        -0.09364     -0.00048913
v  ǁVelocityǁ            0.0001392           7.398         0.77792         0.98706
v  Pressure                -4498.6          9076.8          5801.2          4933.1
v  k                    2.8116e-08         0.40838       0.0025529       0.0047231
v  epsilon              1.4345e-06          7487.1          5.9446          1.9409
v  TurbVisc             2.3768e-13         0.11253       0.0011718       0.0045154
v  CourantNb             0.0006986           423.5          4.7901          1.3354
v  FourierNb              0.033192      2.3653e+05          22.173         0.40774
v  total_pressure        4.955e+05      5.0908e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17327       0.0012736        0.001839


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  ------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.263192359E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442505393E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74542E+00 0.14516E+01
   Friction velocity        uet   :  0.56452E-02 0.30672E+01
   Friction velocity        uk    :  0.56348E-02 0.30672E+01
   Dimensionless distance   yplus :  0.38104E-03 0.75823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        609
   Nb of faces within the viscous sub-layer     :      33106
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14917E+01      16   0.26350E-01   0.18520E+00 0.12511E+02 
c  Velocity[X]                                      0.52946E-01 
c  Velocity[Y]                                      0.65585E-01 
c  Velocity[Z]                                      0.66665E-01 
c  Pressure     0.71041E-02     377   0.28155E-01   0.92630E-01 0.56439E+00 
c  k            0.16821E-01       9   0.15406E-03   0.33495E-04 0-----------------------------------------------------------------------------
c  Velocity     0.14914E+01      17   0.25379E-01   0.18310E+00 0.12445E+02 
c  Velocity[X]                                      0.52103E-01 
c  Velocity[Y]                                      0.63624E-01 
c  Velocity[Z]                                      0.67370E-01 
c  Pressure     0.72038E-02     374   0.28259E-01   0.94089E-01 0.52032E+00 
c  k            0.16822E-01      11   0.88131E-04   0.20808E-04 0.15238E+02 
c  epsilon      0.45583E+02       8   0.29465E-03   0.92629E+03 0.55743E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1623e-05                             8
a  epsilon               -0.048531                            12
a  Local Time Step      4.2278e-08                        224788


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8773          3.3952         0.27277        0.048994
v  Velocity[Y]             -4.1644          4.0429         0.14092          0.1184
v  Velocity[Z]             -6.4501          5.3367       -0.093862     -0.00050117
v  ǁVelocityǁ           0.00024475          7.3419         0.77871         0.98715
v  Pressure                -4513.3          9077.7            5801          4932.7
v  k                    2.8226e-08         0.40686       0.0025521       0.0047226
v  epsilon              4.7247e-05          7451.7          5.9432          1.9406
v  TurbVisc             2.3692e-13         0.11253        0.001145       0.0045107
v  CourantNb             0.0012034          758.87          4.7994          1.3357
v  FourierNb              0.033213      2.3653e+05          22.169         0.40758
v  total_pressure       4.9549e+05      5.0908e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17327       0.0012731       0.0018411


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0332      2.3729e+05          26.968          1.7433


 TIME FOR THE TIME STEP               94:        0.78717E+02

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


 INSTANT    0.950000000E+00   TIME STEP NUMBER              95
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.430682297E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442530280E+00
Free inlet               13         Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442556883E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69582E+00 0.14503E+01
   Friction velocity        uet   :  0.62736E-02 0.51313E+01
   Friction velocity        uk    :  0.63150E-02 0.51313E+01
   Dimensionless distance   yplus :  0.29926E-03 0.75664E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        607
   Nb of faces within the viscous sub-layer     :      33093
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14914E+01      16   0.24896E-01   0.18665E+00 0.12592E+02 
c  Velocity[X]                                      0.53824E-01 
c  Velocity[Y]                                      0.65036E-01 
c  Velocity[Z]                                      0.67786E-01 
c  Pressure     0.69907E-02     426   0.27679E-01   0.91530E-01 0.52355E+00 
c  k            0.16826E-01      10   0.10370E-03   0.31363E-04 0.18620E+02 
c  epsilon      0.45650E+02       9   0.44567E-03   0.19226E+04 0.80261E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ----------v  Velocity[Z]             -6.4712          5.2024       -0.093416     -0.00048771
v  ǁVelocityǁ           0.00017193          7.3557         0.77705           0.987
v  Pressure                -4496.4            9076          5801.8          4932.3
v  k                    2.8207e-08         0.40736       0.0025503       0.0047235
v  epsilon              4.8182e-05            7464          5.9384          1.9407
v  TurbVisc             2.3721e-13         0.11253       0.0012007       0.0045202
v  CourantNb             0.0020909          532.08          4.7841          1.3351
v  FourierNb              0.033159      2.3653e+05          22.178         0.40817
v  total_pressure        4.955e+05      5.0908e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17327       0.0012746        0.001838


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98662      2.3706e+05          26.962          1.7432


 TIME FOR THE TIME STEP               92:        0.67628E+02

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


 INSTANT    0.930000000E+00   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.271946848E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442486135E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLSSymmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442556883E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69582E+00 0.14503E+01
   Friction velocity        uet   :  0.62736E-02 0.51313E+01
   Friction velocity        uk    :  0.63150E-02 0.51313E+01
   Dimensionless distance   yplus :  0.29926E-03 0.75664E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        607
   Nb of faces within the viscous sub-layer     :      33093
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14914E+01      16   0.24896E-01   0.18665E+00 0.12592E+02 
c  Velocity[X]                                      0.53824E-01 
c  Velocity[Y]                                      0.65036E-01 
c  Velocity[Z]                                      0.67786E-01 
c  Pressure     0.69907E-02     426   0.27679E-01   0.91530E-01 0.52355E+00 
c  k            0.16826E-01      10   0.10370E-03   0.31363E-04 0.18620E+02 
c  epsilon      0.45650E+02       9   0.44567E-03   0.19226E+04 0.80261E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.2508e-05                             8
a  epsilon               -0.066257                            14
a  Local Time Step      4.2278e-08                        225061


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8796          3.3998         0.27297        0.048993
v  Velocity[Y]             -3.9904          4.0318         0.14075          0.1184
v  Velocity[Z]              -6.476          5.5486       -0.094206     -0.00049878
v  ǁVelocityǁ           0.00018267          7.3664         0.78011         0.98731
v  Pressure                -4503.6          9075.9            5800          4931.1
v  k                    2.8013e-08         0.40729       0.0025535       0.0047224
v  epsilon              4.6695e-05          7458.9          5.9464          1.9433
v  TurbVisc              2.383e-13         0.11253       0.0010922       0.004501v  epsilon              4.4211e-05          7461.1          5.9573           1.943
v  TurbVisc             2.4169e-13         0.11253       0.0010655       0.0044974
v  CourantNb             0.0028224          870.99          4.8114          1.3367
v  FourierNb              0.033167      2.3653e+05          22.157         0.40627
v  total_pressure       4.9548e+05      5.0906e+05      5.0578e+05      5.0492e+05
v  Local Time Step           0.001         0.17327       0.0012708       0.0018388


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.95562       2.374e+05          26.968           1.743


 TIME FOR THE TIME STEP               97:        0.88110E+02

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


 INSTANT    0.980000000E+00   TIME STEP NUMBER              98
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.124516703E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442528976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72453E+00 0.14500E+01
   Friction velocity        uet   :  0.10525E-02 0.42379E+01
   Friction velocity        uk    :  0.10519E-02 0.42379E+01
   Dimensionless distance   yplus :  0.54076E-03 0.75614E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        603
   Nb of faces within the viscous sub-layer     :      33089
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14911E+01      19   0.25129E-01   0.17795E+00 0.12303E+02 
c  Velocity[X]                                      0.51677E-01 
c  Velocity[Y]                                      0.63215E-01 
c  Velocity[Z]                                      0.63060E-01 
c  Pressure     0.70157E-02     395   0.27457E-01   0.91584E-01 0.54578E+00 
c  k            0.16826E-01      10   0.83239E-04   0.27951E-04 0.17677E+02 
c  epsilon      0.45673E+02       8   0.21294E-03   0.75935E+03 0.50436E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.3368e-05                             8
a  epsilon                -0.13712                            15
a  Local Time Step      4.2278e-08                        225256


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8771          3.3789         0.27316        0.048965
v  Velocity[Y]             -4.2277          4.0244          0.1408         0.11844
v  Velocity[Z]             -6.4782          5.6715        -0.09461     -0.00041291
v  ǁVelocityǁ           0.00021487          7.3605         0.78155         0.98739
v v  epsilon              4.4211e-05          7461.1          5.9573           1.943
v  TurbVisc             2.4169e-13         0.11253       0.0010655       0.0044974
v  CourantNb             0.0028224          870.99          4.8114          1.3367
v  FourierNb              0.033167      2.3653e+05          22.157         0.40627
v  total_pressure       4.9548e+05      5.0906e+05      5.0578e+05      5.0492e+05
v  Local Time Step           0.001         0.17327       0.0012708       0.0018388


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.95562       2.374e+05          26.968           1.743


 TIME FOR THE TIME STEP               97:        0.85290E+02

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


 INSTANT    0.980000000E+00   TIME STEP NUMBER              98
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.124516703E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442528976E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72453E+00 0.14500E+01
   Friction velocity        uet   :  0.10525E-02 0.42379E+01
   Friction velocity        uk    :  0.10519E-02 0.42379E+01
   Dimensionless distance   yplus :  0.54076E-03 0.75614E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        603
   Nb of faces within the viscous sub-layer     :      33089
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14911E+01      19   0.25129E-01   0.17795E+00 0.12303E+02 
c  Velocity[X]                                      0.51677E-01 
c  Velocity[Y]                                      0.63215E-01 
c  Velocity[Z]                                      0.63060E-01 
c  Pressure     0.70157E-02     395   0.27457E-01   0.91584E-01 0.54578E+00 
c  k            0.1682c  Velocity[Z]                                      0.62517E-01 
c  Pressure     0.68115E-02     397   0.26666E-01   0.88900E-01 0.57610E+00 
c  k            0.16829E-01      10   0.98651E-04   0.36561E-04 0.20185E+02 
c  epsilon      0.45726E+02       9   0.37340E-03   0.16406E+04 0.74203E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.3529e-05                             9
a  epsilon               -0.092607                            17
a  Local Time Step      4.2278e-08                        225294


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8737          3.3789         0.27316        0.048947
v  Velocity[Y]             -4.1481          4.0332         0.14083         0.11844
v  Velocity[Z]             -6.5108          5.5891       -0.094815     -0.00040907
v  ǁVelocityǁ           0.00014666          7.3818         0.78223         0.98744
v  Pressure                -4533.5          9057.3          5783.1          4918.4
v  k                     2.673e-08          0.4092       0.0025502       0.0047221
v  epsilon              4.2275e-05          7506.1           5.951          1.9451
v  TurbVisc             2.3514e-13         0.11253       0.0010133       0.0044892
v  CourantNb            0.00053788          552.11          4.8194          1.3373
v  FourierNb              0.033176      2.3653e+05          22.149         0.40533
v  total_pressure       4.9547e+05      5.0906e+05      5.0578e+05      5.0492e+05
v  Local Time Step           0.001         0.17327       0.0012697       0.0018341


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97466      2.3708e+05          26.969          1.7426


 TIME FOR THE TIME STEP               99:        0.72179E+Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442556883E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69582E+00 0.14503E+01
   Friction velocity        uet   :  0.62736E-02 0.51313E+01
   Friction velocity        uk    :  0.63150E-02 0.51313E+01
   Dimensionless distance   yplus :  0.29926E-03 0.75664E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        607
   Nb of faces within the viscous sub-layer     :      33093
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14914E+01      16   0.24896E-01   0.18665E+00 0.12592E+02 
c  Velocity[X]                                      0.53824E-01 
c  Velocity[Y]                                      0.65036E-01 
c  Velocity[Z]                                      0.67786E-01 
c  Pressure     0.69907E-02     426   0.27679E-01   0.91530E-01 0.52355E+00 
c  k            0.16826E-01      10   0.10370E-03   0.31363E-04 0.18620E+02 
c  epsilon      0.45650E+02       9   0.44567E-03   0.19226E+04 0.80261E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.2508e-05                             8
a  epsilon               -0.066257                            14
a  Local Time Step      4.2278e-08                        225061


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8796          3.3998         0.27297        0.048993
v  Velocity[Y]             -3.9904          4.0318         0.14075          0.1184
v  Velocity[Z]              -6.476          5.5486       -0.094206     -0.00049878
v  ǁVelocityǁ           0.00018267          7.3664         0.78011         0.98731
v  Pressure                -4503.6          9075.9            5800          4931.1
v  k                    2.8013e-08         0.40729       0.0025535       0.0047224
v  epsilon              4.6695e-05          7458.9          5.9464          1.9433
v  TurbVisc              2.383e-13         0.11253       0.0010922       0.0045019
v  CourantNb                     0          339.36           4.805          1.3364
v  FourierNb              0.033193      2.3653e+05          22.161         0.40659
v  total_pressure        4.955e+05      5.0908e+05       5.058e+05      5.0493e+05
v  Local Time Step           0.001         0.17327       0.0012714       0.0018381


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9917      2.3686e+05          26.966           1.743


 TIME FOR THE TIME STEP               96:        0.75570E+02

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


 INSTANT    0.970000000E+00   TIME STEP NUMBER              97
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.332973391E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442541624E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74036E+00 0.14514E+01
   Friction velocity        uet   :  0.68432E-02 0.39714E+01
   Friction velocity        uk    :  0.68454E-02 0.39714E+01
   DimensiFree surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75757E+00 0.14500E+01
   Friction velocity        uet   :  0.59232E-02 0.34315E+01
   Friction velocity        uk    :  0.59114E-02 0.34315E+01
   Dimensionless distance   yplus :  0.29203E-03 0.75408E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        613
   Nb of faces within the viscous sub-layer     :      33088
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14964E+01      17   0.24933E-01   0.11769E+03 0.20243E+03 
c  Velocity[X]                                      0.60954E+01 
c  Velocity[Y]                                      0.11514E+02 
c  Velocity[Z]                                      0.10008E+03 
c  Pressure     0.27099E-01    2371   0.16743E+01   0.33537E+00 0.68733E+03 
c  k            0.19793E-01      19   0.11909E-02   0.13611E-02 0.10233E+03 
c  epsilon      0.45730E+02      18   0.55619E-03   0.28062E+04 0.99085E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.3254e-07                             2
a  epsilon                -0.03428                            11
a  Local Time Step      4.2278e-08                        225479


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.3288           6.901         0.34602        0.072525
v  Velocity[Y]             -5.8036          6.6118         0.22927         0.16963
v  Velocity[Z]             -8.4088          6.9732        -0.11538       0.0010509
v  ǁVelocityǁ           0.00076491          9.5165         0.96787          1.3579
v  Pressure                 228.99      1.2455e+05           66588           63802
v  k                    2.7716e-08           0.389        0.002622       0.0049467
v  epsilon              6.3184e-05          7220.5          6.2034          1.9914
v  TurbVisc             2.4107e-13         0.11253      0.00096251       0.0044813
v  CourantNb             0.0025629          788.66          4.8286          1.3378
v  FourierNb              0.033155      2.3653e+05          22.142         0.40456
v  total_pressure       5.0023e+05      6.2455e+05      5.6659e+05       5.638e+05
v  Local Time Step           0.001         0.17327        0.001269       0.0018333


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0332      2.3732e+05           26.97          1.7423


 TIME FOR THE TIME STEP              101:        0.17739E+03

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


 INSTANT    0.102000000E+01   TIME STEP NUMBER             102
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.146812366E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3 Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75757E+00 0.14500E+01
   Friction velocity        uet   :  0.59232E-02 0.34315E+01
   Friction velocity        uk    :  0.59114E-02 0.34315E+01
   Dimensionless distance   yplus :  0.29203E-03 0.75408E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        613
   Nb of faces within the viscous sub-layer     :      33088
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14964E+01      17   0.24933E-01   0.11769E+03 0.20243E+03 
c  Velocity[X]                                      0.60954E+01 
c  Velocity[Y]                                      0.11514E+02 
c  Velocity[Z]                                      0.10008E+03 
c  Pressure     0.27099E-01    2371   0.16743E+01   0.33537E+00 0.68733E+03 
c  k            0.19793E-01      19   0.11909E-02   0.13611E-02 0.10233E+03 
c  epsilon      0.45730E+02      18   0.55619E-03   0.28062E+04 0.99085E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.3254e-07                             2
a  epsilon                -0.03428                            11
a  Local Time Step      4.2278e-08                        225479


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.3288           6.901         0.34602        0.072525
v  Velocity[Y]             -5.8036          6.6118         0.22927         0.16963
v  Velocity[Z]             -8.4088          6.9732        -0.11538       0.0010509
v  ǁVelocityǁ           0.00076491          9.5165         0.96787          1.3579
v  Pressure                 228.99      1.2455e+05           66588           63802
v  k                    2.7716e-08           0.389        0.002622       0.0049467
v  epsilon              6.3184e-05          7220.5          6.2034          1.9914
v  TurbVisc             2.4107e-13         0.11253      0.00096251       0.0044813
v  CourantNb             0.0025629          788.66          4.8286          1.3378
v  FourierNb              0.033155      2.3653e+05          22.142         0.40456
v  total_pressure       5.0023e+05      6.2455e+05      5.6659e+05      v  total_pressure       5.0017e+05      5.8842e+05      5.4876e+05      5.4586e+05
v  Local Time Step           0.001        0.043071       0.0010516       0.0011602


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6771      2.3654e+05          28.327          1.9013


 TIME FOR THE TIME STEP              102:        0.15459E+03

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


 INSTANT    0.103000000E+01   TIME STEP NUMBER             103
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.368831735E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699700285E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23443E+01 0.19540E+01
   Friction velocity        uet   :  0.18630E-01 0.14558E+02
   Friction velocity        uk    :  0.18549E-01 0.14558E+02
   Dimensionless distance   yplus :  0.83055E-03 0.88056E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2730
   Nb of faces within the viscous sub-layer     :      29649
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35874E+01      29   0.18425E-01   0.48688E+01 0.42143E+02 
c  Velocity[X]                                      0.94254E+00 
c  Velocity[Y]                                      0.17241E+01 
c  Velocity[Z]                                      0.22022E+01 
c  Pressure     0.38368E-01    2997   0.51729E+00   0.37310E+00 0.17000E+04 
c  k            0.30602E-01      17   0.75895E-02   0.36187E-01 0.47598E+03 
c  epsilon      0.24533E+03      12   0.19336E-01   0.20189E+08 0.39729E+04 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0014654                            81
a  epsilon                 -15.377                           112
a  Local Time Step      4.2278e-08                        248083


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.7956          4.5916         0.39384        0.080606
v  Velocity[Y]             -5.4802          6.6649         0.26401         0.19518
v  Velocity[Z]             -9.2132          6.7357        -0.12283     -0.00077525
v  ǁVelocityǁ            0.0011489          10.478          1.0793          1.5503
v  Pressure                -1805.5           28535           18116           15518
v  k                    9.4519e-09         0.54298       0.0037675       0.0059511
v  epsilon              0.00019078           18448          14.225           3.405
v  TurbVisc             2.5999e-13         0.13597      0.00081118       0.0047393
v v  total_pressure       5.0017e+05      5.8842e+05      5.4876e+05      5.4586e+05
v  Local Time Step           0.001        0.043071       0.0010516       0.0011602


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6771      2.3654e+05          28.327          1.9013


 TIME FOR THE TIME STEP              102:        0.16856E+03

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


 INSTANT    0.103000000E+01   TIME STEP NUMBER             103
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.368831735E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699700285E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23443E+01 0.19540E+01
   Friction velocity        uet   :  0.18630E-01 0.14558E+02
   Friction velocity        uk    :  0.18549E-01 0.14558E+02
   Dimensionless distance   yplus :  0.83055E-03 0.88056E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2730
   Nb of faces within the viscous sub-layer     :      29649
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35874E+01      29   0.18425E-01   0.48688E+01 0.42143E+02 
c  Velocity[X]                                      0.94254E+00 
c  Velocity[Y]                                      0.17241E+01 
c  Velocity[Z]                                      0.22022E+01 
c  Pressure     0.38368E-01    2997   0.51729E+00   0.37310E+00 0.17000E+04 
c  k            0.30602E-01      17   0.75895E-02   0.36187E-01 0.47598E+03 
c  epsilon      0.24533E+03      12   0.19336E-01   0.20189E+08 0.39729E+04 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ----------
  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016137                            60
a  epsilon                 -1.6613                            89
a  Local Time Step      4.2278e-08                        246328


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8649          4.7918         0.39641        0.078547
v  Velocity[Y]             -6.1122          7.2063         0.25064         0.18991
v  Velocity[Z]             -9.7646          7.1095        -0.12452      -0.0012506
v  ǁVelocityǁ           0.00065924          11.158          1.0865          1.5213
v  Pressure                 -14325           12201          6031.9          3712.7
v  k                    4.0324e-09         0.80175       0.0040797       0.0061867
v  epsilon              5.3097e-06           32502          17.488          3.5797
v  TurbVisc             2.7728e-13         0.13852       0.0007675       0.0047993
v  CourantNb             0.0027248          2014.4          6.4015          1.6279
v  FourierNb              0.025081      2.3653e+05          21.901         0.30396
v  total_pressure       4.8568e+05       5.122e+05      5.0603e+05      5.0371e+05
v  Local Time Step           0.001        0.052116       0.0010636       0.0011675


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52859      2.3854e+05          28.303          1.9318


 TIME FOR THE TIME STEP              104:        0.15435E+03

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


 INSTANT    0.105000000E+01   TIME STEP NUMBER             105
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.147453267E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699596074E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33839E+01 0.20425E+01
   Friction velocity        uet   :  0.82019E-02 0.16613E+02
   Friction velocity        uk    :  0.81965E-02 0.16613E+02
   Dimensionless distance   yplus :  0.14123E-02 0.88213E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2734
   Nb of faces within the viscous sub-layer     :      29976
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31071E+01      31   0.21476E-01   0.32250E+01 0.35172E+02 
c  Velocity[X]                                      0.63985E+00 
c  Velocity[Y]                                      0.11756E+01 
c  Velocity[Z]                                      0.14095E+01 
c  Pressure     0.42580E-01    1371   0.11876E+00   0.38294E+00 0.20940E+03 
c  k            0.32398E-01      21   0.85362E-03   0.14819E-02 0.91020E+0
  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016137                            60
a  epsilon                 -1.6613                            89
a  Local Time Step      4.2278e-08                        246328


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -1.8649          4.7918         0.39641        0.078547
v  Velocity[Y]             -6.1122          7.2063         0.25064         0.18991
v  Velocity[Z]             -9.7646          7.1095        -0.12452      -0.0012506
v  ǁVelocityǁ           0.00065924          11.158          1.0865          1.5213
v  Pressure                 -14325           12201          6031.9          3712.7
v  k                    4.0324e-09         0.80175       0.0040797       0.0061867
v  epsilon              5.3097e-06           32502          17.488          3.5797
v  TurbVisc             2.7728e-13         0.13852       0.0007675       0.0047993
v  CourantNb             0.0027248          2014.4          6.4015          1.6279
v  FourierNb              0.025081      2.3653e+05          21.901         0.30396
v  total_pressure       4.8568e+05       5.122e+05      5.0603e+05      5.0371e+05
v  Local Time Step           0.001        0.052116       0.0010636       0.0011675


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52859      2.3854e+05          28.303          1.9318


 TIME FOR THE TIME STEP              104:        0.15146E+03

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


 INSTANT    0.105000000E+01   TIME STEP NUMBER             105
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.147453267E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699596074E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33839E+01 0.20425E+01
   Friction velocity        uet   :  0.820------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38354E+01 0.20764E+01
   Friction velocity        uet   :  0.69379E-02 0.15419E+02
   Friction velocity        uk    :  0.69347E-02 0.15419E+02
   Dimensionless distance   yplus :  0.15946E-02 0.87654E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2685
   Nb of faces within the viscous sub-layer     :      30087
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.30736E+01      32   0.22701E-01   0.21564E+01 0.28800E+02 
c  Velocity[X]                                      0.52991E+00 
c  Velocity[Y]                                      0.92899E+00 
c  Velocity[Z]                                      0.69753E+00 
c  Pressure     0.23813E-01    1621   0.96749E-01   0.20815E+00 0.36004E+03 
c  k            0.33028E-01      20   0.53952E-03   0.13334E-02 0.84429E+02 
c  epsilon      0.18959E+03      16   0.11933E-02   0.25795E+06 0.37073E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.7559e-05                             9
a  epsilon                -0.18542                            13
a  Local Time Step      4.2278e-08                        244958


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.0027          5.1161         0.40776        0.078357
v  Velocity[Y]             -7.3273          7.8654         0.23826         0.18603
v  Velocity[Z]              -10.78          7.7854        -0.12375     -0.00027768
v  ǁVelocityǁ           0.00038581          12.002          1.1099          1.5016
v  Pressure                -9571.6           18329           11870          9695.8
v  k                    1.2488e-08         0.76078       0.0044435       0.0064608
v  epsilon               1.561e-05           30027          20.898          3.6598
v  TurbVisc             4.0354e-13         0.14075      0.00072334        0.004945
v  CourantNb             0.0014035          1673.6          6.6688          1.6511
v  FourierNb              0.025072      2.3653e+05          21.922         0.30726
v  total_pressure       4.9043e+05      5.1833e+05      5.1187e+05       5.097e+05
v  Local Time Step           0.001        0.063061       0.0010758       0.0011742


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57195      2.3807e+05          28.591          1.9584


 TIME FOR THE TIME STEP              106:        0.15895E+03

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


 INSTANT    0.107000000E+01   TIME STEP NUMBER             107
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.222213821E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699516196E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
 ------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38354E+01 0.20764E+01
   Friction velocity        uet   :  0.69379E-02 0.15419E+02
   Friction velocity        uk    :  0.69347E-02 0.15419E+02
   Dimensionless distance   yplus :  0.15946E-02 0.87654E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2685
   Nb of faces within the viscous sub-layer     :      30087
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.30736E+01      32   0.22701E-01   0.21564E+01 0.28800E+02 
c  Velocity[X]                                      0.52991E+00 
c  Velocity[Y]                                      0.92899E+00 
c  Velocity[Z]                                      0.69753E+00 
c  Pressure     0.23813E-01    1621   0.96749E-01   0.20815E+00 0.36004E+03 
c  k            0.33028E-01      20   0.53952E-03   0.13334E-02 0.84429E+02 
c  epsilon      0.18959E+03      16   0.11933E-02   0.25795E+06 0.37073E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.7559e-05                             9
a  epsilon                -0.18542                            13
a  Local Time Step      4.2278e-08                        244958


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.0027          5.1161         0.40776        0.078357
v  Velocity[Y]             -7.3273          7.8654         0.23826         0.18603
v  Velocity[Z]              -10.78          7.7854        -0.12375     -0.00027768
v  ǁVelocityǁ           0.00038581          12.002          1.1099          1.5016
v  Pressure                -9571.6           18329           11870          9695.8
v  k                    1.2488e-08         0.76078       0.0044435       0.0064608
v  epsilon               1.561e-05           30027          20.898          3.6598
v  TurbVisc             4.0354e-13         0.14075      0.00072334        0.004945
v  CourantNb             0.0014035          1673.6          6.6688          1.6511
v  FourierNb              0.025072      2.3653e+05          21.922         0.30726
v  total_pressure       4.9043e+05      5.1833e+05      5.1187e+05       5.097e+05
v  Local Time Step           0.001        0.063061       0.0010758       0.0011742


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57195      2.3807e+05          28.591          1.958   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62235      2.3691e+05          28.736            1.97


 TIME FOR THE TIME STEP              107:        0.15514E+03

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


 INSTANT    0.108000000E+01   TIME STEP NUMBER             108
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.124043368E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699758217E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42277E+01 0.21361E+01
   Friction velocity        uet   :  0.11443E-01 0.15892E+02
   Friction velocity        uk    :  0.11441E-01 0.15892E+02
   Dimensionless distance   yplus :  0.11438E-02 0.88122E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2717
   Nb of faces within the viscous sub-layer     :      30076
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31416E+01      29   0.23760E-01   0.17514E+01 0.25573E+02 
c  Velocity[X]                                      0.39753E+00 
c  Velocity[Y]                                      0.74567E+00 
c  Velocity[Z]                                      0.60824E+00 
c  Pressure     0.19911E-01     744   0.67698E-01   0.16516E+00 0.71057E+01 
c  k            0.34462E-01      19   0.33944E-03   0.83973E-03 0.64337E+02 
c  epsilon      0.20345E+03      14   0.85385E-03   0.12392E+06 0.23648E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.2799e-06                             5
a  epsilon               -0.061701                             8
a  Local Time Step      4.2278e-08                        244163


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.136          5.6925         0.42304        0.078472
v  Velocity[Y]              -7.167            7.82         0.24086          0.1875
v  Velocity[Z]             -11.651          8.3984        -0.12356     -1.8844e-05
v  ǁVelocityǁ           0.00031142          13.049          1.1445          1.5174
v  Pressure                -7791.7           21194           13973           11749
v  k                    5.7743e-08         0.77511       0.0047883       0.0066922
v  epsilon              4.8212e-05           31313          23.612          3.8529
v  TurbVisc             4.6376e-13         0.14147      0.00068832       0.0050961
v  CourantNb              0.004916          1628.1          6.9505          1.6712
v  FourierNb              0.025066      2.3653e+05           21.94          0.3095
v  total_pressure       4.9221e+05      5.2119e+05      5.1397e+05      5.1175e+05
v  Local Time Step           0.001        0.062289        0.00108   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62235      2.3691e+05          28.736            1.97


 TIME FOR THE TIME STEP              107:        0.14782E+03

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


 INSTANT    0.108000000E+01   TIME STEP NUMBER             108
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.124043368E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699758217E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42277E+01 0.21361E+01
   Friction velocity        uet   :  0.11443E-01 0.15892E+02
   Friction velocity        uk    :  0.11441E-01 0.15892E+02
   Dimensionless distance   yplus :  0.11438E-02 0.88122E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2717
   Nb of faces within the viscous sub-layer     :      30076
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31416E+01      29   0.23760E-01   0.17514E+01 0.25573E+02 
c  Velocity[X]                                      0.39753E+00 
c  Velocity[Y]                                      0.74567E+00 
c  Velocity[Z]                                      0.60824E+00 
c  Pressure     0.19911E-01     744   0.67698E-01   0.16516E+00 0.71057E+01 
c  k            0.34462E-01      19   0.33944E-03   0.83973E-03 0.64337E+02 
c  epsilon      0.20345E+03      14   0.85385E-03   0.12392E+06 0.23648E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.2799e-06                             5
a  epsilon               -0.061701                             8
a  Local Time Step      4.2278e-08                        244163


  ** Computed fields on cells
  a  epsilon               -0.094877                             8
a  Local Time Step      4.2278e-08                        244073


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.1791           6.076         0.42937        0.078166
v  Velocity[Y]             -7.0702          7.8912         0.24242         0.18766
v  Velocity[Z]             -12.218           8.624        -0.12426     -0.00012696
v  ǁVelocityǁ           0.00019374          13.763          1.1597          1.5221
v  Pressure                  -8318           20339           13447           11246
v  k                    1.4092e-08         0.78138        0.004952       0.0067966
v  epsilon              4.0487e-05           31837          25.141          3.9502
v  TurbVisc             3.4076e-13         0.14162      0.00067451       0.0051689
v  CourantNb             0.0017492          1667.9          7.0892          1.6797
v  FourierNb              0.025064      2.3653e+05          21.948          0.3102
v  total_pressure       4.9168e+05      5.2034e+05      5.1345e+05      5.1125e+05
v  Local Time Step           0.001        0.062641       0.0010901       0.0011688


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5139      2.3735e+05          29.037          1.9899


 TIME FOR THE TIME STEP              109:        0.13242E+03

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


 INSTANT    0.110000000E+01   TIME STEP NUMBER             110
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.367583301E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699566031E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43550E+01 0.21695E+01
   Friction velocity        uet   :  0.78461E-02 0.17190E+02
   Friction velocity        uk    :  0.78435E-02 0.17190E+02
   Dimensionless distance   yplus :  0.21876E-02 0.88543E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2772
   Nb of faces within the viscous sub-layer     :      29988
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31476E+01      31   0.25408E-01   0.15095E+01 0.23566E+02 
c  Velocity[X]                                      0.33629E+00 
c  Velocity[Y]                                      0.65951E+00 
c  Velocity[Z]                                      0.51369E+00 
c  Pressure     0.18078E-01    1328   0.54683E-01   0.14393E+00 0.21458E+02 
c  k            0.35585E-01      21   0.30247E-03   0.69626E-03 0.56841E+02 
c  epsilon      0.20956E+03      15   0.62959E-03   0.10485E+06 0.20268E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.7971e-06                             4
a  epsilon                -0.15041                             3
a  Local Time Step      4.2278e-08                        244054


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.2558          6.0678          0.4343         0.07796
v  Velocity[Y]             -7.1323           7.666         0.24371         0.18764
v  Velocity[Z]             -12.728          8.7971        -0.12546     -0.00025789
v  ǁVelocityǁ            0.0001939          14.223          1.1727          1.5252
v  Pressure                -8608.8           20034           13126           10960
v  k                    8.8457e-09         0.78742       0.0051557       0.0068911
v  epsilon              1.8603e-05           32288          26.966           4.046
v  TurbVisc             4.2541e-13          0.1417      0.00066221       0.0052391
v  CourantNb            0.00027217          1546.7           7.217          1.6874
v  FourierNb              0.025064      2.3653e+05          21.953         0.31093
v  total_pressure       4.9139e+05      5.2003e+05      5.1313e+05      5.1096e+05
v  Local Time Step           0.001        0.068905       0.0010939       0.0011669


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52161      2.3789e+05           29.17          1.9983


 TIME FOR THE TIME STEP              110:        0.14596E+03

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


 INSTANT    0.111000000E+01   TIME STEP NUMBER             111
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.113475762E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699660964E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43486E+01 0.21747E+01
   Friction velocity        uet   :  0.80545E-02 0.17994E+02
   Friction velocity        uk    :  0.80494E-02 0.17994E+02
   Dimensionless distance   yplus :  0.22961E-02 0.88667E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2778
   Nb of faces within the viscous sub-layer     :      29937
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31461E+01      30   0.26074E-01   0.14431E+01 0.22982E+02 
c  Velocity[X]                                      0.32264E+00 
c  Velocity[Y]                                      0.62278E+00 
c  Velocity[Z]                                      0.49765E+00 
c  Pressure     0.18027E-01    1049   0.52106E-01   0.14060E+00 0.36427E+01 
c  k            0.36040E-01      15   0.26295E-03   0.54116E-03 0.49494E+02 
c  epsilon      0.21522E+03      12   0.56392E-03   0.10220E+06 0.19493E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -2.467e-06                             4
a  epsilon               -0.050761                             3
a  Local Time Step      4.2278e-08                        244173


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -2.33          6.1338         0.43873        0.077903
v  Velocity[Y]             -7.2227          7.7298         0.24485         0.18765
v  Velocity[Z]             -11.953          8.8685        -0.12662     -0.00030732
v  ǁVelocityǁ           0.00018761          13.548          1.1839          1.5279
v  Pressure                -8638.5           19968           13060           10921
v  k                    1.7535e-08         0.82469       0.0052417       0.0069762
v  epsilon              2.7125e-05           32336          28.081           4.119
v  TurbVisc             4.7569e-13         0.14174      0.00065069       0.0053066
v  CourantNb             0.0014049          1596.6          7.3255          1.6943
v  FourierNb              0.025064      2.3653e+05          21.958          0.3117
v  total_pressure       4.9136e+05      5.1997e+05      5.1306e+05      5.1092e+05
v  Local Time Step           0.001        0.075796       0.0010973       0.0011658


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64469      2.3765e+05          29.284           2.006


 TIME FOR THE TIME STEP              111:        0.11932E+03

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


 INSTANT    0.112000000E+01   TIME STEP NUMBER             112
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.233402756E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699716348E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47485E+01 0.21850E+01
   Friction velocity        uet   :  0.11906E-01 0.18213E+02
   Friction velocity        uk    :  0.11816E-01 0.18213E+02
   Dimensionless distance   yplus :  0.23240E-02 0.88816E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2777
   Nb of faces within the viscous sub-layer     :      29899
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31471E+01      26   0.26630E-01   0.13541E+01 0.22246E+02 
c  Velocity[X]                                      0.30061E+00 
c  Velocity[Y]                                      0.58117E+00 
c  Velocity[Z]                                      0.47234E+00 
c  Pressure     0.17897E-01     581   0.49899E-01   0.13754E+00 0.23950E+01 
c  k            0.36445E-01      17   0.22589E-03   0.48765E-03 0.46590E+02 
c  epsilon      0.22516E+03      14   0.61749E-03   0.93967E+05 0.18243E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00025529                             9
a  epsilon                 -24.319                            10
a  Local Time Step      4.2278e-08                        244353


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.4119           5.869         0.44217        0.077898
v  Velocity[Y]             -7.2068          7.4143           0.246          0.1877
v  Velocity[Z]             -11.941          8.9374        -0.12793     -0.00027828
v  ǁVelocityǁ           0.00023712          13.386          1.1932          1.5305
v  Pressure                -8621.7           19963           13058           10937
v  k                    6.6862e-08         0.80561       0.0053975       0.0070526
v  epsilon              2.1186e-05           32576          29.028          4.1884
v  TurbVisc             4.9023e-13         0.14177      0.00063995       0.0053713
v  CourantNb             0.0018045            1475          7.4234          1.7003
v  FourierNb              0.025064      2.3653e+05          21.962         0.31246
v  total_pressure       4.9138e+05      5.1996e+05      5.1306e+05      5.1094e+05
v  Local Time Step           0.001        0.083375       0.0011005       0.0011655


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72055      2.3783e+05          29.385          2.0127


 TIME FOR THE TIME STEP              112:        0.94178E+02

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


 INSTANT    0.113000000E+01   TIME STEP NUMBER             113
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.128958245E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699702918E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41526E+01 0.21908E+01
   Friction velocity        uet   :  0.89144E-02 0.18832E+02
   Friction velocity        uk    :  0.89089E-02 0.18832E+02
   Dimensionless distance   yplus :  0.24030E-02 0.88954E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2788
   Nb of faces within the viscous sub-layer     :      29861
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31489E+01      24   0.27433E-01   0.12885E+01 0.21660E+02 
c  Velocity[X]                                      0.29776E+00 
c  Velocity[Y]                                      0.54739E+00 
c  Velocity[Z]                                      0.44333E+00 
c  Pressure     0.17446E-01     582   0.47750E-01   0.13218E+00 0.21312E+01 
c  k            0.36771E-01      15   0.21503E-03   0.49129E-03 0.46344E+02 
c  epsilon      0.22695E+03      13   0.10732E-02   0.11730E+06 0.20013E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.5679e-06                             4
a  epsilon               -0.020453                             3
a  Local Time Step      4.2278e-08                        244577


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.525          5.8752         0.44483         0.07786
v  Velocity[Y]             -7.1568          7.3842         0.24687         0.18782
v  Velocity[Z]             -11.382          8.9451        -0.12956     -0.00024832
v  ǁVelocityǁ           0.00040866          12.893          1.2011          1.5329
v  Pressure                -8620.4           19960           13057           10950
v  k                    5.6256e-08         0.82598       0.0054653       0.0071218
v  epsilon              3.6929e-05           32898           30.07          4.2466
v  TurbVisc             5.0925e-13         0.14178      0.00063047       0.0054329
v  CourantNb            0.00020866          1816.6          7.5026          1.7056
v  FourierNb              0.025065      2.3653e+05          21.964         0.31313
v  total_pressure       4.9138e+05      5.1996e+05      5.1306e+05      5.1095e+05
v  Local Time Step           0.001        0.081573       0.0011033       0.0011652


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.79284        2.38e+05          29.467          2.0187


 TIME FOR THE TIME STEP              113:        0.85987E+02

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


 INSTANT    0.114000000E+01   TIME STEP NUMBER             114
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.132507790E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699661452E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45287E+01 0.21938E+01
   Friction velocity        uet   :  0.69864E-02 0.19164E+02
   Friction velocity        uk    :  0.69816E-02 0.19164E+02
   Dimensionless distance   yplus :  0.24453E-02 0.89107E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2801
   Nb of faces within the viscous sub-layer     :      29817
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31508E+01      23   0.27387E-01   0.12199E+01 0.21043E+02 
c  Velocity[X]                                      0.28836E+00 
c  Velocity[Y]                                      0.49956E+00 
c  Velocity[Z]                                      0.43203E+00 
c  Pressure     0.16924E-01     533   0.45110E-01   0.12662E+00 0.19059E+01 
c  k            0.37041E-01      17   0.20045E-03   0.43019E-03 0.43132E+02 
c  epsilon      0.22438E+03      15   0.59613E-03   0.99953E+05 0.18364E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0021296                             4
a  epsilon                 -24.991                             8
a  Local Time Step      4.2278e-08                        244763


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5998          5.8757         0.44667        0.077784
v  Velocity[Y]             -7.0708          7.2569         0.24721         0.18792
v  Velocity[Z]             -11.678          8.9359        -0.13175     -0.00024995
v  ǁVelocityǁ           0.00040593          13.128           1.208          1.5351
v  Pressure                -8619.8           19965           13054           10961
v  k                    4.9087e-08         0.82939       0.0055663       0.0071862
v  epsilon              2.6077e-05           32696          30.753           4.299
v  TurbVisc             6.6895e-13         0.14179      0.00062098       0.0054914
v  CourantNb             0.0003293          1937.7          7.5651          1.7104
v  FourierNb              0.025066      2.3653e+05          21.965         0.31378
v  total_pressure       4.9138e+05      5.1996e+05      5.1305e+05      5.1096e+05
v  Local Time Step           0.001        0.045032       0.0011057       0.0011646


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.79818      2.3804e+05           29.53          2.0242


 TIME FOR THE TIME STEP              114:        0.82552E+02

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


 INSTANT    0.115000000E+01   TIME STEP NUMBER             115
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.155011706E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699699995E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39554E+01 0.21923E+01
   Friction velocity        uet   :  0.52888E-02 0.17589E+02
   Friction velocity        uk    :  0.52850E-02 0.17589E+02
   Dimensionless distance   yplus :  0.22443E-02 0.89245E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2812
   Nb of faces within the viscous sub-layer     :      29777
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31526E+01      24   0.27967E-01   0.11874E+01 0.20729E+02 
c  Velocity[X]                                      0.28188E+00 
c  Velocity[Y]                                      0.48590E+00 
c  Velocity[Z]                                      0.41966E+00 
c  Pressure     0.16500E-01     448   0.43016E-01   0.12208E+00 0.16471E+01 
c  k            0.37270E-01      15   0.19975E-03   0.41378E-03 0.42022E+02 
c  epsilon      0.22070E+03      13   0.62096E-03   0.71279E+05 0.15358E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.3969e-07                             1
a  epsilon               -0.014309                             3
a  Local Time Step      4.2278e-08                        244979


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6731          5.8988         0.44808        0.077783
v  Velocity[Y]             -6.9651          7.2228         0.24691         0.18791
v  Velocity[Z]             -11.305          8.9088        -0.13419     -0.00032118
v  ǁVelocityǁ           0.00042273          12.821          1.2141          1.5372
v  Pressure                -8623.1           19967           13053           10964
v  k                    8.8461e-08         0.83884       0.0056228       0.0072445
v  epsilon              4.9644e-05           32821          31.302          4.3435
v  TurbVisc             3.4636e-13          0.1418      0.00061209       0.0055468
v  CourantNb            0.00030928          1563.9          7.6143          1.7149
v  FourierNb              0.025068      2.3653e+05          21.966         0.31439
v  total_pressure       4.9138e+05      5.1997e+05      5.1305e+05      5.1096e+05
v  Local Time Step           0.001         0.03278       0.0011078       0.0011653


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67643      2.3792e+05           29.58          2.0293


 TIME FOR THE TIME STEP              115:        0.79244E+02

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


 INSTANT    0.116000000E+01   TIME STEP NUMBER             116
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.107974056E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699744593E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44297E+01 0.21865E+01
   Friction velocity        uet   :  0.76999E-02 0.16782E+02
   Friction velocity        uk    :  0.76971E-02 0.16782E+02
   Dimensionless distance   yplus :  0.21414E-02 0.89365E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2814
   Nb of faces within the viscous sub-layer     :      29750
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31541E+01      24   0.27910E-01   0.11583E+01 0.20437E+02 
c  Velocity[X]                                      0.27170E+00 
c  Velocity[Y]                                      0.47039E+00 
c  Velocity[Z]                                      0.41617E+00 
c  Pressure     0.16035E-01     483   0.40715E-01   0.11769E+00 0.16212E+01 
c  k            0.37468E-01      16   0.18359E-03   0.39639E-03 0.40775E+02 
c  epsilon      0.21717E+03      13   0.62508E-03   0.74689E+05 0.15586E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012657                             2
a  epsilon                 -28.564                             8
a  Local Time Step      4.2278e-08                        245171


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7341          5.9692         0.44885        0.077793
v  Velocity[Y]             -6.8997           7.208         0.24621         0.18783
v  Velocity[Z]             -11.448          8.8781        -0.13711     -0.00040124
v  ǁVelocityǁ           0.00049551          12.941          1.2198           1.539
v  Pressure                -8603.4           19968           13051           10964
v  k                    9.9972e-08         0.84505       0.0056981       0.0072969
v  epsilon              5.2764e-05           32345          32.013          4.3812
v  TurbVisc             4.7695e-13          0.1418      0.00060422       0.0055991
v  CourantNb                     0          1443.4          7.6552          1.7191
v  FourierNb              0.025069      2.3653e+05          21.966         0.31494
v  total_pressure        4.914e+05      5.1997e+05      5.1305e+05      5.1096e+05
v  Local Time Step           0.001        0.024064       0.0011095       0.0011665


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64257      2.3732e+05          29.621           2.034


 TIME FOR THE TIME STEP              116:        0.83218E+02

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


 INSTANT    0.117000000E+01   TIME STEP NUMBER             117
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.670747472E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699791377E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42870E+01 0.21874E+01
   Friction velocity        uet   :  0.70547E-02 0.14706E+02
   Friction velocity        uk    :  0.70521E-02 0.14706E+02
   Dimensionless distance   yplus :  0.18765E-02 0.89483E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2822
   Nb of faces within the viscous sub-layer     :      29731
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31556E+01      24   0.28006E-01   0.11259E+01 0.20123E+02 
c  Velocity[X]                                      0.26229E+00 
c  Velocity[Y]                                      0.45605E+00 
c  Velocity[Z]                                      0.40760E+00 
c  Pressure     0.15606E-01     518   0.38941E-01   0.11354E+00 0.20074E+01 
c  k            0.37633E-01      13   0.19680E-03   0.34455E-03 0.37908E+02 
c  epsilon      0.21584E+03      11   0.61606E-03   0.50523E+05 0.12752E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.6931e-07                             1
a  epsilon               -0.069267                             7
a  Local Time Step      4.2277e-08                        245384


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7341          5.9379         0.44943        0.077773
v  Velocity[Y]             -6.8619          7.2701         0.24533         0.18773
v  Velocity[Z]             -11.247          8.8225        -0.14048       -0.000478
v  ǁVelocityǁ           0.00061641          12.803          1.2255          1.5408
v  Pressure                -8627.6           19973           13048           10963
v  k                    1.0314e-07         0.84632       0.0057604       0.0073442
v  epsilon              5.7549e-05           32695          32.618          4.4112
v  TurbVisc             5.0831e-13         0.14181      0.00059753       0.0056485
v  CourantNb             0.0021472          1127.9          7.6921          1.7231
v  FourierNb              0.025071      2.3653e+05          21.966         0.31546
v  total_pressure       4.9137e+05      5.1997e+05      5.1305e+05      5.1096e+05
v  Local Time Step           0.001        0.021112        0.001111       0.0011686


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72996      2.3683e+05          29.658          2.0386


 TIME FOR THE TIME STEP              117:        0.80280E+02

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


 INSTANT    0.118000000E+01   TIME STEP NUMBER             118
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.208372591E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699741604E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44757E+01 0.21737E+01
   Friction velocity        uet   :  0.99470E-02 0.13009E+02
   Friction velocity        uk    :  0.99416E-02 0.13009E+02
   Dimensionless distance   yplus :  0.16599E-02 0.89600E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2814
   Nb of faces within the viscous sub-layer     :      29694
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31564E+01      23   0.27714E-01   0.11156E+01 0.19977E+02 
c  Velocity[X]                                      0.26236E+00 
c  Velocity[Y]                                      0.44388E+00 
c  Velocity[Z]                                      0.40936E+00 
c  Pressure     0.15247E-01     555   0.37456E-01   0.11058E+00 0.16383E+01 
c  k            0.37786E-01      15   0.17460E-03   0.32591E-03 0.36444E+02 
c  epsilon      0.21275E+03      10   0.44681E-03   0.41452E+05 0.11497E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.1458e-05                             2
a  epsilon                 -12.455                             9
a  Local Time Step      4.2277e-08                        245571


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5712          5.8838         0.44956        0.077726
v  Velocity[Y]             -6.7707          7.3043         0.24453         0.18763
v  Velocity[Z]              -11.21          8.7953        -0.14385     -0.00052036
v  ǁVelocityǁ           0.00059473          12.739          1.2307          1.5423
v  Pressure                -8577.9           19978           13046           10966
v  k                     1.006e-08         0.85183       0.0058105       0.0073901
v  epsilon              6.2865e-05           31716           32.97           4.445
v  TurbVisc             5.2237e-13         0.14181      0.00059172       0.0056951
v  CourantNb                     0          1126.6          7.7343           1.727
v  FourierNb              0.025072      2.3653e+05          21.966         0.31586
v  total_pressure       4.9142e+05      5.1998e+05      5.1305e+05      5.1097e+05
v  Local Time Step           0.001        0.022823       0.0011122       0.0011711


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70804      2.3659e+05            29.7          2.0429


 TIME FOR THE TIME STEP              118:        0.87840E+02

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


 INSTANT    0.119000000E+01   TIME STEP NUMBER             119
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.289150059E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699757246E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43627E+01 0.21738E+01
   Friction velocity        uet   :  0.97502E-02 0.10944E+02
   Friction velocity        uk    :  0.96956E-02 0.10944E+02
   Dimensionless distance   yplus :  0.13777E-02 0.89709E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2824
   Nb of faces within the viscous sub-layer     :      29662
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31575E+01      26   0.27561E-01   0.10700E+01 0.19546E+02 
c  Velocity[X]                                      0.26259E+00 
c  Velocity[Y]                                      0.41092E+00 
c  Velocity[Z]                                      0.39649E+00 
c  Pressure     0.15398E-01     467   0.37397E-01   0.11119E+00 0.17143E+01 
c  k            0.37935E-01      13   0.47814E-03   0.30133E-03 0.35165E+02 
c  epsilon      0.21635E+03      11   0.54479E-03   0.33247E+05 0.10216E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                -0.24637                            10
a  Local Time Step      4.2277e-08                        245809


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5893          5.8932         0.44966        0.077702
v  Velocity[Y]               -6.82          7.3563         0.24391          0.1875
v  Velocity[Z]             -11.019          8.7429        -0.14711     -0.00049319
v  ǁVelocityǁ           0.00070351          12.551           1.236          1.5439
v  Pressure                -8527.5           19988           13043           10967
v  k                     1.207e-08         0.85345       0.0058579       0.0074307
v  epsilon              9.6896e-06           32308          33.504          4.4676
v  TurbVisc             5.1896e-13         0.14181      0.00058654        0.005739
v  CourantNb             0.0022019          1043.4          7.7726          1.7307
v  FourierNb              0.025074      2.3653e+05          21.965         0.31633
v  total_pressure       4.9147e+05      5.1999e+05      5.1304e+05      5.1097e+05
v  Local Time Step           0.001        0.025105       0.0011132       0.0011742


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69661      2.3702e+05          29.738           2.047


 TIME FOR THE TIME STEP              119:        0.81933E+02

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


 INSTANT    0.120000000E+01   TIME STEP NUMBER             120
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.344212035E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699670652E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42958E+01 0.21601E+01
   Friction velocity        uet   :  0.44076E-02 0.10432E+02
   Friction velocity        uk    :  0.43997E-02 0.10432E+02
   Dimensionless distance   yplus :  0.11940E-02 0.89621E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2820
   Nb of faces within the viscous sub-layer     :      29663
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31581E+01      23   0.28481E-01   0.10648E+01 0.19475E+02 
c  Velocity[X]                                      0.24740E+00 
c  Velocity[Y]                                      0.40867E+00 
c  Velocity[Z]                                      0.40871E+00 
c  Pressure     0.15323E-01     566   0.37001E-01   0.10992E+00 0.15749E+01 
c  k            0.38063E-01      11   0.12316E-03   0.20037E-03 0.28534E+02 
c  epsilon      0.21878E+03      12   0.37430E-03   0.33858E+05 0.10278E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -8.2258                            16
a  Local Time Step      4.2277e-08                        246102


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6291          5.9232         0.44963        0.077667
v  Velocity[Y]             -6.8403           7.364         0.24367         0.18737
v  Velocity[Z]             -11.095          8.7126        -0.15008     -0.00041568
v  ǁVelocityǁ           0.00031567          12.637          1.2411          1.5453
v  Pressure                -8467.4           19998           13043           10970
v  k                    1.0646e-07         0.85206        0.005884       0.0074676
v  epsilon              7.4339e-05           31443          33.868          4.4867
v  TurbVisc             5.2125e-13         0.14181      0.00058133       0.0057806
v  CourantNb             0.0018486          1057.4           7.814          1.7342
v  FourierNb              0.025075      2.3653e+05          21.964         0.31665
v  total_pressure       4.9153e+05         5.2e+05      5.1304e+05      5.1097e+05
v  Local Time Step           0.001        0.027616       0.0011139       0.0011777


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43024      2.3722e+05          29.778          2.0508


 TIME FOR THE TIME STEP              120:        0.83309E+02

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


 INSTANT    0.121000000E+01   TIME STEP NUMBER             121
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.317239439E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699580397E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41722E+01 0.21580E+01
   Friction velocity        uet   :  0.10953E-01 0.98773E+01
   Friction velocity        uk    :  0.10947E-01 0.98773E+01
   Dimensionless distance   yplus :  0.10883E-02 0.89802E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2819
   Nb of faces within the viscous sub-layer     :      29642
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31584E+01      23   0.27668E-01   0.10586E+01 0.19413E+02 
c  Velocity[X]                                      0.25519E+00 
c  Velocity[Y]                                      0.39436E+00 
c  Velocity[Z]                                      0.40902E+00 
c  Pressure     0.15681E-01     861   0.37129E-01   0.11178E+00 0.36104E+01 
c  k            0.38176E-01      14   0.14914E-03   0.19421E-03 0.28001E+02 
c  epsilon      0.22147E+03      13   0.56523E-03   0.33943E+05 0.10253E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00054801                            10
a  epsilon                 -6.1325                            18
a  Local Time Step      4.2277e-08                        246365


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6009          5.8296         0.44988        0.077663
v  Velocity[Y]             -6.9317          7.4276         0.24375         0.18728
v  Velocity[Z]             -10.936          8.6875        -0.15301     -0.00043124
v  ǁVelocityǁ           0.00082814          12.423          1.2465          1.5467
v  Pressure                -8404.6           20063           13091           11014
v  k                    1.0715e-07         0.85204       0.0059097       0.0075022
v  epsilon               7.848e-05           31752          33.981          4.5055
v  TurbVisc             5.1979e-13         0.14181      0.00057644       0.0058196
v  CourantNb             0.0006939          1177.9           7.851          1.7375
v  FourierNb              0.025077      2.3653e+05          21.962         0.31698
v  total_pressure        4.916e+05      5.2006e+05      5.1309e+05      5.1101e+05
v  Local Time Step           0.001        0.030377       0.0011142       0.0011813


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75756      2.3725e+05          29.813          2.0545


 TIME FOR THE TIME STEP              121:        0.97136E+02

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


 INSTANT    0.122000000E+01   TIME STEP NUMBER             122
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.326716721E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699550823E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42180E+01 0.21497E+01
   Friction velocity        uet   :  0.83774E-02 0.96114E+01
   Friction velocity        uk    :  0.83728E-02 0.96114E+01
   Dimensionless distance   yplus :  0.98213E-03 0.89639E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2817
   Nb of faces within the viscous sub-layer     :      29616
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31593E+01      24   0.27717E-01   0.10148E+01 0.18983E+02 
c  Velocity[X]                                      0.24656E+00 
c  Velocity[Y]                                      0.36894E+00 
c  Velocity[Z]                                      0.39928E+00 
c  Pressure     0.15072E-01     440   0.35339E-01   0.10681E+00 0.12468E+01 
c  k            0.38288E-01      13   0.18411E-03   0.33250E-03 0.36650E+02 
c  epsilon      0.22408E+03      12   0.56131E-03   0.82598E+05 0.15771E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.5445e-05                             2
a  epsilon                  -8.317                            18
a  Local Time Step      4.2277e-08                        246722


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6029          5.7416         0.45018        0.077655
v  Velocity[Y]             -6.9564          7.4811         0.24421         0.18724
v  Velocity[Z]             -10.836          8.6812        -0.15605     -0.00049166
v  ǁVelocityǁ           0.00075323          12.313          1.2519          1.5481
v  Pressure                -8354.4           20075           13091           11018
v  k                    4.1205e-08         0.85319       0.0059568       0.0075366
v  epsilon              8.2126e-05           31166          34.502          4.5419
v  TurbVisc               5.23e-13         0.14181       0.0005716       0.0058564
v  CourantNb            0.00047996          1174.1          7.8902          1.7407
v  FourierNb              0.025079      2.3653e+05           21.96         0.31708
v  total_pressure       4.9165e+05      5.2007e+05      5.1309e+05      5.1102e+05
v  Local Time Step           0.001        0.033415       0.0011142       0.0011849


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76536      2.3703e+05           29.85          2.0578


 TIME FOR THE TIME STEP              122:        0.81926E+02

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


 INSTANT    0.123000000E+01   TIME STEP NUMBER             123
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.629928865E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699570509E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40933E+01 0.21438E+01
   Friction velocity        uet   :  0.85925E-02 0.90378E+01
   Friction velocity        uk    :  0.85878E-02 0.90378E+01
   Dimensionless distance   yplus :  0.82790E-03 0.89535E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2820
   Nb of faces within the viscous sub-layer     :      29598
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31600E+01      25   0.27782E-01   0.10026E+01 0.18840E+02 
c  Velocity[X]                                      0.23801E+00 
c  Velocity[Y]                                      0.37097E+00 
c  Velocity[Z]                                      0.39360E+00 
c  Pressure     0.15413E-01     870   0.35290E-01   0.10857E+00 0.22869E+01 
c  k            0.38382E-01      13   0.15664E-03   0.28041E-03 0.33443E+02 
c  epsilon      0.22623E+03      11   0.67576E-03   0.98810E+05 0.17170E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021969                             1
a  epsilon                 -0.1066                            17
a  Local Time Step      4.2277e-08                        247066


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5966          5.7044         0.45076        0.077702
v  Velocity[Y]             -6.9636          7.4692         0.24496         0.18722
v  Velocity[Z]              -10.78          8.6774        -0.15883     -0.00057482
v  ǁVelocityǁ           0.00084983          12.116          1.2575          1.5496
v  Pressure                -8367.9           20115           13112           11043
v  k                      6.42e-08           0.851       0.0059756       0.0075663
v  epsilon              8.4686e-05           31356           34.75          4.5584
v  TurbVisc             5.2384e-13         0.14181      0.00056737       0.0058912
v  CourantNb             0.0060246          1151.3          7.9271          1.7437
v  FourierNb               0.02508      2.3653e+05          21.957         0.31716
v  total_pressure       4.9163e+05      5.2012e+05      5.1311e+05      5.1104e+05
v  Local Time Step           0.001        0.036756       0.0011138       0.0011881


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69182      2.3693e+05          29.884          2.0609


 TIME FOR THE TIME STEP              123:        0.10426E+03

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


 INSTANT    0.124000000E+01   TIME STEP NUMBER             124
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.134991449E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699621948E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40501E+01 0.21342E+01
   Friction velocity        uet   :  0.10324E-01 0.87480E+01
   Friction velocity        uk    :  0.10318E-01 0.87480E+01
   Dimensionless distance   yplus :  0.62322E-03 0.89803E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2823
   Nb of faces within the viscous sub-layer     :      29569
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31608E+01      28   0.27975E-01   0.98194E+00 0.18638E+02 
c  Velocity[X]                                      0.22819E+00 
c  Velocity[Y]                                      0.36480E+00 
c  Velocity[Z]                                      0.38894E+00 
c  Pressure     0.15193E-01     420   0.34333E-01   0.10600E+00 0.10777E+01 
c  k            0.38466E-01      13   0.13792E-03   0.32182E-03 0.35800E+02 
c  epsilon      0.22595E+03      11   0.50147E-03   0.72839E+05 0.14759E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002672                             5
a  epsilon                 -10.544                            23
a  Local Time Step      4.2277e-08                        247433


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6034          5.7059         0.45131        0.077726
v  Velocity[Y]             -7.0572          7.4348         0.24585         0.18722
v  Velocity[Z]             -10.749           8.674        -0.16133     -0.00062455
v  ǁVelocityǁ           0.00086788          12.211          1.2629           1.551
v  Pressure                -8371.7           20129           13110           11046
v  k                    7.8953e-08         0.85036       0.0059903       0.0075966
v  epsilon              8.6803e-05           30749          34.634          4.5853
v  TurbVisc             5.2483e-13         0.14181      0.00056337        0.005924
v  CourantNb            0.00026486          1123.3          7.9661          1.7466
v  FourierNb              0.025083      2.3653e+05          21.954          0.3172
v  total_pressure       4.9163e+05      5.2013e+05      5.1311e+05      5.1105e+05
v  Local Time Step           0.001        0.030106       0.0011134       0.0011908


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.594      2.3674e+05           29.92          2.0638


 TIME FOR THE TIME STEP              124:        0.78675E+02

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


 INSTANT    0.125000000E+01   TIME STEP NUMBER             125
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.199471288E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699671767E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40245E+01 0.21327E+01
   Friction velocity        uet   :  0.12149E-01 0.78898E+01
   Friction velocity        uk    :  0.12138E-01 0.78898E+01
   Dimensionless distance   yplus :  0.80009E-03 0.89560E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2818
   Nb of faces within the viscous sub-layer     :      29532
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31615E+01      25   0.27977E-01   0.96860E+00 0.18497E+02 
c  Velocity[X]                                      0.23103E+00 
c  Velocity[Y]                                      0.35014E+00 
c  Velocity[Z]                                      0.38743E+00 
c  Pressure     0.15093E-01     647   0.33829E-01   0.10495E+00 0.12446E+01 
c  k            0.38529E-01      18   0.20714E-03   0.27516E-03 0.33085E+02 
c  epsilon      0.22127E+03      12   0.69642E-03   0.71484E+05 0.14573E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022267                             6
a  epsilon                -0.12915                            19
a  Local Time Step      4.2277e-08                        247844


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6168          5.6181         0.45204        0.077762
v  Velocity[Y]             -7.1017          7.3564         0.24666          0.1872
v  Velocity[Z]             -10.722          8.6784        -0.16382     -0.00065754
v  ǁVelocityǁ           0.00085242          12.012          1.2684          1.5525
v  Pressure                -8402.9           20140           13103           11049
v  k                    1.0752e-07         0.84785       0.0060593       0.0076242
v  epsilon              5.2994e-05           31153          35.417           4.609
v  TurbVisc             5.3468e-13         0.14181      0.00055979        0.005955
v  CourantNb              0.007398          1020.6          8.0041          1.7495
v  FourierNb              0.025085      2.3653e+05          21.951         0.31721
v  total_pressure        4.916e+05      5.2014e+05       5.131e+05      5.1105e+05
v  Local Time Step           0.001        0.033117       0.0011126       0.0011941


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61268      2.3693e+05          29.955          2.0667


 TIME FOR THE TIME STEP              125:        0.95255E+02

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


 INSTANT    0.126000000E+01   TIME STEP NUMBER             126
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.269348344E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699726060E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40001E+01 0.21250E+01
   Friction velocity        uet   :  0.12897E-01 0.80495E+01
   Friction velocity        uk    :  0.12885E-01 0.80495E+01
   Dimensionless distance   yplus :  0.77113E-03 0.89744E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2807
   Nb of faces within the viscous sub-layer     :      29516
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31621E+01      25   0.28571E-01   0.93379E+00 0.18153E+02 
c  Velocity[X]                                      0.22453E+00 
c  Velocity[Y]                                      0.33230E+00 
c  Velocity[Z]                                      0.37696E+00 
c  Pressure     0.14941E-01     441   0.32905E-01   0.10356E+00 0.10889E+01 
c  k            0.38599E-01      14   0.17081E-03   0.22527E-03 0.29886E+02 
c  epsilon      0.22335E+03      10   0.39768E-03   0.43010E+05 0.11331E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019709                             8
a  epsilon                 -6.8583                            16
a  Local Time Step      4.2277e-08                        248297


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6347           5.583         0.45283        0.077785
v  Velocity[Y]             -7.0821          7.2858         0.24751         0.18718
v  Velocity[Z]             -10.642             8.7        -0.16621     -0.00073435
v  ǁVelocityǁ           0.00061375          11.983          1.2734          1.5538
v  Pressure                -8406.6           20152           13100           11050
v  k                    1.0914e-07          0.8446       0.0060348       0.0076496
v  epsilon              7.9234e-05           30465          34.945          4.6214
v  TurbVisc             5.1342e-13         0.14181      0.00055665       0.0059842
v  CourantNb             0.0034841           884.2          8.0468          1.7522
v  FourierNb              0.025088      2.3653e+05          21.948         0.31713
v  total_pressure       4.9159e+05      5.2015e+05       5.131e+05      5.1105e+05
v  Local Time Step           0.001        0.036429       0.0011118       0.0011973


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68985      2.3662e+05          29.994          2.0694


 TIME FOR THE TIME STEP              126:        0.69531E+02

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


 INSTANT    0.127000000E+01   TIME STEP NUMBER             127
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.114823948E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699773546E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39337E+01 0.21279E+01
   Friction velocity        uet   :  0.11288E-01 0.80275E+01
   Friction velocity        uk    :  0.11197E-01 0.80275E+01
   Dimensionless distance   yplus :  0.76826E-03 0.89434E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2811
   Nb of faces within the viscous sub-layer     :      29485
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31627E+01      24   0.28290E-01   0.93502E+00 0.18141E+02 
c  Velocity[X]                                      0.22796E+00 
c  Velocity[Y]                                      0.33830E+00 
c  Velocity[Z]                                      0.36876E+00 
c  Pressure     0.15088E-01     754   0.33247E-01   0.10420E+00 0.26175E+01 
c  k            0.38657E-01      12   0.13227E-03   0.20751E-03 0.28597E+02 
c  epsilon      0.22460E+03      11   0.44679E-03   0.44945E+05 0.11507E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015506                             6
a  epsilon                -0.16677                            15
a  Local Time Step      4.2277e-08                        248738


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6599          5.5442         0.45357        0.077784
v  Velocity[Y]             -7.2457           7.217         0.24824         0.18716
v  Velocity[Z]              -10.61          8.7201        -0.16822     -0.00074374
v  ǁVelocityǁ           0.00085118          11.885          1.2782           1.555
v  Pressure                -8489.2           20121           13058           11017
v  k                    1.0877e-07         0.84419       0.0060865       0.0076727
v  epsilon              7.4778e-05           31044          35.583          4.6407
v  TurbVisc             5.2616e-13         0.14181      0.00055306       0.0060116
v  CourantNb             0.0033838          742.91          8.0827           1.755
v  FourierNb              0.025091      2.3653e+05          21.944         0.31708
v  total_pressure       4.9151e+05      5.2012e+05      5.1306e+05      5.1102e+05
v  Local Time Step           0.001        0.040072        0.001111       0.0012008


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72458      2.3655e+05          30.026          2.0721


 TIME FOR THE TIME STEP              127:        0.95495E+02

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


 INSTANT    0.128000000E+01   TIME STEP NUMBER             128
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.751671869E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699747433E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39099E+01 0.21146E+01
   Friction velocity        uet   :  0.97578E-02 0.86214E+01
   Friction velocity        uk    :  0.96807E-02 0.86214E+01
   Dimensionless distance   yplus :  0.54417E-03 0.89148E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2812
   Nb of faces within the viscous sub-layer     :      29446
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31625E+01      27   0.28050E-01   0.91079E+00 0.17921E+02 
c  Velocity[X]                                      0.22442E+00 
c  Velocity[Y]                                      0.33878E+00 
c  Velocity[Z]                                      0.34758E+00 
c  Pressure     0.14718E-01     696   0.32380E-01   0.10169E+00 0.14917E+01 
c  k            0.38678E-01      13   0.22028E-03   0.24510E-03 0.31011E+02 
c  epsilon      0.21623E+03      11   0.40217E-03   0.48903E+05 0.12087E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00054905                             8
a  epsilon                 -6.6353                            12
a  Local Time Step      4.2277e-08                        249192


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6801          5.5733         0.45448         0.07777
v  Velocity[Y]             -7.2505          7.1316         0.24881         0.18707
v  Velocity[Z]             -10.596          8.7012        -0.17033      -0.0007449
v  ǁVelocityǁ           0.00083854          11.913          1.2827          1.5561
v  Pressure                -8555.1           20115           13037           11004
v  k                    1.1073e-07         0.83608       0.0061018        0.007696
v  epsilon               7.115e-05           30214           35.52          4.6556
v  TurbVisc               5.21e-13         0.14181      0.00055049       0.0060376
v  CourantNb             0.0051796          725.31          8.1169          1.7578
v  FourierNb              0.025094      2.3653e+05           21.94         0.31709
v  total_pressure       4.9144e+05      5.2011e+05      5.1304e+05        5.11e+05
v  Local Time Step           0.001        0.044079       0.0011102       0.0012044


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56264       2.367e+05          30.057          2.0749


 TIME FOR THE TIME STEP              128:        0.82059E+02

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


 INSTANT    0.129000000E+01   TIME STEP NUMBER             129
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.909441686E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699688140E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38897E+01 0.21243E+01
   Friction velocity        uet   :  0.11929E-01 0.92079E+01
   Friction velocity        uk    :  0.11822E-01 0.92079E+01
   Dimensionless distance   yplus :  0.42375E-03 0.89425E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2810
   Nb of faces within the viscous sub-layer     :      29414
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31625E+01      23   0.28468E-01   0.88845E+00 0.17676E+02 
c  Velocity[X]                                      0.21634E+00 
c  Velocity[Y]                                      0.32366E+00 
c  Velocity[Z]                                      0.34845E+00 
c  Pressure     0.14478E-01     413   0.31601E-01   0.99812E-01 0.11150E+01 
c  k            0.38728E-01      12   0.22757E-03   0.20709E-03 0.28494E+02 
c  epsilon      0.21833E+03       9   0.34049E-03   0.36549E+05 0.10383E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010818                             8
a  epsilon                 -10.436                            15
a  Local Time Step      4.2277e-08                        249593


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6967          5.6018         0.45549        0.077788
v  Velocity[Y]             -7.5903          7.0072         0.24929         0.18704
v  Velocity[Z]             -10.615          8.7356         -0.1721     -0.00071564
v  ǁVelocityǁ            0.0008374          11.962           1.287          1.5572
v  Pressure                -8607.5           20134           13035           11008
v  k                    1.1227e-07         0.83513       0.0061162       0.0077166
v  epsilon              6.8356e-05           31048          35.521          4.6715
v  TurbVisc             5.3031e-13         0.14181      0.00054799       0.0060621
v  CourantNb             0.0015944          789.12          8.1476          1.7605
v  FourierNb              0.025097      2.3653e+05          21.937         0.31715
v  total_pressure       4.9139e+05      5.2013e+05      5.1304e+05      5.1101e+05
v  Local Time Step           0.001        0.048487       0.0011095       0.0012077


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55978      2.3663e+05          30.084          2.0776


 TIME FOR THE TIME STEP              129:        0.76553E+02

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


 INSTANT    0.130000000E+01   TIME STEP NUMBER             130
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.189764498E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699620270E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39095E+01 0.21199E+01
   Friction velocity        uet   :  0.74158E-02 0.10067E+02
   Friction velocity        uk    :  0.74094E-02 0.10067E+02
   Dimensionless distance   yplus :  0.61569E-03 0.88898E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2805
   Nb of faces within the viscous sub-layer     :      29382
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31623E+01      24   0.29089E-01   0.87976E+00 0.17591E+02 
c  Velocity[X]                                      0.21432E+00 
c  Velocity[Y]                                      0.31801E+00 
c  Velocity[Z]                                      0.34743E+00 
c  Pressure     0.14305E-01     515   0.31153E-01   0.98302E-01 0.11733E+01 
c  k            0.38751E-01      13   0.16544E-03   0.22693E-03 0.29790E+02 
c  epsilon      0.21487E+03      13   0.68152E-03   0.60576E+05 0.13325E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011719                             8
a  epsilon                -0.26613                            10
a  Local Time Step      4.2277e-08                        249972


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7139          5.5848         0.45633        0.077836
v  Velocity[Y]             -7.6272          6.9204         0.24936         0.18699
v  Velocity[Z]             -10.665          8.7491        -0.17384     -0.00069151
v  ǁVelocityǁ           0.00084868          11.908          1.2909          1.5583
v  Pressure                -8656.3           20157           13034           11013
v  k                    1.0894e-07         0.83452       0.0061678        0.007736
v  epsilon              6.5859e-05           30366          36.487          4.6881
v  TurbVisc             5.3625e-13         0.14181      0.00054574       0.0060852
v  CourantNb             0.0027757          904.52          8.1758          1.7629
v  FourierNb              0.025101      2.3653e+05          21.934         0.31709
v  total_pressure       4.9134e+05      5.2016e+05      5.1303e+05      5.1101e+05
v  Local Time Step           0.001        0.053335       0.0011088       0.0012099


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61114      2.3654e+05           30.11            2.08


 TIME FOR THE TIME STEP              130:        0.89338E+02

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


 INSTANT    0.131000000E+01   TIME STEP NUMBER             131
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.336985738E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699599623E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39437E+01 0.21278E+01
   Friction velocity        uet   :  0.10699E-01 0.97732E+01
   Friction velocity        uk    :  0.10690E-01 0.97732E+01
   Dimensionless distance   yplus :  0.70823E-03 0.89051E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2796
   Nb of faces within the viscous sub-layer     :      29350
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31624E+01      23   0.27930E-01   0.86523E+00 0.17442E+02 
c  Velocity[X]                                      0.21298E+00 
c  Velocity[Y]                                      0.31429E+00 
c  Velocity[Z]                                      0.33796E+00 
c  Pressure     0.14269E-01     377   0.31014E-01   0.97805E-01 0.96623E+00 
c  k            0.38782E-01      12   0.12262E-03   0.16715E-03 0.25508E+02 
c  epsilon      0.21474E+03      11   0.41216E-03   0.37666E+05 0.10552E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001756                             4
a  epsilon                  -20.81                            15
a  Local Time Step      4.2277e-08                        250371


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7266          5.5511         0.45735        0.077845
v  Velocity[Y]             -7.5678          6.8697         0.24915         0.18697
v  Velocity[Z]             -10.645          8.7892         -0.1752     -0.00063811
v  ǁVelocityǁ           0.00088824          11.937          1.2947          1.5592
v  Pressure                -8685.9           20177           13034           11014
v  k                    1.1048e-07          0.8325       0.0061531       0.0077536
v  epsilon              6.3756e-05           31150          35.793          4.6895
v  TurbVisc             5.1456e-13         0.14181      0.00054323       0.0061068
v  CourantNb             0.0032053          897.27          8.1992          1.7654
v  FourierNb              0.025105      2.3653e+05          21.932         0.31708
v  total_pressure       4.9131e+05      5.2018e+05      5.1303e+05      5.1101e+05
v  Local Time Step           0.001        0.058669       0.0011082        0.001212


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73892      2.3657e+05          30.131          2.0825


 TIME FOR THE TIME STEP              131:        0.58617E+02

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


 INSTANT    0.132000000E+01   TIME STEP NUMBER             132
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.508229440E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699561797E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39360E+01 0.21209E+01
   Friction velocity        uet   :  0.73867E-02 0.92263E+01
   Friction velocity        uk    :  0.74253E-02 0.92263E+01
   Dimensionless distance   yplus :  0.67364E-03 0.88333E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2790
   Nb of faces within the viscous sub-layer     :      29325
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31621E+01      24   0.28229E-01   0.84318E+00 0.17202E+02 
c  Velocity[X]                                      0.20798E+00 
c  Velocity[Y]                                      0.31096E+00 
c  Velocity[Z]                                      0.32424E+00 
c  Pressure     0.14073E-01     421   0.30502E-01   0.96191E-01 0.10544E+01 
c  k            0.38789E-01      12   0.12070E-03   0.19617E-03 0.27591E+02 
c  epsilon      0.21142E+03       9   0.37198E-03   0.43182E+05 0.11274E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021015                             4
a  epsilon                 -10.961                            11
a  Local Time Step      4.2277e-08                        250714


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7458          5.5809         0.45802        0.077845
v  Velocity[Y]             -7.3532          6.8034         0.24863         0.18697
v  Velocity[Z]             -10.661            8.78        -0.17656     -0.00067724
v  ǁVelocityǁ            0.0008319          11.962           1.298          1.5602
v  Pressure                -8694.8           20202           13033           11017
v  k                    1.1285e-07         0.83247       0.0061699       0.0077706
v  epsilon              6.2168e-05           30467          36.004          4.6978
v  TurbVisc             5.2885e-13         0.14181      0.00054098       0.0061275
v  CourantNb             0.0022744          890.21          8.2215          1.7677
v  FourierNb              0.025109      2.3653e+05          21.929         0.31711
v  total_pressure       4.9131e+05       5.202e+05      5.1303e+05      5.1102e+05
v  Local Time Step           0.001        0.064536       0.0011076       0.0012144


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.715      2.3685e+05          30.151          2.0848


 TIME FOR THE TIME STEP              132:        0.69492E+02

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


 INSTANT    0.133000000E+01   TIME STEP NUMBER             133
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.159210288E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699564928E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39531E+01 0.21261E+01
   Friction velocity        uet   :  0.15345E-01 0.88291E+01
   Friction velocity        uk    :  0.15330E-01 0.88291E+01
   Dimensionless distance   yplus :  0.73778E-03 0.87774E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2794
   Nb of faces within the viscous sub-layer     :      29294
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31619E+01      21   0.28887E-01   0.83680E+00 0.17126E+02 
c  Velocity[X]                                      0.20222E+00 
c  Velocity[Y]                                      0.29261E+00 
c  Velocity[Z]                                      0.34197E+00 
c  Pressure     0.14218E-01     378   0.30425E-01   0.96842E-01 0.10235E+01 
c  k            0.38815E-01      14   0.13661E-03   0.16058E-03 0.24962E+02 
c  epsilon      0.21188E+03      15   0.67063E-03   0.34093E+05 0.10030E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022756                             4
a  epsilon               -0.098411                             7
a  Local Time Step      4.2277e-08                        250987


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7563           5.584         0.45865        0.077858
v  Velocity[Y]             -7.6618           6.734          0.2479           0.187
v  Velocity[Z]             -10.671          8.7731        -0.17805     -0.00073641
v  ǁVelocityǁ           0.00077764          11.998          1.3014          1.5612
v  Pressure                -8720.6           20235           13032           11021
v  k                    1.1168e-07         0.82814       0.0062021       0.0077871
v  epsilon              6.0791e-05           31005           36.61          4.7077
v  TurbVisc             5.4012e-13         0.14181      0.00053904       0.0061469
v  CourantNb            0.00058704          879.61          8.2373            1.77
v  FourierNb              0.025113      2.3653e+05          21.927         0.31716
v  total_pressure       4.9128e+05      5.2023e+05      5.1303e+05      5.1102e+05
v  Local Time Step           0.001        0.070989       0.0011071       0.0012172


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81667      2.3699e+05          30.164          2.0871


 TIME FOR THE TIME STEP              133:        0.69416E+02

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


 INSTANT    0.134000000E+01   TIME STEP NUMBER             134
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.223014546E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699595466E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39676E+01 0.21202E+01
   Friction velocity        uet   :  0.76330E-02 0.80279E+01
   Friction velocity        uk    :  0.76245E-02 0.80279E+01
   Dimensionless distance   yplus :  0.58610E-03 0.86915E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2788
   Nb of faces within the viscous sub-layer     :      29270
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31618E+01      20   0.29187E-01   0.83398E+00 0.17105E+02 
c  Velocity[X]                                      0.20520E+00 
c  Velocity[Y]                                      0.28204E+00 
c  Velocity[Z]                                      0.34674E+00 
c  Pressure     0.14115E-01     378   0.30203E-01   0.96046E-01 0.99447E+00 
c  k            0.38834E-01      12   0.11429E-03   0.17224E-03 0.25829E+02 
c  epsilon      0.21145E+03      11   0.39727E-03   0.33334E+05 0.99264E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019563                             4
a  epsilon                 -19.512                             8
a  Local Time Step      4.2277e-08                        251264


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.783          5.6139         0.45934        0.077865
v  Velocity[Y]             -7.9879          6.7136           0.247           0.187
v  Velocity[Z]             -10.675          8.8084        -0.17935     -0.00082104
v  ǁVelocityǁ           0.00081748          11.993          1.3048          1.5621
v  Pressure                -8755.3           20264           13030           11023
v  k                    1.1138e-07         0.82983       0.0061852       0.0078024
v  epsilon              5.9974e-05           30358          36.107          4.7113
v  TurbVisc             5.2916e-13         0.14181      0.00053689       0.0061652
v  CourantNb            0.00078008          863.77          8.2596          1.7722
v  FourierNb              0.025117      2.3653e+05          21.925         0.31715
v  total_pressure       4.9124e+05      5.2026e+05      5.1303e+05      5.1102e+05
v  Local Time Step           0.001        0.078088       0.0011067       0.0012188


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85182      2.3713e+05          30.185          2.0894


 TIME FOR THE TIME STEP              134:        0.74081E+02

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


 INSTANT    0.135000000E+01   TIME STEP NUMBER             135
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.212028920E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699629735E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39618E+01 0.21332E+01
   Friction velocity        uet   :  0.13493E-01 0.76068E+01
   Friction velocity        uk    :  0.13382E-01 0.76068E+01
   Dimensionless distance   yplus :  0.67640E-03 0.86257E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2792
   Nb of faces within the viscous sub-layer     :      29232
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31614E+01      20   0.28489E-01   0.82297E+00 0.16986E+02 
c  Velocity[X]                                      0.20911E+00 
c  Velocity[Y]                                      0.29284E+00 
c  Velocity[Z]                                      0.32102E+00 
c  Pressure     0.13938E-01     337   0.29709E-01   0.94581E-01 0.82319E+00 
c  k            0.38862E-01      16   0.11612E-03   0.14943E-03 0.24028E+02 
c  epsilon      0.21315E+03      10   0.35105E-03   0.14264E+05 0.64623E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.5212e-05                             2
a  epsilon                -0.11982                             5
a  Local Time Step      4.2277e-08                        251514


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7898          5.5897         0.45997        0.077902
v  Velocity[Y]             -8.1131          6.7091         0.24603         0.18703
v  Velocity[Z]             -10.712          8.8355        -0.18053     -0.00094754
v  ǁVelocityǁ           0.00073476          12.013           1.308           1.563
v  Pressure                -8789.5           20295           13028           11025
v  k                    5.2002e-08         0.83411       0.0062133       0.0078186
v  epsilon              5.9552e-05           31348          36.369          4.7232
v  TurbVisc             5.4463e-13         0.14181      0.00053499       0.0061824
v  CourantNb              0.003024          984.67          8.2814          1.7744
v  FourierNb              0.025121      2.3653e+05          21.924         0.31726
v  total_pressure       4.9121e+05      5.2029e+05      5.1303e+05      5.1103e+05
v  Local Time Step           0.001        0.085897       0.0011065         0.00122


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90158      2.3731e+05          30.205          2.0917


 TIME FOR THE TIME STEP              135:        0.53253E+02

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


 INSTANT    0.136000000E+01   TIME STEP NUMBER             136
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.354657216E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699715451E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40019E+01 0.21288E+01
   Friction velocity        uet   :  0.14002E-01 0.60023E+01
   Friction velocity        uk    :  0.13754E-01 0.60023E+01
   Dimensionless distance   yplus :  0.55545E-03 0.85337E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2795
   Nb of faces within the viscous sub-layer     :      29220
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31613E+01      24   0.28713E-01   0.79814E+00 0.16726E+02 
c  Velocity[X]                                      0.20403E+00 
c  Velocity[Y]                                      0.27500E+00 
c  Velocity[Z]                                      0.31911E+00 
c  Pressure     0.13725E-01     339   0.28923E-01   0.92827E-01 0.84477E+00 
c  k            0.38874E-01      11   0.12102E-03   0.14547E-03 0.23727E+02 
c  epsilon      0.21148E+03      12   0.43028E-03   0.22534E+05 0.81368E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.9463e-05                             2
a  epsilon                   -7.45                             7
a  Local Time Step      4.2277e-08                        251724


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.8028          5.6188         0.46049         0.07795
v  Velocity[Y]             -7.9344          6.7503         0.24496         0.18707
v  Velocity[Z]             -10.776          8.8113        -0.18182      -0.0010633
v  ǁVelocityǁ           0.00069871          12.044          1.3112           1.564
v  Pressure                -8779.9           20323           13025           11027
v  k                    8.5621e-09         0.83164       0.0062168       0.0078323
v  epsilon              4.7044e-05           30644          36.377          4.7282
v  TurbVisc             5.2891e-13         0.14181      0.00053326       0.0061986
v  CourantNb             0.0011172           948.9          8.2993          1.7765
v  FourierNb              0.025125      2.3653e+05          21.923         0.31722
v  total_pressure       4.9122e+05      5.2032e+05      5.1302e+05      5.1103e+05
v  Local Time Step           0.001        0.094487       0.0011062       0.0012205


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73614      2.3748e+05          30.222          2.0937


 TIME FOR THE TIME STEP              136:        0.67150E+02

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


 INSTANT    0.137000000E+01   TIME STEP NUMBER             137
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.221376061E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699818666E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40501E+01 0.21370E+01
   Friction velocity        uet   :  0.10013E-01 0.58044E+01
   Friction velocity        uk    :  0.99608E-02 0.58044E+01
   Dimensionless distance   yplus :  0.70172E-03 0.84419E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2790
   Nb of faces within the viscous sub-layer     :      29187
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31612E+01      20   0.28670E-01   0.79005E+00 0.16637E+02 
c  Velocity[X]                                      0.19591E+00 
c  Velocity[Y]                                      0.27741E+00 
c  Velocity[Z]                                      0.31673E+00 
c  Pressure     0.13602E-01     403   0.28495E-01   0.91947E-01 0.74909E+00 
c  k            0.38916E-01      12   0.20833E-03   0.21006E-03 0.28489E+02 
c  epsilon      0.21552E+03      12   0.89330E-03   0.52571E+05 0.12329E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -1.274e-05                             2
a  epsilon                -0.11849                             4
a  Local Time Step      4.2277e-08                        251935


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.8178          5.6175         0.46103        0.077988
v  Velocity[Y]             -7.6438          6.7428         0.24388         0.18716
v  Velocity[Z]             -10.751          8.8203        -0.18292       -0.001172
v  ǁVelocityǁ           0.00055516          12.095          1.3143          1.5649
v  Pressure                -8775.7           20350           13020           11028
v  k                    1.2249e-08         0.83237       0.0062406       0.0078471
v  epsilon              1.3666e-05           31405          36.647          4.7447
v  TurbVisc             5.3752e-13         0.14181      0.00053141       0.0062139
v  CourantNb             0.0037875          996.21          8.3188          1.7786
v  FourierNb              0.025128      2.3653e+05          21.921         0.31718
v  total_pressure       4.9122e+05      5.2035e+05      5.1302e+05      5.1103e+05
v  Local Time Step           0.001         0.10394        0.001106       0.0012209


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.93871      2.3753e+05           30.24          2.0958


 TIME FOR THE TIME STEP              137:        0.71813E+02

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


 INSTANT    0.138000000E+01   TIME STEP NUMBER             138
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.138785069E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699929824E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40328E+01 0.21324E+01
   Friction velocity        uet   :  0.12421E-01 0.61101E+01
   Friction velocity        uk    :  0.12406E-01 0.61101E+01
   Dimensionless distance   yplus :  0.53757E-03 0.83331E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2783
   Nb of faces within the viscous sub-layer     :      29171
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31612E+01      19   0.28325E-01   0.76941E+00 0.16419E+02 
c  Velocity[X]                                      0.19306E+00 
c  Velocity[Y]                                      0.27085E+00 
c  Velocity[Z]                                      0.30549E+00 
c  Pressure     0.13316E-01     341   0.28082E-01   0.90188E-01 0.75765E+00 
c  k            0.38940E-01      12   0.92010E-04   0.13676E-03 0.22966E+02 
c  epsilon      0.21721E+03      10   0.54282E-03   0.16067E+05 0.68313E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.7502e-07                             2
a  epsilon                 -7.9186                             3
a  Local Time Step      4.2277e-08                        252074


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.8292          5.6252          0.4615        0.078025
v  Velocity[Y]             -7.9531          6.7225         0.24292         0.18719
v  Velocity[Z]             -10.758          8.8022        -0.18393      -0.0012966
v  ǁVelocityǁ           0.00059372          12.084          1.3173          1.5658
v  Pressure                  -8781           20373           13016           11028
v  k                    7.8781e-08         0.83262       0.0062373       0.0078602
v  epsilon              5.8646e-05           30824          36.431           4.748
v  TurbVisc             5.2723e-13         0.14181      0.00052953       0.0062282
v  CourantNb             0.0037736           985.8          8.3389          1.7806
v  FourierNb              0.025131      2.3653e+05           21.92          0.3172
v  total_pressure       4.9122e+05      5.2037e+05      5.1302e+05      5.1103e+05
v  Local Time Step           0.001         0.11433       0.0011057       0.0012206


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76794      2.3752e+05          30.259          2.0978


 TIME FOR THE TIME STEP              138:        0.72277E+02

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


 INSTANT    0.139000000E+01   TIME STEP NUMBER             139
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.141694699E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.700065752E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40414E+01 0.21375E+01
   Friction velocity        uet   :  0.90318E-02 0.59562E+01
   Friction velocity        uk    :  0.90102E-02 0.59562E+01
   Dimensionless distance   yplus :  0.48312E-03 0.82563E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2783
   Nb of faces within the viscous sub-layer     :      29146
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31612E+01      25   0.29024E-01   0.76661E+00 0.16386E+02 
c  Velocity[X]                                      0.19451E+00 
c  Velocity[Y]                                      0.27465E+00 
c  Velocity[Z]                                      0.29745E+00 
c  Pressure     0.13453E-01    1521   0.28309E-01   0.91262E-01 0.96894E+01 
c  k            0.38951E-01      11   0.95185E-04   0.10369E-03 0.19650E+02 
c  epsilon      0.21624E+03       9   0.33231E-03   0.10162E+05 0.53723E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.3197e-07                             1
a  epsilon                -0.11422                             2
a  Local Time Step      4.2277e-08                        252251


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.832          5.6375         0.46199        0.078063
v  Velocity[Y]             -7.9583          6.7111         0.24184         0.18719
v  Velocity[Z]             -10.847          8.7865        -0.18459      -0.0010358
v  ǁVelocityǁ           0.00033501          12.104            1.32          1.5663
v  Pressure                -8951.2           20227           12843           10892
v  k                    3.0532e-08         0.83363       0.0062558       0.0078719
v  epsilon              6.0046e-05           31356          36.612          4.7546
v  TurbVisc             5.4384e-13         0.14181      0.00052765       0.0062415
v  CourantNb             0.0056388          994.46          8.3574          1.7826
v  FourierNb              0.025134      2.3653e+05          21.919         0.31698
v  total_pressure       4.9105e+05      5.2023e+05      5.1284e+05      5.1089e+05
v  Local Time Step           0.001         0.12576       0.0011054       0.0012188


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7554      2.3739e+05          30.277          2.0996


 TIME FOR THE TIME STEP              139:        0.14588E+03

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


 INSTANT    0.140000000E+01   TIME STEP NUMBER             140
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.272705465E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699753700E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41161E+01 0.21373E+01
   Friction velocity        uet   :  0.12049E-01 0.63608E+01
   Friction velocity        uk    :  0.12034E-01 0.63608E+01
   Dimensionless distance   yplus :  0.81165E-03 0.82553E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2785
   Nb of faces within the viscous sub-layer     :      29124
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31591E+01      21   0.28489E-01   0.76563E+00 0.16378E+02 
c  Velocity[X]                                      0.20552E+00 
c  Velocity[Y]                                      0.26373E+00 
c  Velocity[Z]                                      0.29637E+00 
c  Pressure     0.13293E-01     311   0.28324E-01   0.91296E-01 0.74430E+00 
c  k            0.38961E-01      11   0.12892E-03   0.12145E-03 0.21473E+02 
c  epsilon      0.21599E+03      10   0.81494E-03   0.29337E+05 0.91991E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.6776e-07                             1
a  epsilon                 -6.5423                             4
a  Local Time Step      4.2277e-08                        252418


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.841          5.6856         0.46221        0.078066
v  Velocity[Y]              -7.667           6.695         0.24084         0.18722
v  Velocity[Z]             -10.843          8.8171        -0.18522     -0.00078464
v  ǁVelocityǁ           0.00046169          12.271          1.3226          1.5667
v  Pressure                -8939.8           20247           12842           10896
v  k                    1.1198e-07         0.83487        0.006274       0.0078834
v  epsilon               6.051e-05           30993          36.835          4.7632
v  TurbVisc             5.5095e-13         0.14181       0.0005258        0.006254
v  CourantNb             0.0033956          872.18          8.3733          1.7843
v  FourierNb              0.025136      2.3653e+05          21.918         0.31694
v  total_pressure       4.9106e+05      5.2025e+05      5.1284e+05       5.109e+05
v  Local Time Step           0.001         0.13834       0.0011051        0.001218


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78108      2.3706e+05          30.292          2.1012


 TIME FOR THE TIME STEP              140:        0.73110E+02

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


 INSTANT    0.141000000E+01   TIME STEP NUMBER             141
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.669417951E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699487571E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41283E+01 0.21432E+01
   Friction velocity        uet   :  0.11441E-01 0.59322E+01
   Friction velocity        uk    :  0.11347E-01 0.59322E+01
   Dimensionless distance   yplus :  0.75696E-03 0.82539E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2788
   Nb of faces within the viscous sub-layer     :      29097
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31581E+01      20   0.28334E-01   0.74366E+00 0.16130E+02 
c  Velocity[X]                                      0.20396E+00 
c  Velocity[Y]                                      0.25482E+00 
c  Velocity[Z]                                      0.28487E+00 
c  Pressure     0.13150E-01     751   0.28328E-01   0.91303E-01 0.52637E+01 
c  k            0.38978E-01      11   0.14435E-03   0.18541E-03 0.26701E+02 
c  epsilon      0.21655E+03       9   0.56555E-03   0.41759E+05 0.10974E+03 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.2549e-07                             1
a  epsilon                -0.12912                             3
a  Local Time Step      4.2277e-08                        252506


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -2.83          5.7069         0.46267        0.078097
v  Velocity[Y]             -7.4636          6.7176         0.23977         0.18723
v  Velocity[Z]             -10.873          8.8013        -0.18565     -0.00072005
v  ǁVelocityǁ           0.00055997          12.267          1.3251          1.5674
v  Pressure                -8842.4           20355           12926           10969
v  k                    1.1316e-07         0.83486       0.0062807        0.007895
v  epsilon              4.7962e-05           31526          36.811          4.7746
v  TurbVisc             5.2209e-13         0.14181      0.00052362       0.0062658
v  CourantNb                     0          905.04          8.3887          1.7858
v  FourierNb              0.025138      2.3653e+05          21.917         0.31688
v  total_pressure       4.9116e+05      5.2036e+05      5.1293e+05      5.1097e+05
v  Local Time Step           0.001         0.15217       0.0011048       0.0012168


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.79715      2.3718e+05          30.306          2.1027


 TIME FOR THE TIME STEP              141:        0.97465E+02

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


 INSTANT    0.142000000E+01   TIME STEP NUMBER             142
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.284596172E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699446358E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41512E+01 0.21361E+01
   Friction velocity        uet   :  0.92256E-02 0.57245E+01
   Friction velocity        uk    :  0.92101E-02 0.57245E+01
   Dimensionless distance   yplus :  0.73045E-03 0.82831E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2788
   Nb of faces within the viscous sub-layer     :      29077
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31585E+01      24   0.28217E-01   0.73125E+00 0.15982E+02 
c  Velocity[X]                                      0.18937E+00 
c  Velocity[Y]                                      0.25686E+00 
c  Velocity[Z]                                      0.28503E+00 
c  Pressure     0.12940E-01     823   0.27832E-01   0.89857E-01 0.32162E+01 
c  k            0.38988E-01      11   0.34682E-03   0.13219E-03 0.22522E+02 
c  epsilon      0.21629E+03      10   0.36154E-03   0.22210E+05 0.80112E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.5909e-07                             1
a  epsilon                 -6.3379                             6
a  Local Time Step      4.2277e-08                        252647


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.839          5.6776         0.46296        0.078135
v  Velocity[Y]             -8.0647          6.7263         0.23884         0.18725
v  Velocity[Z]             -10.865          8.7848        -0.18633     -0.00081702
v  ǁVelocityǁ           0.00045882           12.27          1.3275          1.5682
v  Pressure                  -8761           20429           12981           11012
v  k                     1.146e-07         0.83718       0.0062856       0.0079044
v  epsilon              6.0615e-05           30851          36.735          4.7741
v  TurbVisc             5.3832e-13         0.14181       0.0005215       0.0062768
v  CourantNb            0.00099285          905.99          8.4046          1.7876
v  FourierNb              0.025139      2.3653e+05          21.916         0.31689
v  total_pressure       4.9124e+05      5.2043e+05      5.1298e+05      5.1101e+05
v  Local Time Step           0.001         0.16358       0.0011046       0.0012173


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96766      2.3733e+05          30.321          2.1045


 TIME FOR THE TIME STEP              142:        0.83255E+02

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


 INSTANT    0.143000000E+01   TIME STEP NUMBER             143
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.738417957E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699510829E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41454E+01 0.21449E+01
   Friction velocity        uet   :  0.92174E-02 0.61057E+01
   Friction velocity        uk    :  0.92113E-02 0.61057E+01
   Dimensionless distance   yplus :  0.77910E-03 0.83494E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2798
   Nb of faces within the viscous sub-layer     :      29049
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31590E+01      19   0.28110E-01   0.72594E+00 0.15919E+02 
c  Velocity[X]                                      0.19169E+00 
c  Velocity[Y]                                      0.24675E+00 
c  Velocity[Z]                                      0.28750E+00 
c  Pressure     0.12924E-01     418   0.27665E-01   0.89828E-01 0.71950E+00 
c  k            0.38997E-01      11   0.86848E-04   0.10137E-03 0.19674E+02 
c  epsilon      0.21608E+03      12   0.33711E-03   0.20897E+05 0.77588E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023182                             4
a  epsilon                -0.26441                            13
a  Local Time Step      4.2277e-08                        252786


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.8269          5.6808         0.46336        0.078155
v  Velocity[Y]             -8.2179          6.7399          0.2379         0.18725
v  Velocity[Z]             -10.917          8.8028        -0.18685     -0.00089571
v  ǁVelocityǁ           0.00058046          12.322          1.3299          1.5689
v  Pressure                -8699.7           20448           12981           11014
v  k                    1.1394e-07         0.83211        0.006305       0.0079145
v  epsilon              6.0897e-05           31627           37.05          4.7802
v  TurbVisc             5.4226e-13         0.14181      0.00051931        0.006287
v  CourantNb                     0          905.03          8.4197          1.7896
v  FourierNb               0.02514      2.3653e+05          21.915          0.3168
v  total_pressure        4.913e+05      5.2045e+05      5.1298e+05      5.1101e+05
v  Local Time Step           0.001         0.16358       0.0011043       0.0012168


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81814      2.3724e+05          30.335          2.1064


 TIME FOR THE TIME STEP              143:        0.81051E+02

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


 INSTANT    0.144000000E+01   TIME STEP NUMBER             144
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.763799480E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699549299E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42016E+01 0.21406E+01
   Friction velocity        uet   :  0.13876E-01 0.47412E+01
   Friction velocity        uk    :  0.13720E-01 0.47412E+01
   Dimensionless distance   yplus :  0.60499E-03 0.84128E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2801
   Nb of faces within the viscous sub-layer     :      29034
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31593E+01      20   0.28965E-01   0.71495E+00 0.15796E+02 
c  Velocity[X]                                      0.18092E+00 
c  Velocity[Y]                                      0.24936E+00 
c  Velocity[Z]                                      0.28467E+00 
c  Pressure     0.12884E-01     435   0.27560E-01   0.89524E-01 0.95313E+00 
c  k            0.39013E-01      11   0.12618E-03   0.12713E-03 0.22025E+02 
c  epsilon      0.21670E+03      13   0.44374E-03   0.28187E+05 0.89969E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010284                             4
a  epsilon                 -5.0594                            13
a  Local Time Step      4.2277e-08                        252948


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.8243          5.7139         0.46366        0.078127
v  Velocity[Y]              -8.111          6.7273         0.23713         0.18722
v  Velocity[Z]             -10.994           8.803        -0.18722     -0.00097219
v  ǁVelocityǁ           0.00050178          12.366          1.3322          1.5697
v  Pressure                -8681.6           20465           12980           11017
v  k                    1.1606e-07         0.83699       0.0063058       0.0079241
v  epsilon              1.9804e-05           31021          36.944          4.7917
v  TurbVisc             5.3751e-13         0.14181      0.00051678       0.0062966
v  CourantNb             0.0049139          905.35          8.4315          1.7914
v  FourierNb              0.025141      2.3653e+05          21.914         0.31675
v  total_pressure       4.9132e+05      5.2046e+05      5.1298e+05      5.1102e+05
v  Local Time Step           0.001         0.16358       0.0011039       0.0012171


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73906      2.3681e+05          30.345          2.1081


 TIME FOR THE TIME STEP              144:        0.74420E+02

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


 INSTANT    0.145000000E+01   TIME STEP NUMBER             145
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.113345556E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699557991E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42614E+01 0.21449E+01
   Friction velocity        uet   :  0.55194E-02 0.49353E+01
   Friction velocity        uk    :  0.55139E-02 0.49353E+01
   Dimensionless distance   yplus :  0.52408E-03 0.84643E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2801
   Nb of faces within the viscous sub-layer     :      29028
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31593E+01      23   0.28142E-01   0.73167E+00 0.15961E+02 
c  Velocity[X]                                      0.19045E+00 
c  Velocity[Y]                                      0.25323E+00 
c  Velocity[Z]                                      0.28799E+00 
c  Pressure     0.13141E-01     473   0.28375E-01   0.91479E-01 0.89598E+00 
c  k            0.39021E-01      11   0.10377E-03   0.11674E-03 0.21126E+02 
c  epsilon      0.21591E+03      10   0.34008E-03   0.17848E+05 0.71775E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.7792e-05                             3
a  epsilon                -0.13427                             7
a  Local Time Step      4.2277e-08                        253109


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.8103           5.727         0.46399        0.078125
v  Velocity[Y]             -7.7739          6.6873         0.23643         0.18723
v  Velocity[Z]             -11.014          8.8092         -0.1875     -0.00098566
v  ǁVelocityǁ            0.0003529          12.475          1.3344          1.5703
v  Pressure                -8627.3           20476           12980           11020
v  k                    1.1614e-07         0.83481       0.0063061       0.0079322
v  epsilon              6.2218e-05           31630          36.915            4.79
v  TurbVisc             5.4047e-13         0.14181      0.00051449       0.0063055
v  CourantNb             0.0062069          900.02          8.4438          1.7933
v  FourierNb              0.025141      2.3653e+05          21.913         0.31673
v  total_pressure       4.9137e+05      5.2048e+05      5.1298e+05      5.1102e+05
v  Local Time Step           0.001         0.16358       0.0011036       0.0012179


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76255      2.3712e+05          30.357            2.11


 TIME FOR THE TIME STEP              145:        0.75817E+02

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


 INSTANT    0.146000000E+01   TIME STEP NUMBER             146
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.171577129E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699601856E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42602E+01 0.21348E+01
   Friction velocity        uet   :  0.11399E-01 0.55655E+01
   Friction velocity        uk    :  0.11387E-01 0.55655E+01
   Dimensionless distance   yplus :  0.68227E-03 0.85107E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2806
   Nb of faces within the viscous sub-layer     :      29002
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31596E+01      21   0.28480E-01   0.69276E+00 0.15539E+02 
c  Velocity[X]                                      0.18255E+00 
c  Velocity[Y]                                      0.23517E+00 
c  Velocity[Z]                                      0.27505E+00 
c  Pressure     0.12604E-01     444   0.27194E-01   0.87635E-01 0.77802E+00 
c  k            0.39023E-01      10   0.38896E-03   0.14489E-03 0.23453E+02 
c  epsilon      0.21488E+03       9   0.60479E-03   0.26154E+05 0.86910E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015623                             5
a  epsilon                -0.24791                            15
a  Local Time Step      4.2277e-08                        253239


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.8073          5.7393         0.46421        0.078107
v  Velocity[Y]             -7.8305          6.6664         0.23587         0.18721
v  Velocity[Z]             -10.991          8.8395        -0.18804      -0.0010274
v  ǁVelocityǁ           0.00034511          12.436          1.3365          1.5711
v  Pressure                -8593.8           20487           12980           11020
v  k                    1.1677e-07          0.8357       0.0063127        0.007941
v  epsilon              6.3112e-05           30782           36.87          4.7955
v  TurbVisc             5.3912e-13         0.14181      0.00051212       0.0063138
v  CourantNb             0.0018096          943.19          8.4516          1.7949
v  FourierNb               0.02514      2.3653e+05          21.912         0.31683
v  total_pressure       4.9141e+05      5.2049e+05      5.1298e+05      5.1102e+05
v  Local Time Step           0.001         0.16358       0.0011034       0.0012193


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0272      2.3675e+05          30.363          2.1117


 TIME FOR THE TIME STEP              146:        0.72989E+02

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


 INSTANT    0.147000000E+01   TIME STEP NUMBER             147
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.315760697E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699615138E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42701E+01 0.21464E+01
   Friction velocity        uet   :  0.27063E-02 0.72038E+01
   Friction velocity        uk    :  0.27043E-02 0.72038E+01
   Dimensionless distance   yplus :  0.91921E-03 0.85509E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2804
   Nb of faces within the viscous sub-layer     :      28967
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31597E+01      20   0.28362E-01   0.69111E+00 0.15518E+02 
c  Velocity[X]                                      0.18949E+00 
c  Velocity[Y]                                      0.22908E+00 
c  Velocity[Z]                                      0.27254E+00 
c  Pressure     0.12600E-01     343   0.27184E-01   0.87658E-01 0.70526E+00 
c  k            0.39044E-01      13   0.23769E-03   0.13921E-03 0.23031E+02 
c  epsilon      0.21666E+03      13   0.64072E-03   0.31885E+05 0.95454E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018927                             6
a  epsilon                 -17.023                            19
a  Local Time Step      4.2277e-08                        253395


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7906          5.7515         0.46431        0.078081
v  Velocity[Y]             -7.7393          6.6839         0.23541         0.18724
v  Velocity[Z]             -11.052          9.2363        -0.18836      -0.0010719
v  ǁVelocityǁ           0.00041084          12.524          1.3384          1.5717
v  Pressure                -8542.2           20493           12980           11021
v  k                    1.1602e-07         0.83454       0.0063381        0.007951
v  epsilon              6.4391e-05           31701          37.219          4.8108
v  TurbVisc             5.5078e-13         0.14181      0.00051013       0.0063215
v  CourantNb                     0          888.76          8.4678          1.7966
v  FourierNb               0.02514      2.3653e+05          21.911         0.31688
v  total_pressure       4.9146e+05      5.2049e+05      5.1298e+05      5.1102e+05
v  Local Time Step           0.001         0.16358       0.0011033        0.001221


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0261      2.3714e+05          30.379          2.1135


 TIME FOR THE TIME STEP              147:        0.74451E+02

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


 INSTANT    0.148000000E+01   TIME STEP NUMBER             148
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.183576531E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699596243E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42596E+01 0.21431E+01
   Friction velocity        uet   :  0.71974E-02 0.67179E+01
   Friction velocity        uk    :  0.71864E-02 0.67179E+01
   Dimensionless distance   yplus :  0.85721E-03 0.85840E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2803
   Nb of faces within the viscous sub-layer     :      28935
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31597E+01      20   0.28018E-01   0.67703E+00 0.15346E+02 
c  Velocity[X]                                      0.17650E+00 
c  Velocity[Y]                                      0.22671E+00 
c  Velocity[Z]                                      0.27382E+00 
c  Pressure     0.13032E-01     545   0.28061E-01   0.90696E-01 0.79824E+00 
c  k            0.39050E-01      11   0.10724E-03   0.10296E-03 0.19789E+02 
c  epsilon      0.21582E+03      10   0.49011E-03   0.24875E+05 0.84644E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.6466e-05                             5
a  epsilon                -0.20822                            20
a  Local Time Step      4.2277e-08                        253533


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7807          5.7339         0.46437        0.078074
v  Velocity[Y]             -7.7112          6.7009         0.23524         0.18722
v  Velocity[Z]             -11.096          8.8463        -0.18878      -0.0011095
v  ǁVelocityǁ           0.00054048          12.559          1.3403          1.5723
v  Pressure                -8469.2           20500           12980           11024
v  k                    1.1679e-07         0.83633       0.0063427       0.0079594
v  epsilon               6.576e-05           31018          37.308          4.8132
v  TurbVisc             5.4453e-13         0.14181      0.00050814       0.0063287
v  CourantNb                     0          970.61          8.4728          1.7983
v  FourierNb              0.025139      2.3653e+05           21.91         0.31691
v  total_pressure       4.9153e+05       5.205e+05      5.1298e+05      5.1102e+05
v  Local Time Step           0.001         0.16359       0.0011031       0.0012219


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78083      2.3664e+05          30.383          2.1152


 TIME FOR THE TIME STEP              148:        0.83302E+02

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


 INSTANT    0.149000000E+01   TIME STEP NUMBER             149
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.280656916E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699612877E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43222E+01 0.21427E+01
   Friction velocity        uet   :  0.72410E-02 0.59129E+01
   Friction velocity        uk    :  0.72298E-02 0.59129E+01
   Dimensionless distance   yplus :  0.54234E-03 0.86129E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2803
   Nb of faces within the viscous sub-layer     :      28923
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31598E+01      25   0.28443E-01   0.68700E+00 0.15470E+02 
c  Velocity[X]                                      0.17437E+00 
c  Velocity[Y]                                      0.23430E+00 
c  Velocity[Z]                                      0.27832E+00 
c  Pressure     0.13153E-01     424   0.28111E-01   0.91594E-01 0.78058E+00 
c  k            0.39054E-01       9   0.39898E-03   0.11866E-03 0.21198E+02 
c  epsilon      0.21459E+03       7   0.34723E-03   0.16140E+05 0.68217E+02 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00063222                             7
a  epsilon                 -46.623                            18
a  Local Time Step      4.2277e-08                        253657


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7642          5.7588         0.46445        0.078113
v  Velocity[Y]             -7.6166          6.6993         0.23513         0.18719
v  Velocity[Z]             -11.127          8.8721          -0.189      -0.0010672
v  ǁVelocityǁ           0.00063485            12.6          1.3423          1.5729
v  Pressure                -8399.9           20505           12980           11026
v  k                    1.1977e-07         0.83628        0.006337       0.0079673
v  epsilon              6.7026e-05           31551          36.905          4.8165
v  TurbVisc             5.4864e-13         0.14181      0.00050635       0.0063353
v  CourantNb             0.0085047          1021.6          8.4862          1.7998
v  FourierNb              0.025138      2.3653e+05          21.909         0.31685
v  total_pressure        4.916e+05      5.2051e+05      5.1298e+05      5.1103e+05
v  Local Time Step           0.001         0.16359       0.0011028       0.0012223


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7155      2.3708e+05          30.395          2.1166


 TIME FOR THE TIME STEP              149:        0.64450E+02

===============================================================


 INSTANT    0.150000000E+01   TIME STEP NUMBER             150
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.516521931E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699581593E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43997E+01 0.21381E+01
   Friction velocity        uet   :  0.54182E-02 0.83118E+01
   Friction velocity        uk    :  0.54019E-02 0.83118E+01
   Dimensionless distance   yplus :  0.64572E-03 0.86402E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2810
   Nb of faces within the viscous sub-layer     :      28904
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31598E+01      22   0.28682E-01   0.69769E+00 0.15590E+02 
c  Velocity[X]                                      0.17921E+00 
c  Velocity[Y]                                      0.23408E+00 
c  Velocity[Z]                                      0.28440E+00 
c  Pressure     0.12529E-01     372   0.27214E-01   0.87254E-01 0.71107E+00 
c  k            0.39065E-01      12   0.24841E-03   0.15950E-03 0.24631E+02 
c  epsilon      0.21632E+03      12   0.71163E-03   0.51278E+05 0.12058E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00029974                             8
a  epsilon                 -1.7806                            20
a  Local Time Step      4.2277e-08                        253796


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.768          5.7025         0.46446        0.078088
v  Velocity[Y]             -7.3156           6.711         0.23524         0.18714
v  Velocity[Z]             -11.123           8.878        -0.18925      -0.0010268
v  ǁVelocityǁ           0.00043416          12.573          1.3443          1.5735
v  Pressure                -8334.9           20506           12981           11028
v  k                    1.1524e-07         0.83275       0.0063721       0.0079749
v  epsilon              6.8814e-05           30940          37.646          4.8304
v  TurbVisc             5.6649e-13         0.14181      0.00050478       0.0063416
v  CourantNb             0.0085174          944.07          8.4946          1.8013
v  FourierNb              0.025137      2.3653e+05          21.908         0.31676
v  total_pressure       4.9167e+05      5.2051e+05      5.1298e+05      5.1103e+05
v  Local Time Step           0.001         0.11229       0.0011024       0.0012222


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90681      2.3663e+05          30.402          2.1181


 TIME FOR THE TIME STEP              150:        0.70193E+02

===============================================================


 INSTANT    0.151000000E+01   TIME STEP NUMBER             151
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.242995528E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699547092E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43662E+01 0.21378E+01
   Friction velocity        uet   :  0.88998E-02 0.60055E+01
   Friction velocity        uk    :  0.88824E-02 0.60055E+01
   Dimensionless distance   yplus :  0.76631E-03 0.86595E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2808
   Nb of faces within the viscous sub-layer     :      28889
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31597E+01      22   0.28189E-01   0.67724E+00 0.15367E+02 
c  Velocity[X]                                      0.17755E+00 
c  Velocity[Y]                                      0.22927E+00 
c  Velocity[Z]                                      0.27042E+00 
c  Pressure     0.12458E-01     268   0.26962E-01   0.86740E-01 0.59710E+00 
c  k            0.39071E-01      15   0.15716E-03   0.22111E-03 0.28722E+02 
c  epsilon      0.21577E+03      12   0.48194E-03   0.48506E+05 0.11747E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011539                             9
a  epsilon                 -23.664                            23
a  Local Time Step      4.2277e-08                        253916


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.759          5.7607         0.46465        0.078067
v  Velocity[Y]             -7.1741          6.7429         0.23546         0.18712
v  Velocity[Z]              -11.09          8.8768        -0.18968      -0.0009937
v  ǁVelocityǁ           0.00033497          12.545          1.3466           1.574
v  Pressure                -8238.1           20507           12982           11031
v  k                    1.1125e-07         0.83369       0.0063706       0.0079828
v  epsilon              7.0773e-05           31325          37.321          4.8375
v  TurbVisc             5.3606e-13         0.14181      0.00050303       0.0063474
v  CourantNb             0.0078616           875.8          8.5102          1.8029
v  FourierNb              0.025136      2.3653e+05          21.907         0.31681
v  total_pressure       4.9176e+05      5.2051e+05      5.1298e+05      5.1103e+05
v  Local Time Step           0.001         0.12352       0.0011021       0.0012236


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98865      2.3724e+05          30.417          2.1197


 TIME FOR THE TIME STEP              151:        0.65325E+02

===============================================================


 INSTANT    0.152000000E+01   TIME STEP NUMBER             152
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.273952710E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699556007E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43668E+01 0.21342E+01
   Friction velocity        uet   :  0.12729E-01 0.65597E+01
   Friction velocity        uk    :  0.12696E-01 0.65597E+01
   Dimensionless distance   yplus :  0.83702E-03 0.86725E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2800
   Nb of faces within the viscous sub-layer     :      28882
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31596E+01      21   0.28640E-01   0.67726E+00 0.15349E+02 
c  Velocity[X]                                      0.17263E+00 
c  Velocity[Y]                                      0.22433E+00 
c  Velocity[Z]                                      0.28030E+00 
c  Pressure     0.12739E-01     277   0.27357E-01   0.88515E-01 0.58784E+00 
c  k            0.39074E-01      11   0.40206E-03   0.13353E-03 0.22506E+02 
c  epsilon      0.21605E+03       9   0.41976E-03   0.28120E+05 0.89599E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019501                             8
a  epsilon                 -1.0533                            23
a  Local Time Step      4.2277e-08                        254023


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -2.756          5.7927          0.4647        0.078032
v  Velocity[Y]              -7.842          6.7124         0.23585         0.18711
v  Velocity[Z]             -11.233          8.8887        -0.19018      -0.0009931
v  ǁVelocityǁ           0.00036638          12.715          1.3487          1.5746
v  Pressure                -8180.2           20503           12982           11031
v  k                    8.5886e-08         0.83685       0.0063713       0.0079876
v  epsilon              7.2691e-05           30739          37.451          4.8326
v  TurbVisc             5.5183e-13         0.14181      0.00050139       0.0063528
v  CourantNb                     0          860.75          8.5244          1.8043
v  FourierNb              0.025135      2.3653e+05          21.906         0.31678
v  total_pressure       4.9182e+05       5.205e+05      5.1298e+05      5.1103e+05
v  Local Time Step           0.001         0.13588       0.0011018       0.0012258


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6308      2.3669e+05          30.431          2.1211


 TIME FOR THE TIME STEP              152:        0.62547E+02

===============================================================


 INSTANT    0.153000000E+01   TIME STEP NUMBER             153
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.113355694E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699536317E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41917E+01 0.21406E+01
   Friction velocity        uet   :  0.10262E-01 0.75842E+01
   Friction velocity        uk    :  0.10251E-01 0.75842E+01
   Dimensionless distance   yplus :  0.73560E-03 0.86818E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2802
   Nb of faces within the viscous sub-layer     :      28868
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31596E+01      20   0.28542E-01   0.70211E+00 0.15623E+02 
c  Velocity[X]                                      0.17416E+00 
c  Velocity[Y]                                      0.23893E+00 
c  Velocity[Z]                                      0.28903E+00 
c  Pressure     0.13098E-01     427   0.28187E-01   0.91025E-01 0.80576E+00 
c  k            0.39077E-01      11   0.22827E-03   0.14371E-03 0.23384E+02 
c  epsilon      0.21582E+03       8   0.40611E-03   0.21172E+05 0.77755E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021046                            10
a  epsilon                 -31.853                            23
a  Local Time Step      4.2277e-08                        254113


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7387           5.782         0.46482        0.078015
v  Velocity[Y]             -8.0721          6.6998         0.23629         0.18711
v  Velocity[Z]             -11.187          8.9196        -0.19036        -0.00095
v  ǁVelocityǁ           0.00052723          12.672          1.3507          1.5752
v  Pressure                -8108.6           20510           12982           11036
v  k                    7.5778e-08         0.83364       0.0063781       0.0079942
v  epsilon              7.4532e-05           31518          37.294          4.8433
v  TurbVisc             5.4329e-13         0.14181      0.00049996       0.0063577
v  CourantNb              0.003144          867.22           8.536          1.8056
v  FourierNb              0.025134      2.3653e+05          21.905         0.31657
v  total_pressure       4.9189e+05      5.2051e+05      5.1298e+05      5.1104e+05
v  Local Time Step           0.001         0.14946       0.0011012       0.0012248


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.95019      2.3661e+05          30.441          2.1222


 TIME FOR THE TIME STEP              153:        0.64342E+02

===============================================================


 INSTANT    0.154000000E+01   TIME STEP NUMBER             154
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.253313623E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699487899E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43775E+01 0.21307E+01
   Friction velocity        uet   :  0.12890E-01 0.65147E+01
   Friction velocity        uk    :  0.12882E-01 0.65147E+01
   Dimensionless distance   yplus :  0.60135E-03 0.86866E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2805
   Nb of faces within the viscous sub-layer     :      28840
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31594E+01      20   0.28360E-01   0.67447E+00 0.15305E+02 
c  Velocity[X]                                      0.17729E+00 
c  Velocity[Y]                                      0.22493E+00 
c  Velocity[Z]                                      0.27225E+00 
c  Pressure     0.12786E-01     354   0.27192E-01   0.88785E-01 0.59303E+00 
c  k            0.39087E-01      11   0.12952E-03   0.13284E-03 0.22284E+02 
c  epsilon      0.21712E+03      10   0.78551E-03   0.42746E+05 0.11001E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021106                             9
a  epsilon                 -0.3672                            22
a  Local Time Step      4.2277e-08                        254230


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7413          5.7458         0.46467         0.07803
v  Velocity[Y]                -8.1          6.6833         0.23687         0.18713
v  Velocity[Z]             -11.194          8.9233        -0.19086     -0.00091572
v  ǁVelocityǁ           0.00049548          12.667          1.3527          1.5757
v  Pressure                -8004.3           20512           12984           11037
v  k                    5.9273e-08         0.83342       0.0064011       0.0079998
v  epsilon              7.6757e-05           30491          37.933          4.8467
v  TurbVisc             5.5271e-13         0.14181      0.00049896       0.0063623
v  CourantNb             0.0029107          924.81          8.5491           1.807
v  FourierNb              0.025133      2.3653e+05          21.905         0.31649
v  total_pressure         4.92e+05      5.2051e+05      5.1298e+05      5.1104e+05
v  Local Time Step           0.001         0.11555       0.0011008       0.0012252


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.833      2.3743e+05          30.454          2.1235


 TIME FOR THE TIME STEP              154:        0.72076E+02

===============================================================


 INSTANT    0.155000000E+01   TIME STEP NUMBER             155
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.610895608E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699439365E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42917E+01 0.21384E+01
   Friction velocity        uet   :  0.86158E-02 0.62813E+01
   Friction velocity        uk    :  0.86108E-02 0.62813E+01
   Dimensionless distance   yplus :  0.53346E-03 0.86888E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2800
   Nb of faces within the viscous sub-layer     :      28835
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31589E+01      21   0.27964E-01   0.65356E+00 0.15062E+02 
c  Velocity[X]                                      0.17729E+00 
c  Velocity[Y]                                      0.21906E+00 
c  Velocity[Z]                                      0.25722E+00 
c  Pressure     0.12497E-01     253   0.26639E-01   0.86624E-01 0.56097E+00 
c  k            0.39089E-01      11   0.40553E-03   0.11740E-03 0.20859E+02 
c  epsilon      0.21684E+03       9   0.61539E-03   0.38287E+05 0.10395E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003537                             9
a  epsilon                 -3.8564                            25
a  Local Time Step      4.2277e-08                        254251


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7423          5.7562         0.46482        0.078052
v  Velocity[Y]             -8.0387          6.6788         0.23733         0.18715
v  Velocity[Z]             -11.212          8.9573        -0.19139     -0.00088218
v  ǁVelocityǁ           0.00036111          12.694          1.3548          1.5763
v  Pressure                  -7865           20515           12984           11038
v  k                    3.5296e-08         0.83391        0.006403       0.0080054
v  epsilon              6.7263e-05           31460          37.806            4.85
v  TurbVisc             5.5994e-13         0.14181        0.000498       0.0063665
v  CourantNb            0.00089399          894.57          8.5597          1.8083
v  FourierNb              0.025132      2.3653e+05          21.904         0.31646
v  total_pressure       4.9214e+05      5.2051e+05      5.1298e+05      5.1104e+05
v  Local Time Step           0.001         0.11303       0.0011004       0.0012258


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74995      2.3665e+05          30.464          2.1247


 TIME FOR THE TIME STEP              155:        0.69208E+02

===============================================================


 INSTANT    0.156000000E+01   TIME STEP NUMBER             156
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.366381743E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699410072E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43634E+01 0.21307E+01
   Friction velocity        uet   :  0.11058E-01 0.78125E+01
   Friction velocity        uk    :  0.11032E-01 0.78125E+01
   Dimensionless distance   yplus :  0.55656E-03 0.86871E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2796
   Nb of faces within the viscous sub-layer     :      28819
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31586E+01      19   0.27953E-01   0.64697E+00 0.14994E+02 
c  Velocity[X]                                      0.17385E+00 
c  Velocity[Y]                                      0.22310E+00 
c  Velocity[Z]                                      0.25002E+00 
c  Pressure     0.12620E-01     743   0.26942E-01   0.87271E-01 0.34068E+01 
c  k            0.39093E-01      12   0.23229E-03   0.15630E-03 0.24432E+02 
c  epsilon      0.21740E+03      11   0.51213E-03   0.43223E+05 0.11026E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00032134                            11
a  epsilon                -0.38587                            24
a  Local Time Step      4.2277e-08                        254351


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7386          5.7209         0.46498        0.078097
v  Velocity[Y]             -7.7006          6.6784         0.23787         0.18714
v  Velocity[Z]             -11.189          8.9977        -0.19194     -0.00095619
v  ǁVelocityǁ           0.00041412          12.661           1.357           1.577
v  Pressure                -7716.7           20576           13038           11086
v  k                    1.4792e-08         0.83239       0.0064193       0.0080115
v  epsilon              5.2999e-05           30617          38.013          4.8571
v  TurbVisc             5.7312e-13         0.14181      0.00049734       0.0063706
v  CourantNb             0.0005902          988.05          8.5706          1.8096
v  FourierNb              0.025131      2.3653e+05          21.904          0.3164
v  total_pressure       4.9228e+05      5.2058e+05      5.1304e+05      5.1109e+05
v  Local Time Step           0.001         0.10189       0.0011001       0.0012263


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.932      2.3674e+05          30.474           2.126


 TIME FOR THE TIME STEP              156:        0.87764E+02

===============================================================


 INSTANT    0.157000000E+01   TIME STEP NUMBER             157
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.139253364E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699487861E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43299E+01 0.21360E+01
   Friction velocity        uet   :  0.90473E-02 0.63958E+01
   Friction velocity        uk    :  0.90429E-02 0.63958E+01
   Dimensionless distance   yplus :  0.54438E-03 0.86844E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2795
   Nb of faces within the viscous sub-layer     :      28812
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31590E+01      25   0.28151E-01   0.64776E+00 0.14989E+02 
c  Velocity[X]                                      0.17033E+00 
c  Velocity[Y]                                      0.22404E+00 
c  Velocity[Z]                                      0.25339E+00 
c  Pressure     0.12576E-01     286   0.26850E-01   0.87106E-01 0.54032E+00 
c  k            0.39096E-01      14   0.12544E-03   0.18093E-03 0.26282E+02 
c  epsilon      0.21735E+03      10   0.40696E-03   0.39830E+05 0.10594E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00032927                            11
a  epsilon                 -2.5299                            25
a  Local Time Step      4.2277e-08                        254465


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7314          5.7306         0.46514        0.078112
v  Velocity[Y]             -7.3037          6.6613         0.23834         0.18713
v  Velocity[Z]             -11.113          9.0159        -0.19255      -0.0010057
v  ǁVelocityǁ           0.00021203          12.599           1.359          1.5776
v  Pressure                -7589.8           20580           13038           11087
v  k                    3.4329e-08         0.83469       0.0064227       0.0080167
v  epsilon               5.178e-05           31311          38.045          4.8617
v  TurbVisc             5.3618e-13         0.14181       0.0004968       0.0063743
v  CourantNb             0.0024154          900.13          8.5852          1.8109
v  FourierNb              0.025131      2.3653e+05          21.903         0.31619
v  total_pressure       4.9241e+05      5.2058e+05      5.1304e+05      5.1109e+05
v  Local Time Step           0.001         0.11208       0.0010995       0.0012261


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0274      2.3716e+05          30.488          2.1271


 TIME FOR THE TIME STEP              157:        0.66995E+02

===============================================================


 INSTANT    0.158000000E+01   TIME STEP NUMBER             158
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.216639598E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699583593E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43197E+01 0.21318E+01
   Friction velocity        uet   :  0.65629E-02 0.55610E+01
   Friction velocity        uk    :  0.65604E-02 0.55610E+01
   Dimensionless distance   yplus :  0.55326E-03 0.86791E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2798
   Nb of faces within the viscous sub-layer     :      28804
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31589E+01      23   0.28586E-01   0.64913E+00 0.14988E+02 
c  Velocity[X]                                      0.18136E+00 
c  Velocity[Y]                                      0.21516E+00 
c  Velocity[Z]                                      0.25261E+00 
c  Pressure     0.12883E-01     274   0.27390E-01   0.89218E-01 0.56159E+00 
c  k            0.39099E-01      12   0.42212E-03   0.17802E-03 0.26062E+02 
c  epsilon      0.21806E+03      15   0.51674E-03   0.36271E+05 0.10105E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003111                            11
a  epsilon                -0.36711                            27
a  Local Time Step      4.2277e-08                        254469


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7276          5.7683          0.4652        0.078122
v  Velocity[Y]             -7.6332           6.646         0.23882         0.18712
v  Velocity[Z]             -11.269          9.0452        -0.19323      -0.0010443
v  ǁVelocityǁ           0.00033299          12.694          1.3609          1.5783
v  Pressure                -7578.5           20583           13038           11087
v  k                    2.8758e-08         0.83449       0.0064247        0.008021
v  epsilon               6.525e-05           30693          38.089          4.8606
v  TurbVisc             5.4911e-13         0.14181      0.00049649       0.0063778
v  CourantNb             0.0020967           896.2          8.5961          1.8122
v  FourierNb              0.025131      2.3653e+05          21.902         0.31611
v  total_pressure       4.9242e+05      5.2058e+05      5.1304e+05      5.1109e+05
v  Local Time Step           0.001         0.12329       0.0010992       0.0012265


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96556      2.3675e+05          30.498          2.1283


 TIME FOR THE TIME STEP              158:        0.63133E+02

===============================================================


 INSTANT    0.159000000E+01   TIME STEP NUMBER             159
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.146411712E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699619246E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42334E+01 0.21394E+01
   Friction velocity        uet   :  0.80937E-02 0.79887E+01
   Friction velocity        uk    :  0.80907E-02 0.79887E+01
   Dimensionless distance   yplus :  0.30825E-03 0.86755E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2803
   Nb of faces within the viscous sub-layer     :      28783
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31586E+01      22   0.28620E-01   0.64664E+00 0.14948E+02 
c  Velocity[X]                                      0.18238E+00 
c  Velocity[Y]                                      0.21516E+00 
c  Velocity[Z]                                      0.24909E+00 
c  Pressure     0.12751E-01     280   0.26974E-01   0.88066E-01 0.51644E+00 
c  k            0.39099E-01      12   0.23689E-03   0.19819E-03 0.27452E+02 
c  epsilon      0.21671E+03      16   0.44966E-03   0.47652E+05 0.11574E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00031692                            10
a  epsilon                 -3.0042                            27
a  Local Time Step      4.2277e-08                        254508


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7236          5.8094         0.46527        0.078154
v  Velocity[Y]             -7.7549          6.6402         0.23896         0.18713
v  Velocity[Z]             -11.226           9.084        -0.19369       -0.001091
v  ǁVelocityǁ           0.00044613          12.746          1.3626          1.5789
v  Pressure                -7653.6           20587           13037           11087
v  k                    1.0015e-07         0.83378       0.0064404       0.0080268
v  epsilon              6.6873e-05           31380          38.258          4.8719
v  TurbVisc             5.6021e-13         0.14181      0.00049611        0.006381
v  CourantNb             0.0019401          1033.4          8.6078          1.8135
v  FourierNb              0.025131      2.3653e+05          21.902           0.316
v  total_pressure       4.9235e+05      5.2059e+05      5.1304e+05      5.1109e+05
v  Local Time Step           0.001         0.13562       0.0010989       0.0012254


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91677      2.3664e+05           30.51          2.1295


 TIME FOR THE TIME STEP              159:        0.65432E+02

===============================================================


 INSTANT    0.160000000E+01   TIME STEP NUMBER             160
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.333834161E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699683331E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43687E+01 0.21306E+01
   Friction velocity        uet   :  0.57061E-02 0.67025E+01
   Friction velocity        uk    :  0.57039E-02 0.67025E+01
   Dimensionless distance   yplus :  0.48371E-03 0.86729E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2803
   Nb of faces within the viscous sub-layer     :      28772
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31586E+01      19   0.29112E-01   0.64729E+00 0.14957E+02 
c  Velocity[X]                                      0.17941E+00 
c  Velocity[Y]                                      0.21629E+00 
c  Velocity[Z]                                      0.25159E+00 
c  Pressure     0.12674E-01     755   0.26574E-01   0.87302E-01 0.13176E+01 
c  k            0.39103E-01      10   0.10008E-03   0.11869E-03 0.21246E+02 
c  epsilon      0.21671E+03       9   0.35435E-03   0.19981E+05 0.75214E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00031225                            10
a  epsilon                -0.28683                            26
a  Local Time Step      4.2277e-08                        254584


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7262           5.763         0.46535        0.078174
v  Velocity[Y]             -7.6524           6.633         0.23907         0.18717
v  Velocity[Z]             -11.309          9.0995        -0.19413      -0.0010416
v  ǁVelocityǁ           0.00040215          12.734          1.3642          1.5796
v  Pressure                -7731.1           20562           13011           11070
v  k                    7.6234e-08         0.83272       0.0064324       0.0080305
v  epsilon              8.9575e-05           30598          37.998          4.8678
v  TurbVisc             5.4175e-13         0.14181      0.00049553       0.0063838
v  CourantNb             0.0031994          983.53          8.6179          1.8148
v  FourierNb              0.025131      2.3653e+05          21.901         0.31586
v  total_pressure       4.9227e+05      5.2056e+05      5.1301e+05      5.1107e+05
v  Local Time Step           0.001         0.14918       0.0010985       0.0012262


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94122      2.3676e+05          30.519          2.1307


 TIME FOR THE TIME STEP              160:        0.90985E+02

===============================================================


 INSTANT    0.161000000E+01   TIME STEP NUMBER             161
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.131668240E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699676048E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42715E+01 0.21356E+01
   Friction velocity        uet   :  0.11685E-01 0.59779E+01
   Friction velocity        uk    :  0.11584E-01 0.59779E+01
   Dimensionless distance   yplus :  0.76278E-03 0.86728E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2808
   Nb of faces within the viscous sub-layer     :      28761
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31581E+01      20   0.29095E-01   0.65015E+00 0.14985E+02 
c  Velocity[X]                                      0.18482E+00 
c  Velocity[Y]                                      0.22580E+00 
c  Velocity[Z]                                      0.23953E+00 
c  Pressure     0.13220E-01     179   0.27687E-01   0.91009E-01 0.51205E+00 
c  k            0.39102E-01      10   0.39689E-03   0.11234E-03 0.20686E+02 
c  epsilon      0.21664E+03       8   0.31865E-03   0.16590E+05 0.68493E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00031241                             9
a  epsilon                 -2.7483                            26
a  Local Time Step      4.2277e-08                        254703


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7138          5.8173         0.46551        0.078177
v  Velocity[Y]             -7.4344          6.5884         0.23911          0.1872
v  Velocity[Z]              -11.21          9.1392        -0.19486      -0.0010114
v  ǁVelocityǁ           0.00035824          12.743          1.3658          1.5801
v  Pressure                -7759.5           20567           13011           11070
v  k                    5.3628e-08         0.83331       0.0064333       0.0080348
v  epsilon              6.3118e-05           31214          37.975          4.8709
v  TurbVisc              5.392e-13         0.14181      0.00049532       0.0063865
v  CourantNb             0.0027198          968.06          8.6247           1.816
v  FourierNb              0.025132      2.3653e+05            21.9         0.31575
v  total_pressure       4.9224e+05      5.2057e+05      5.1301e+05      5.1107e+05
v  Local Time Step           0.001          0.1641       0.0010982       0.0012261


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0275      2.3682e+05          30.525          2.1318


 TIME FOR THE TIME STEP              161:        0.54346E+02

===============================================================


 INSTANT    0.162000000E+01   TIME STEP NUMBER             162
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.255852975E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699656233E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43432E+01 0.21357E+01
   Friction velocity        uet   :  0.15134E-01 0.69650E+01
   Friction velocity        uk    :  0.14972E-01 0.69650E+01
   Dimensionless distance   yplus :  0.43249E-03 0.86699E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2804
   Nb of faces within the viscous sub-layer     :      28744
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31578E+01      23   0.29039E-01   0.64948E+00 0.14985E+02 
c  Velocity[X]                                      0.18143E+00 
c  Velocity[Y]                                      0.22349E+00 
c  Velocity[Z]                                      0.24456E+00 
c  Pressure     0.12960E-01     317   0.27068E-01   0.89068E-01 0.52647E+00 
c  k            0.39102E-01      10   0.10675E-03   0.11295E-03 0.20756E+02 
c  epsilon      0.21669E+03       9   0.34720E-03   0.16005E+05 0.67278E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00030935                             8
a  epsilon                -0.28946                            28
a  Local Time Step      4.2277e-08                        254770


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7206          5.8709         0.46558         0.07817
v  Velocity[Y]             -7.7458          6.5718         0.23914         0.18721
v  Velocity[Z]             -11.412          9.1849        -0.19553      -0.0010044
v  ǁVelocityǁ           0.00037793            12.9          1.3672          1.5807
v  Pressure                  -7792           20570           13011           11069
v  k                    1.1941e-07         0.83287       0.0064378       0.0080383
v  epsilon              9.2032e-05           30793          37.997          4.8705
v  TurbVisc             5.4589e-13         0.14181      0.00049518       0.0063891
v  CourantNb             0.0014636          938.11          8.6363          1.8171
v  FourierNb              0.025133      2.3653e+05            21.9          0.3157
v  total_pressure       4.9221e+05      5.2057e+05      5.1301e+05      5.1107e+05
v  Local Time Step           0.001         0.17232       0.0010978       0.0012267


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99882      2.3655e+05          30.536          2.1328


 TIME FOR THE TIME STEP              162:        0.64480E+02

===============================================================


 INSTANT    0.163000000E+01   TIME STEP NUMBER             163
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.359644594E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699614744E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42271E+01 0.21414E+01
   Friction velocity        uet   :  0.15393E-01 0.50841E+01
   Friction velocity        uk    :  0.15264E-01 0.50841E+01
   Dimensionless distance   yplus :  0.60623E-03 0.86645E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2813
   Nb of faces within the viscous sub-layer     :      28715
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31571E+01      22   0.28322E-01   0.64788E+00 0.14975E+02 
c  Velocity[X]                                      0.18560E+00 
c  Velocity[Y]                                      0.21378E+00 
c  Velocity[Z]                                      0.24850E+00 
c  Pressure     0.12908E-01     333   0.26865E-01   0.88530E-01 0.53821E+00 
c  k            0.39102E-01      12   0.89141E-04   0.10952E-03 0.20408E+02 
c  epsilon      0.21600E+03       9   0.23524E-03   0.14395E+05 0.63709E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00030082                             8
a  epsilon                -0.33243                            25
a  Local Time Step      4.2277e-08                        254858


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7135          5.8333          0.4658        0.078158
v  Velocity[Y]             -7.9867          6.5693         0.23893         0.18724
v  Velocity[Z]             -11.213          9.1923        -0.19591     -0.00094154
v  ǁVelocityǁ           0.00041975          12.762          1.3687          1.5812
v  Pressure                -7808.4           20572           13011           11072
v  k                    1.1871e-07         0.83512       0.0064676       0.0080436
v  epsilon              9.2885e-05           31410          38.327          4.8786
v  TurbVisc             5.6385e-13         0.14181      0.00049517       0.0063914
v  CourantNb             0.0082793          1031.3          8.6422          1.8182
v  FourierNb              0.025133      2.3653e+05          21.899         0.31552
v  total_pressure       4.9219e+05      5.2057e+05      5.1301e+05      5.1107e+05
v  Local Time Step           0.001         0.17316       0.0010976       0.0012257


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0275       2.367e+05          30.542          2.1337


 TIME FOR THE TIME STEP              163:        0.67185E+02

===============================================================


 INSTANT    0.164000000E+01   TIME STEP NUMBER             164
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.303838684E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699623533E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43749E+01 0.21352E+01
   Friction velocity        uet   :  0.17238E-01 0.47134E+01
   Friction velocity        uk    :  0.17183E-01 0.47134E+01
   Dimensionless distance   yplus :  0.43188E-03 0.86614E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2810
   Nb of faces within the viscous sub-layer     :      28708
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31568E+01      20   0.28478E-01   0.63345E+00 0.14796E+02 
c  Velocity[X]                                      0.18146E+00 
c  Velocity[Y]                                      0.20893E+00 
c  Velocity[Z]                                      0.24306E+00 
c  Pressure     0.12796E-01     282   0.26499E-01   0.87905E-01 0.56220E+00 
c  k            0.39101E-01      11   0.83123E-04   0.11800E-03 0.20991E+02 
c  epsilon      0.21552E+03       9   0.22087E-03   0.14700E+05 0.64412E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00030635                             9
a  epsilon                -0.29467                            23
a  Local Time Step      4.2277e-08                        254940


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7162          5.8108         0.46596        0.078166
v  Velocity[Y]             -8.0609          6.5293         0.23871          0.1873
v  Velocity[Z]             -11.404          9.9082        -0.19648      -0.0008889
v  ǁVelocityǁ           0.00044325          12.842            1.37          1.5817
v  Pressure                -7828.3           20579           13011           11070
v  k                    1.2816e-07         0.83465       0.0064667       0.0080467
v  epsilon              9.2684e-05           30779          38.188           4.879
v  TurbVisc              5.546e-13         0.14181       0.0004954       0.0063936
v  CourantNb             0.0077655          966.01          8.6497          1.8193
v  FourierNb              0.025134      2.3653e+05          21.899         0.31527
v  total_pressure       4.9217e+05      5.2058e+05      5.1301e+05      5.1107e+05
v  Local Time Step           0.001          0.1458       0.0010968       0.0012229


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0276      2.3678e+05          30.548          2.1346


 TIME FOR THE TIME STEP              164:        0.69357E+02

===============================================================


 INSTANT    0.165000000E+01   TIME STEP NUMBER             165
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.318223692E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699551130E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41216E+01 0.21352E+01
   Friction velocity        uet   :  0.16463E-01 0.60957E+01
   Friction velocity        uk    :  0.16454E-01 0.60957E+01
   Dimensionless distance   yplus :  0.45493E-03 0.86628E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2811
   Nb of faces within the viscous sub-layer     :      28702
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31562E+01      19   0.28580E-01   0.62576E+00 0.14712E+02 
c  Velocity[X]                                      0.18011E+00 
c  Velocity[Y]                                      0.20718E+00 
c  Velocity[Z]                                      0.23847E+00 
c  Pressure     0.12558E-01     361   0.26226E-01   0.86361E-01 0.58080E+00 
c  k            0.39107E-01       9   0.12604E-03   0.12074E-03 0.21463E+02 
c  epsilon      0.21594E+03       8   0.36730E-03   0.21619E+05 0.77908E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00030543                             8
a  epsilon                -0.29647                            20
a  Local Time Step      4.2277e-08                        255006


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7159          5.8168         0.46623        0.078157
v  Velocity[Y]             -7.9008          6.5506         0.23833         0.18734
v  Velocity[Z]              -11.26          9.2171        -0.19694      -0.0008319
v  ǁVelocityǁ           0.00066519           12.67          1.3711          1.5822
v  Pressure                -7842.8           20583           13012           11072
v  k                    1.1961e-07         0.83194         0.00648        0.008051
v  epsilon              8.6555e-05           31180          38.404          4.8889
v  TurbVisc             6.0531e-13         0.14181      0.00049533       0.0063955
v  CourantNb             0.0070971          914.84           8.656          1.8203
v  FourierNb              0.025135      2.3653e+05          21.898         0.31507
v  total_pressure       4.9216e+05      5.2058e+05      5.1301e+05      5.1107e+05
v  Local Time Step           0.001         0.16037       0.0010964       0.0012232


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96645      2.3657e+05          30.554          2.1354


 TIME FOR THE TIME STEP              165:        0.69849E+02

===============================================================


 INSTANT    0.166000000E+01   TIME STEP NUMBER             166
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.723586803E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699493013E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43148E+01 0.21355E+01
   Friction velocity        uet   :  0.97102E-02 0.63878E+01
   Friction velocity        uk    :  0.96392E-02 0.63878E+01
   Dimensionless distance   yplus :  0.72167E-03 0.86588E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2814
   Nb of faces within the viscous sub-layer     :      28681
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31555E+01      22   0.28560E-01   0.63459E+00 0.14809E+02 
c  Velocity[X]                                      0.17863E+00 
c  Velocity[Y]                                      0.20631E+00 
c  Velocity[Z]                                      0.24964E+00 
c  Pressure     0.12849E-01     284   0.26850E-01   0.88232E-01 0.52999E+00 
c  k            0.39105E-01      11   0.31073E-03   0.14524E-03 0.23464E+02 
c  epsilon      0.21494E+03      14   0.45132E-03   0.33216E+05 0.96739E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00027539                             7
a  epsilon                -0.28655                            24
a  Local Time Step      4.2277e-08                        255075


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7077          5.7133         0.46652        0.078141
v  Velocity[Y]             -7.5303          6.5334         0.23801         0.18739
v  Velocity[Z]             -11.537          9.2114        -0.19734     -0.00077579
v  ǁVelocityǁ           0.00056102          12.816          1.3723          1.5827
v  Pressure                -7887.4           20583           13013           11074
v  k                    1.2252e-07         0.83884       0.0064914       0.0080544
v  epsilon              8.4977e-05           30816          38.492          4.8872
v  TurbVisc             5.4116e-13         0.14181      0.00049525       0.0063973
v  CourantNb             0.0027708          933.26          8.6651          1.8212
v  FourierNb              0.025136      2.3653e+05          21.897         0.31493
v  total_pressure       4.9211e+05      5.2058e+05      5.1301e+05      5.1107e+05
v  Local Time Step           0.001         0.17315       0.0010958       0.0012231


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0085      2.3695e+05          30.562          2.1362


 TIME FOR THE TIME STEP              166:        0.66201E+02

===============================================================


 INSTANT    0.167000000E+01   TIME STEP NUMBER             167
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.141490013E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699411141E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37663E+01 0.21390E+01
   Friction velocity        uet   :  0.68470E-02 0.49876E+01
   Friction velocity        uk    :  0.68378E-02 0.49876E+01
   Dimensionless distance   yplus :  0.29570E-03 0.86547E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2816
   Nb of faces within the viscous sub-layer     :      28684
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31550E+01      21   0.28990E-01   0.62958E+00 0.14762E+02 
c  Velocity[X]                                      0.17722E+00 
c  Velocity[Y]                                      0.21207E+00 
c  Velocity[Z]                                      0.24029E+00 
c  Pressure     0.12502E-01     307   0.26085E-01   0.85878E-01 0.52456E+00 
c  k            0.39084E-01      11   0.98791E-04   0.16677E-03 0.25215E+02 
c  epsilon      0.21373E+03       9   0.25420E-03   0.37136E+05 0.10259E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.000296                             8
a  epsilon                -0.29681                            21
a  Local Time Step      4.2277e-08                        255162


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7112           5.808         0.46691        0.078136
v  Velocity[Y]             -7.5977          6.5031         0.23747         0.18739
v  Velocity[Z]             -11.287          9.2206        -0.19772     -0.00074514
v  ǁVelocityǁ           0.00043483          12.757          1.3735          1.5831
v  Pressure                -7893.3           20583           13014           11077
v  k                     1.264e-07         0.83352       0.0064868       0.0080567
v  epsilon              7.9181e-05           31328          38.372          4.8809
v  TurbVisc             5.7629e-13         0.14181      0.00049494       0.0063989
v  CourantNb              0.010788          1027.7          8.6719          1.8222
v  FourierNb              0.025136      2.3653e+05          21.896         0.31469
v  total_pressure       4.9211e+05      5.2058e+05      5.1301e+05      5.1108e+05
v  Local Time Step           0.001         0.15504       0.0010953       0.0012214


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0278      2.3654e+05          30.568          2.1369


 TIME FOR THE TIME STEP              167:        0.70002E+02

===============================================================


 INSTANT    0.168000000E+01   TIME STEP NUMBER             168
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.102457964E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699347227E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41083E+01 0.21332E+01
   Friction velocity        uet   :  0.14532E-01 0.64529E+01
   Friction velocity        uk    :  0.14411E-01 0.64529E+01
   Dimensionless distance   yplus :  0.81546E-03 0.86541E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2812
   Nb of faces within the viscous sub-layer     :      28674
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31545E+01      24   0.29257E-01   0.63737E+00 0.14851E+02 
c  Velocity[X]                                      0.17920E+00 
c  Velocity[Y]                                      0.21212E+00 
c  Velocity[Z]                                      0.24606E+00 
c  Pressure     0.12774E-01     501   0.26529E-01   0.87808E-01 0.62179E+00 
c  k            0.39088E-01       9   0.11775E-03   0.11118E-03 0.20576E+02 
c  epsilon      0.21444E+03       8   0.30352E-03   0.18777E+05 0.72946E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00029015                             7
a  epsilon                -0.29221                            18
a  Local Time Step      4.2277e-08                        255199


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7062          5.8452         0.46735        0.078154
v  Velocity[Y]             -7.4271          6.5341         0.23708         0.18738
v  Velocity[Z]             -11.525          9.2249        -0.19806     -0.00075197
v  ǁVelocityǁ           0.00049551          12.857          1.3747          1.5835
v  Pressure                -7926.4           20590           13017           11083
v  k                    1.1092e-07         0.83413       0.0064813       0.0080599
v  epsilon              7.8976e-05           30728          38.143          4.8852
v  TurbVisc             5.9505e-13         0.14181      0.00049479       0.0064005
v  CourantNb                     0          938.33          8.6818          1.8231
v  FourierNb              0.025137      2.3653e+05          21.896          0.3143
v  total_pressure       4.9207e+05      5.2059e+05      5.1302e+05      5.1108e+05
v  Local Time Step           0.001        0.093401       0.0010945       0.0012174


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97391      2.3657e+05          30.577          2.1374


 TIME FOR THE TIME STEP              168:        0.72189E+02

===============================================================


 INSTANT    0.169000000E+01   TIME STEP NUMBER             169
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.162756003E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699329322E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41223E+01 0.21425E+01
   Friction velocity        uet   :  0.12241E-01 0.69342E+01
   Friction velocity        uk    :  0.12125E-01 0.69342E+01
   Dimensionless distance   yplus :  0.36731E-03 0.86513E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2810
   Nb of faces within the viscous sub-layer     :      28660
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31543E+01      21   0.28698E-01   0.63348E+00 0.14802E+02 
c  Velocity[X]                                      0.17840E+00 
c  Velocity[Y]                                      0.20709E+00 
c  Velocity[Z]                                      0.24798E+00 
c  Pressure     0.12522E-01     368   0.26199E-01   0.86197E-01 0.54095E+00 
c  k            0.39090E-01      18   0.14870E-03   0.15456E-03 0.24246E+02 
c  epsilon      0.21396E+03      11   0.34107E-03   0.29894E+05 0.91867E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028096                             6
a  epsilon                 -0.2474                            16
a  Local Time Step      4.2277e-08                        255312


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7081          5.8423          0.4677        0.078143
v  Velocity[Y]             -7.9183          6.5407         0.23661         0.18735
v  Velocity[Z]             -11.319          9.2227        -0.19844     -0.00073379
v  ǁVelocityǁ              0.00057          12.867          1.3758          1.5839
v  Pressure                -7944.9           20590           13019           11087
v  k                    3.2486e-08         0.83543       0.0065088       0.0080626
v  epsilon              7.4848e-05           31511          38.612           4.891
v  TurbVisc             5.8399e-13         0.14181      0.00049462        0.006402
v  CourantNb             0.0097191          906.15          8.6904          1.8238
v  FourierNb              0.025137      2.3653e+05          21.895         0.31394
v  total_pressure       4.9206e+05      5.2059e+05      5.1302e+05      5.1109e+05
v  Local Time Step           0.001        0.063012       0.0010937       0.0012143


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96449      2.3679e+05          30.585          2.1377


 TIME FOR THE TIME STEP              169:        0.66440E+02

===============================================================


 INSTANT    0.170000000E+01   TIME STEP NUMBER             170
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.222812687E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699301863E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43256E+01 0.21394E+01
   Friction velocity        uet   :  0.86867E-02 0.87704E+01
   Friction velocity        uk    :  0.86745E-02 0.87704E+01
   Dimensionless distance   yplus :  0.53524E-03 0.86478E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2814
   Nb of faces within the viscous sub-layer     :      28664
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31542E+01      19   0.28863E-01   0.61917E+00 0.14645E+02 
c  Velocity[X]                                      0.17960E+00 
c  Velocity[Y]                                      0.20914E+00 
c  Velocity[Z]                                      0.23043E+00 
c  Pressure     0.12493E-01     572   0.26128E-01   0.86080E-01 0.40936E+01 
c  k            0.39086E-01      11   0.37749E-03   0.11602E-03 0.21024E+02 
c  epsilon      0.21263E+03       9   0.24386E-03   0.17825E+05 0.71169E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002866                             7
a  epsilon                 -1.5042                            20
a  Local Time Step      4.2277e-08                        255367


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7133          5.8552         0.46809        0.078158
v  Velocity[Y]             -7.9861          6.5605         0.23622         0.18738
v  Velocity[Z]             -11.509          9.2265        -0.19895     -0.00089892
v  ǁVelocityǁ           0.00061325          12.936          1.3771          1.5844
v  Pressure                -7966.6           20661           13086           11145
v  k                    5.9006e-08         0.83589       0.0064908       0.0080643
v  epsilon              7.5881e-05           30863          38.251          4.8858
v  TurbVisc             6.6967e-13         0.14181      0.00049407       0.0064032
v  CourantNb             0.0050619          878.59          8.6948          1.8246
v  FourierNb              0.025137      2.3653e+05          21.894         0.31395
v  total_pressure       4.9203e+05      5.2066e+05      5.1309e+05      5.1115e+05
v  Local Time Step           0.001        0.056348       0.0010935       0.0012139


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98851      2.3662e+05          30.589          2.1385


 TIME FOR THE TIME STEP              170:        0.78868E+02

===============================================================


 INSTANT    0.171000000E+01   TIME STEP NUMBER             171
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.151247629E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699450504E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43045E+01 0.21404E+01
   Friction velocity        uet   :  0.17005E-01 0.62462E+01
   Friction velocity        uk    :  0.16776E-01 0.62462E+01
   Dimensionless distance   yplus :  0.79702E-03 0.86456E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2815
   Nb of faces within the viscous sub-layer     :      28644
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31546E+01      19   0.28877E-01   0.60713E+00 0.14483E+02 
c  Velocity[X]                                      0.17126E+00 
c  Velocity[Y]                                      0.20548E+00 
c  Velocity[Z]                                      0.23039E+00 
c  Pressure     0.12644E-01     313   0.26518E-01   0.87146E-01 0.52623E+00 
c  k            0.39096E-01      15   0.22219E-03   0.11128E-03 0.20441E+02 
c  epsilon      0.21479E+03      10   0.37115E-03   0.16629E+05 0.68437E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028005                             6
a  epsilon                -0.28499                            20
a  Local Time Step      4.2277e-08                        255436


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7196          5.8402          0.4685        0.078173
v  Velocity[Y]             -7.9069          6.5821         0.23577         0.18741
v  Velocity[Z]             -11.377          9.2374        -0.19918      -0.0010367
v  ǁVelocityǁ            0.0006177           12.77          1.3782           1.585
v  Pressure                -8028.3           20661           13085           11147
v  k                    2.1277e-08         0.83383       0.0065031       0.0080674
v  epsilon              7.1551e-05           31297          38.494          4.8927
v  TurbVisc             5.5753e-13         0.14181      0.00049334       0.0064043
v  CourantNb              0.012197          948.74          8.7018          1.8254
v  FourierNb              0.025138      2.3653e+05          21.894         0.31375
v  total_pressure       4.9197e+05      5.2066e+05      5.1309e+05      5.1115e+05
v  Local Time Step           0.001        0.061712       0.0010931       0.0012127


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.028      2.3656e+05          30.595          2.1392


 TIME FOR THE TIME STEP              171:        0.74414E+02

===============================================================


 INSTANT    0.172000000E+01   TIME STEP NUMBER             172
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.393824022E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699654897E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43334E+01 0.21412E+01
   Friction velocity        uet   :  0.95168E-02 0.52180E+01
   Friction velocity        uk    :  0.94474E-02 0.52180E+01
   Dimensionless distance   yplus :  0.55585E-03 0.86400E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2811
   Nb of faces within the viscous sub-layer     :      28634
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31552E+01      18   0.29000E-01   0.61451E+00 0.14587E+02 
c  Velocity[X]                                      0.17605E+00 
c  Velocity[Y]                                      0.20539E+00 
c  Velocity[Z]                                      0.23307E+00 
c  Pressure     0.12524E-01     693   0.26163E-01   0.86388E-01 0.26627E+01 
c  k            0.39097E-01      19   0.90488E-04   0.11443E-03 0.20847E+02 
c  epsilon      0.21402E+03      15   0.20352E-03   0.11766E+05 0.57699E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00029914                             6
a  epsilon                -0.36228                            19
a  Local Time Step      4.2277e-08                        255498


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7264             5.8         0.46861        0.078173
v  Velocity[Y]             -7.6688          6.6044         0.23546         0.18743
v  Velocity[Z]             -11.582          9.2232        -0.19945      -0.0011032
v  ǁVelocityǁ           0.00063156          12.886          1.3791          1.5854
v  Pressure                -8084.5           20619           13040           11110
v  k                    1.2645e-07         0.83729       0.0065038       0.0080704
v  epsilon              7.2955e-05           31035          38.367           4.894
v  TurbVisc             5.9306e-13         0.14181      0.00049286       0.0064054
v  CourantNb             0.0029447          895.36           8.709          1.8263
v  FourierNb              0.025137      2.3653e+05          21.893         0.31356
v  total_pressure       4.9192e+05      5.2062e+05      5.1304e+05      5.1111e+05
v  Local Time Step           0.001        0.058441       0.0010926       0.0012117


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0281      2.3713e+05          30.602          2.1399


 TIME FOR THE TIME STEP              172:        0.92491E+02

===============================================================


 INSTANT    0.173000000E+01   TIME STEP NUMBER             173
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.124703762E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699725477E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37658E+01 0.21397E+01
   Friction velocity        uet   :  0.17735E-01 0.56940E+01
   Friction velocity        uk    :  0.17727E-01 0.56940E+01
   Dimensionless distance   yplus :  0.28976E-03 0.86372E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2818
   Nb of faces within the viscous sub-layer     :      28649
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31549E+01      23   0.28846E-01   0.61097E+00 0.14530E+02 
c  Velocity[X]                                      0.17076E+00 
c  Velocity[Y]                                      0.21067E+00 
c  Velocity[Z]                                      0.22953E+00 
c  Pressure     0.12345E-01     306   0.26058E-01   0.85209E-01 0.51797E+00 
c  k            0.39095E-01      11   0.39338E-03   0.15115E-03 0.23921E+02 
c  epsilon      0.21424E+03       8   0.20859E-03   0.13300E+05 0.61349E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028921                             8
a  epsilon                -0.31728                            18
a  Local Time Step      4.2277e-08                        255510


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7297          5.7907         0.46878        0.078181
v  Velocity[Y]             -7.6451          6.6777         0.23513          0.1874
v  Velocity[Z]             -11.332          9.2305         -0.1997      -0.0011638
v  ǁVelocityǁ           0.00048031          12.681          1.3801          1.5858
v  Pressure                -8099.1           20621           13037           11112
v  k                    1.2936e-07         0.83505       0.0064961       0.0080723
v  epsilon              6.9561e-05           31339          38.341           4.892
v  TurbVisc             5.8727e-13         0.14181      0.00049223       0.0064064
v  CourantNb             0.0076035          883.81          8.7137           1.827
v  FourierNb              0.025137      2.3653e+05          21.892         0.31338
v  total_pressure        4.919e+05      5.2062e+05      5.1304e+05      5.1111e+05
v  Local Time Step           0.001        0.057112       0.0010923       0.0012106


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.86368      2.3661e+05          30.606          2.1404


 TIME FOR THE TIME STEP              173:        0.68462E+02

===============================================================


 INSTANT    0.174000000E+01   TIME STEP NUMBER             174
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.153763137E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699778351E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41997E+01 0.21377E+01
   Friction velocity        uet   :  0.12444E-01 0.86227E+01
   Friction velocity        uk    :  0.12404E-01 0.86227E+01
   Dimensionless distance   yplus :  0.67766E-03 0.86316E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2815
   Nb of faces within the viscous sub-layer     :      28624
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31548E+01      18   0.28652E-01   0.59627E+00 0.14346E+02 
c  Velocity[X]                                      0.17185E+00 
c  Velocity[Y]                                      0.20102E+00 
c  Velocity[Z]                                      0.22340E+00 
c  Pressure     0.12184E-01     738   0.25758E-01   0.84090E-01 0.18872E+01 
c  k            0.39102E-01      10   0.95213E-04   0.10425E-03 0.19505E+02 
c  epsilon      0.21527E+03      10   0.27105E-03   0.12013E+05 0.57802E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00029996                             7
a  epsilon                -0.32831                            22
a  Local Time Step      4.2277e-08                        255540


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7241          5.7645         0.46892        0.078216
v  Velocity[Y]             -7.5448          6.6978         0.23503         0.18737
v  Velocity[Z]             -11.626            9.24        -0.19995       -0.001111
v  ǁVelocityǁ           0.00031132          12.934          1.3812          1.5862
v  Pressure                -8177.3           20588           12997           11086
v  k                    1.2914e-07         0.83766       0.0065067       0.0080754
v  epsilon               7.036e-05           30888          38.512          4.8958
v  TurbVisc             6.1591e-13         0.14181      0.00049137       0.0064073
v  CourantNb             0.0056364          926.68          8.7184          1.8277
v  FourierNb              0.025137      2.3654e+05          21.892          0.3133
v  total_pressure       4.9182e+05      5.2059e+05        5.13e+05      5.1109e+05
v  Local Time Step           0.001        0.059825        0.001092       0.0012102


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.92604      2.3668e+05           30.61           2.141


 TIME FOR THE TIME STEP              174:        0.94246E+02

===============================================================


 INSTANT    0.175000000E+01   TIME STEP NUMBER             175
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.191335385E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699790326E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37446E+01 0.21411E+01
   Friction velocity        uet   :  0.10094E-01 0.63888E+01
   Friction velocity        uk    :  0.10087E-01 0.63888E+01
   Dimensionless distance   yplus :  0.46966E-03 0.86263E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2817
   Nb of faces within the viscous sub-layer     :      28631
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31543E+01      18   0.28859E-01   0.59033E+00 0.14287E+02 
c  Velocity[X]                                      0.16789E+00 
c  Velocity[Y]                                      0.19662E+00 
c  Velocity[Z]                                      0.22582E+00 
c  Pressure     0.12048E-01     283   0.25248E-01   0.83076E-01 0.46368E+00 
c  k            0.39099E-01       9   0.77793E-04   0.93835E-04 0.18891E+02 
c  epsilon      0.21481E+03       8   0.22323E-03   0.23042E+05 0.80660E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00029824                             9
a  epsilon                -0.31569                            21
a  Local Time Step      4.2277e-08                        255581


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7247          5.7682         0.46907        0.078249
v  Velocity[Y]             -7.4799          6.7234         0.23478         0.18732
v  Velocity[Z]             -11.378          9.2424         -0.2001       -0.001069
v  ǁVelocityǁ           0.00050549          12.693          1.3822          1.5866
v  Pressure                  -8213           20585           12996           11086
v  k                    1.2865e-07         0.83652       0.0064984       0.0080771
v  epsilon               1.229e-05           31360          38.319           4.895
v  TurbVisc             5.9639e-13         0.14181      0.00049077       0.0064083
v  CourantNb                     0          911.96          8.7264          1.8284
v  FourierNb              0.025137      2.3653e+05          21.891         0.31316
v  total_pressure       4.9179e+05      5.2058e+05        5.13e+05      5.1109e+05
v  Local Time Step           0.001        0.062382       0.0010917       0.0012095


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88327      2.3726e+05          30.617          2.1416


 TIME FOR THE TIME STEP              175:        0.67070E+02

===============================================================


 INSTANT    0.176000000E+01   TIME STEP NUMBER             176
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.917676541E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699741122E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42209E+01 0.21365E+01
   Friction velocity        uet   :  0.14630E-01 0.58266E+01
   Friction velocity        uk    :  0.14505E-01 0.58266E+01
   Dimensionless distance   yplus :  0.57695E-03 0.86170E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2818
   Nb of faces within the viscous sub-layer     :      28626
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31542E+01      19   0.29407E-01   0.59605E+00 0.14352E+02 
c  Velocity[X]                                      0.16702E+00 
c  Velocity[Y]                                      0.21324E+00 
c  Velocity[Z]                                      0.21579E+00 
c  Pressure     0.12137E-01     289   0.25395E-01   0.83695E-01 0.48334E+00 
c  k            0.39081E-01       9   0.17266E-03   0.98073E-04 0.19156E+02 
c  epsilon      0.20797E+03       7   0.23486E-03   0.24329E+05 0.83338E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003134                             7
a  epsilon                -0.49196                            19
a  Local Time Step      4.2277e-08                        255612


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7204          5.7322         0.46908        0.078241
v  Velocity[Y]             -7.9522          6.7684         0.23458         0.18729
v  Velocity[Z]             -11.647          9.2342        -0.20034      -0.0010373
v  ǁVelocityǁ           0.00065632          12.957          1.3831           1.587
v  Pressure                -8229.8           20585           12996           11086
v  k                    1.2844e-07         0.83907       0.0064979       0.0080792
v  epsilon              6.8647e-05           30841          38.347          4.8949
v  TurbVisc             5.9382e-13         0.14181      0.00049012        0.006409
v  CourantNb             0.0098807          880.61          8.7304          1.8291
v  FourierNb              0.025136      2.3653e+05          21.891         0.31307
v  total_pressure       4.9177e+05      5.2058e+05        5.13e+05      5.1109e+05
v  Local Time Step           0.001        0.059173       0.0010917       0.0012084


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91942      2.3664e+05          30.621          2.1422


 TIME FOR THE TIME STEP              176:        0.64309E+02

===============================================================


 INSTANT    0.177000000E+01   TIME STEP NUMBER             177
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.861570660E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699726536E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37302E+01 0.21439E+01
   Friction velocity        uet   :  0.13658E-01 0.61549E+01
   Friction velocity        uk    :  0.13622E-01 0.61549E+01
   Dimensionless distance   yplus :  0.60228E-03 0.86083E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2821
   Nb of faces within the viscous sub-layer     :      28612
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31539E+01      20   0.28837E-01   0.61004E+00 0.14515E+02 
c  Velocity[X]                                      0.17114E+00 
c  Velocity[Y]                                      0.20856E+00 
c  Velocity[Z]                                      0.23034E+00 
c  Pressure     0.12228E-01     543   0.25449E-01   0.84268E-01 0.53738E+00 
c  k            0.39100E-01      10   0.22493E-03   0.11254E-03 0.20599E+02 
c  epsilon      0.21336E+03       9   0.33972E-03   0.22409E+05 0.79499E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00030584                             7
a  epsilon                -0.35152                            22
a  Local Time Step      4.2277e-08                        255654


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7203          5.8312         0.46932        0.078268
v  Velocity[Y]             -7.9766          6.7752         0.23455         0.18728
v  Velocity[Z]             -11.335          9.2625        -0.20051       -0.001009
v  ǁVelocityǁ           0.00055416          12.713           1.384          1.5873
v  Pressure                -8217.8           20586           12995           11086
v  k                    1.2768e-07         0.83467       0.0065123       0.0080816
v  epsilon                 6.7e-05           31513            38.5          4.9029
v  TurbVisc             5.9163e-13         0.14181      0.00048946       0.0064097
v  CourantNb              0.011162          986.79          8.7358          1.8298
v  FourierNb              0.025136      2.3653e+05           21.89         0.31301
v  total_pressure       4.9178e+05      5.2059e+05        5.13e+05      5.1109e+05
v  Local Time Step           0.001        0.056391       0.0010916       0.0012079


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91203      2.3679e+05          30.626          2.1428


 TIME FOR THE TIME STEP              177:        0.67738E+02

===============================================================


 INSTANT    0.178000000E+01   TIME STEP NUMBER             178
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.113380269E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699677581E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41995E+01 0.21354E+01
   Friction velocity        uet   :  0.10965E-01 0.56813E+01
   Friction velocity        uk    :  0.10952E-01 0.56813E+01
   Dimensionless distance   yplus :  0.63118E-03 0.85992E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2824
   Nb of faces within the viscous sub-layer     :      28606
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31536E+01      19   0.28836E-01   0.60720E+00 0.14479E+02 
c  Velocity[X]                                      0.17434E+00 
c  Velocity[Y]                                      0.20294E+00 
c  Velocity[Z]                                      0.22992E+00 
c  Pressure     0.11902E-01     282   0.24862E-01   0.81968E-01 0.55169E+00 
c  k            0.39104E-01      10   0.98892E-04   0.98477E-04 0.19260E+02 
c  epsilon      0.21447E+03       9   0.25751E-03   0.15560E+05 0.66293E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00032214                             8
a  epsilon                -0.34814                            23
a  Local Time Step      4.2277e-08                        255689


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7087          5.6642         0.46943        0.078303
v  Velocity[Y]             -7.7324          6.8142         0.23453         0.18726
v  Velocity[Z]             -11.648          9.2388        -0.20092      -0.0010228
v  ǁVelocityǁ           0.00048206          12.969          1.3848          1.5876
v  Pressure                  -8249           20592           12994           11088
v  k                    1.2799e-07         0.83873       0.0064974       0.0080832
v  epsilon              6.7574e-05           30738          38.352          4.8993
v  TurbVisc             5.8854e-13         0.14181      0.00048881       0.0064103
v  CourantNb              0.011241          956.25          8.7414          1.8303
v  FourierNb              0.025136      2.3653e+05           21.89         0.31294
v  total_pressure       4.9175e+05      5.2059e+05      5.1299e+05      5.1109e+05
v  Local Time Step           0.001        0.052789       0.0010914       0.0012065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98514      2.3685e+05          30.631          2.1432


 TIME FOR THE TIME STEP              178:        0.64865E+02

===============================================================


 INSTANT    0.179000000E+01   TIME STEP NUMBER             179
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.267820180E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699695545E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36837E+01 0.21380E+01
   Friction velocity        uet   :  0.11551E-01 0.49239E+01
   Friction velocity        uk    :  0.11514E-01 0.49239E+01
   Dimensionless distance   yplus :  0.27946E-03 0.85868E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2830
   Nb of faces within the viscous sub-layer     :      28596
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31535E+01      20   0.28679E-01   0.61133E+00 0.14525E+02 
c  Velocity[X]                                      0.17953E+00 
c  Velocity[Y]                                      0.21210E+00 
c  Velocity[Z]                                      0.21970E+00 
c  Pressure     0.12177E-01     264   0.25619E-01   0.83909E-01 0.51066E+00 
c  k            0.39107E-01      10   0.79969E-04   0.10262E-03 0.19609E+02 
c  epsilon      0.21545E+03       7   0.17012E-03   0.95627E+04 0.51937E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00032654                             7
a  epsilon                -0.36361                            20
a  Local Time Step      4.2277e-08                        255631


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7146          5.7596         0.46944        0.078356
v  Velocity[Y]             -7.4502          6.8941         0.23453          0.1872
v  Velocity[Z]             -11.323          9.2541        -0.20132      -0.0010066
v  ǁVelocityǁ           0.00053734           12.64          1.3856          1.5879
v  Pressure                -8252.3           20590           12993           11089
v  k                    1.2443e-07         0.83643       0.0065052       0.0080857
v  epsilon              6.5657e-05           31228          38.392          4.9028
v  TurbVisc             5.8954e-13         0.14181      0.00048821        0.006411
v  CourantNb             0.0096696          963.31          8.7436          1.8309
v  FourierNb              0.025136      2.3653e+05           21.89         0.31286
v  total_pressure       4.9175e+05      5.2059e+05      5.1299e+05      5.1109e+05
v  Local Time Step           0.001        0.051644       0.0010913       0.0012052


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.92694      2.3656e+05          30.633          2.1438


 TIME FOR THE TIME STEP              179:        0.61502E+02

===============================================================


 INSTANT    0.180000000E+01   TIME STEP NUMBER             180
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.101898762E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699715800E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41025E+01 0.21386E+01
   Friction velocity        uet   :  0.16549E-01 0.63778E+01
   Friction velocity        uk    :  0.16466E-01 0.63778E+01
   Dimensionless distance   yplus :  0.39254E-03 0.85749E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2820
   Nb of faces within the viscous sub-layer     :      28588
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31534E+01      19   0.28404E-01   0.60087E+00 0.14391E+02 
c  Velocity[X]                                      0.16655E+00 
c  Velocity[Y]                                      0.20815E+00 
c  Velocity[Z]                                      0.22618E+00 
c  Pressure     0.12153E-01     254   0.25247E-01   0.83592E-01 0.47786E+00 
c  k            0.39125E-01      11   0.16039E-03   0.34803E-03 0.36427E+02 
c  epsilon      0.21693E+03       9   0.38299E-03   0.98405E+05 0.16517E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003303                             8
a  epsilon                -0.37565                            19
a  Local Time Step      4.2277e-08                        255669


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7007          5.7759         0.46946        0.078397
v  Velocity[Y]             -7.3158          6.9081         0.23474         0.18713
v  Velocity[Z]              -11.62          9.2525        -0.20166      -0.0010118
v  ǁVelocityǁ            0.0006145          12.926          1.3864          1.5883
v  Pressure                -8248.6           20590           12993           11090
v  k                    1.2438e-07         0.83594       0.0065064       0.0080884
v  epsilon              6.3286e-05           30950          38.396          4.9136
v  TurbVisc             5.6555e-13         0.14181      0.00048775       0.0064116
v  CourantNb             0.0025884          1000.1          8.7496          1.8315
v  FourierNb              0.025135      2.3653e+05          21.889         0.31281
v  total_pressure       4.9175e+05      5.2059e+05      5.1299e+05      5.1109e+05
v  Local Time Step           0.001        0.055344       0.0010914       0.0012048


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0281      2.3656e+05          30.639          2.1443


 TIME FOR THE TIME STEP              180:        0.57512E+02

===============================================================


 INSTANT    0.181000000E+01   TIME STEP NUMBER             181
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.284556532E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699715833E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37220E+01 0.21413E+01
   Friction velocity        uet   :  0.14294E-01 0.57944E+01
   Friction velocity        uk    :  0.14126E-01 0.57944E+01
   Dimensionless distance   yplus :  0.30198E-03 0.85610E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2819
   Nb of faces within the viscous sub-layer     :      28593
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31534E+01      20   0.28174E-01   0.59400E+00 0.14308E+02 
c  Velocity[X]                                      0.16572E+00 
c  Velocity[Y]                                      0.20420E+00 
c  Velocity[Z]                                      0.22408E+00 
c  Pressure     0.12052E-01     341   0.24947E-01   0.82800E-01 0.58976E+00 
c  k            0.39127E-01      10   0.20121E-03   0.14020E-03 0.22900E+02 
c  epsilon      0.21385E+03       9   0.31918E-03   0.28663E+05 0.88654E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00034484                             8
a  epsilon                -0.36967                            19
a  Local Time Step      4.2277e-08                        255716


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6986          5.7793         0.46953         0.07843
v  Velocity[Y]             -7.7933          6.9619         0.23499         0.18709
v  Velocity[Z]             -11.344          9.2492        -0.20178     -0.00097951
v  ǁVelocityǁ           0.00057446          12.668          1.3873          1.5887
v  Pressure                -8269.9           20595           12991           11093
v  k                    1.2028e-07         0.83839       0.0064999       0.0080901
v  epsilon              6.1257e-05           31347          38.243          4.9109
v  TurbVisc             5.9287e-13         0.14181      0.00048717       0.0064121
v  CourantNb            0.00086202          979.55          8.7544          1.8321
v  FourierNb              0.025135      2.3653e+05          21.889         0.31266
v  total_pressure       4.9173e+05       5.206e+05      5.1299e+05      5.1109e+05
v  Local Time Step           0.001        0.060878       0.0010912       0.0012034


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0281      2.3691e+05          30.643          2.1447


 TIME FOR THE TIME STEP              181:        0.67422E+02

===============================================================


 INSTANT    0.182000000E+01   TIME STEP NUMBER             182
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.139365969E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699771769E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42253E+01 0.21361E+01
   Friction velocity        uet   :  0.80483E-02 0.87389E+01
   Friction velocity        uk    :  0.80113E-02 0.87389E+01
   Dimensionless distance   yplus :  0.89561E-03 0.85446E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2823
   Nb of faces within the viscous sub-layer     :      28574
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31536E+01      20   0.28434E-01   0.58912E+00 0.14256E+02 
c  Velocity[X]                                      0.16552E+00 
c  Velocity[Y]                                      0.20625E+00 
c  Velocity[Z]                                      0.21735E+00 
c  Pressure     0.11848E-01     727   0.24456E-01   0.81335E-01 0.16111E+01 
c  k            0.39153E-01      10   0.25401E-03   0.13759E-03 0.22886E+02 
c  epsilon      0.22039E+03       8   0.33386E-03   0.22588E+05 0.79347E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00034163                             7
a  epsilon                -0.37713                            28
a  Local Time Step      4.2277e-08                        255718


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6986          5.7743         0.46961        0.078414
v  Velocity[Y]             -7.9419          6.9694         0.23515         0.18707
v  Velocity[Z]             -11.592          9.2335        -0.20208     -0.00090446
v  ǁVelocityǁ           0.00042935          12.888           1.388          1.5889
v  Pressure                -8305.7           20567           12963           11071
v  k                    2.4614e-08         0.83702       0.0065019       0.0080926
v  epsilon               5.963e-05           30821          38.351          4.9165
v  TurbVisc             6.3889e-13         0.14181      0.00048651       0.0064126
v  CourantNb            0.00010732          879.89           8.761          1.8327
v  FourierNb              0.025135      2.3653e+05          21.889         0.31247
v  total_pressure       4.9169e+05      5.2057e+05      5.1296e+05      5.1107e+05
v  Local Time Step           0.001         0.05775       0.0010909       0.0012021


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91974       2.367e+05           30.65          2.1452


 TIME FOR THE TIME STEP              182:        0.90882E+02

===============================================================


 INSTANT    0.183000000E+01   TIME STEP NUMBER             183
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.176308356E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699704572E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39810E+01 0.21371E+01
   Friction velocity        uet   :  0.13942E-01 0.70616E+01
   Friction velocity        uk    :  0.13937E-01 0.70616E+01
   Dimensionless distance   yplus :  0.34141E-03 0.85278E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2820
   Nb of faces within the viscous sub-layer     :      28563
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31532E+01      20   0.29264E-01   0.59612E+00 0.14326E+02 
c  Velocity[X]                                      0.16799E+00 
c  Velocity[Y]                                      0.20186E+00 
c  Velocity[Z]                                      0.22626E+00 
c  Pressure     0.12096E-01     204   0.24993E-01   0.82981E-01 0.39653E+00 
c  k            0.39181E-01       9   0.79195E-04   0.14717E-03 0.23621E+02 
c  epsilon      0.22445E+03       9   0.52070E-03   0.28154E+05 0.88375E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00035647                             6
a  epsilon                -0.37721                            21
a  Local Time Step      4.2277e-08                        255682


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6964           5.842         0.46982        0.078411
v  Velocity[Y]             -7.9357          6.9981         0.23531         0.18703
v  Velocity[Z]             -11.265          9.2521         -0.2024     -0.00087206
v  ǁVelocityǁ           0.00034115          12.729          1.3888          1.5892
v  Pressure                -8290.5           20570           12963           11071
v  k                    1.1269e-07         0.83417       0.0064964       0.0080957
v  epsilon              3.8981e-05           31157          38.153          4.9232
v  TurbVisc             5.4201e-13         0.14181      0.00048602        0.006413
v  CourantNb             0.0038569          910.51          8.7631          1.8332
v  FourierNb              0.025135      2.3653e+05          21.889         0.31243
v  total_pressure       4.9171e+05      5.2057e+05      5.1296e+05      5.1107e+05
v  Local Time Step           0.001         0.05512       0.0010908       0.0012011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0193       2.367e+05          30.652          2.1457


 TIME FOR THE TIME STEP              183:        0.61623E+02

===============================================================


 INSTANT    0.184000000E+01   TIME STEP NUMBER             184
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.145896719E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699648559E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42930E+01 0.21343E+01
   Friction velocity        uet   :  0.12674E-01 0.56678E+01
   Friction velocity        uk    :  0.12626E-01 0.56678E+01
   Dimensionless distance   yplus :  0.72322E-03 0.85108E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2818
   Nb of faces within the viscous sub-layer     :      28553
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31532E+01      20   0.29431E-01   0.60278E+00 0.14408E+02 
c  Velocity[X]                                      0.17522E+00 
c  Velocity[Y]                                      0.21007E+00 
c  Velocity[Z]                                      0.21749E+00 
c  Pressure     0.12363E-01     244   0.25245E-01   0.84566E-01 0.47335E+00 
c  k            0.39192E-01      10   0.15289E-03   0.11485E-03 0.20842E+02 
c  epsilon      0.22552E+03       9   0.50382E-03   0.17816E+05 0.70125E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00036008                             6
a  epsilon                -0.38104                            19
a  Local Time Step      4.2277e-08                        255655


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -2.69          5.7031         0.46979        0.078427
v  Velocity[Y]             -7.6695          7.0014         0.23562           0.187
v  Velocity[Z]              -11.59          9.2569        -0.20263     -0.00085107
v  ǁVelocityǁ           0.00031208          12.875          1.3894          1.5895
v  Pressure                -8268.1           20571           12963           11071
v  k                    1.0877e-07         0.83836        0.006513       0.0080977
v  epsilon              5.6458e-05           30791          38.422          4.9302
v  TurbVisc             5.8425e-13         0.14181      0.00048562       0.0064135
v  CourantNb             0.0030134          903.78          8.7702          1.8339
v  FourierNb              0.025134      2.3653e+05          21.888         0.31248
v  total_pressure       4.9173e+05      5.2057e+05      5.1296e+05      5.1107e+05
v  Local Time Step           0.001        0.060632       0.0010907       0.0012015


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85964      2.3679e+05          30.658          2.1463


 TIME FOR THE TIME STEP              184:        0.55743E+02

===============================================================


 INSTANT    0.185000000E+01   TIME STEP NUMBER             185
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.161358400E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699598571E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36808E+01 0.21391E+01
   Friction velocity        uet   :  0.11993E-01 0.72400E+01
   Friction velocity        uk    :  0.11990E-01 0.72400E+01
   Dimensionless distance   yplus :  0.27804E-03 0.84952E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2822
   Nb of faces within the viscous sub-layer     :      28546
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31528E+01      18   0.28560E-01   0.60823E+00 0.14481E+02 
c  Velocity[X]                                      0.17407E+00 
c  Velocity[Y]                                      0.20699E+00 
c  Velocity[Z]                                      0.22717E+00 
c  Pressure     0.12130E-01     290   0.24905E-01   0.82857E-01 0.49020E+00 
c  k            0.39194E-01      15   0.12149E-03   0.12060E-03 0.21381E+02 
c  epsilon      0.22550E+03      13   0.38672E-03   0.14514E+05 0.63285E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00035881                             9
a  epsilon                -0.38287                            19
a  Local Time Step      4.2277e-08                        255618


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7036          5.7603         0.46991        0.078452
v  Velocity[Y]             -7.5383          6.9957         0.23593         0.18698
v  Velocity[Z]             -11.194          9.2796        -0.20277      -0.0007953
v  ǁVelocityǁ           0.00032633          12.622            1.39          1.5897
v  Pressure                -8241.9           20576           12964           11074
v  k                    1.0318e-07         0.83407       0.0065184       0.0080991
v  epsilon              5.4887e-05           31312          38.528          4.9331
v  TurbVisc             5.8807e-13         0.14181      0.00048521       0.0064139
v  CourantNb            0.00099196          923.25          8.7664          1.8343
v  FourierNb              0.025134      2.3653e+05          21.888         0.31226
v  total_pressure       4.9176e+05      5.2058e+05      5.1296e+05      5.1107e+05
v  Local Time Step           0.001          0.0609       0.0010904       0.0012009


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88707      2.3666e+05          30.655          2.1466


 TIME FOR THE TIME STEP              185:        0.66384E+02

===============================================================


 INSTANT    0.186000000E+01   TIME STEP NUMBER             186
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.260538439E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699584773E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41991E+01 0.21308E+01
   Friction velocity        uet   :  0.10897E-01 0.65246E+01
   Friction velocity        uk    :  0.10894E-01 0.65246E+01
   Dimensionless distance   yplus :  0.83255E-03 0.84764E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2827
   Nb of faces within the viscous sub-layer     :      28549
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31529E+01      19   0.27711E-01   0.58089E+00 0.14158E+02 
c  Velocity[X]                                      0.16276E+00 
c  Velocity[Y]                                      0.19946E+00 
c  Velocity[Z]                                      0.21867E+00 
c  Pressure     0.11721E-01     202   0.24132E-01   0.80031E-01 0.40554E+00 
c  k            0.39198E-01      15   0.10171E-03   0.11209E-03 0.20500E+02 
c  epsilon      0.22626E+03      11   0.25719E-03   0.11218E+05 0.55657E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00035921                             6
a  epsilon                -0.38073                            21
a  Local Time Step      4.2277e-08                        255547


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7017          5.7431         0.47016        0.078424
v  Velocity[Y]             -7.5523           6.989         0.23621         0.18691
v  Velocity[Z]             -11.554          9.2901        -0.20294     -0.00076391
v  ǁVelocityǁ           0.00030862          12.829          1.3906          1.5901
v  Pressure                -8221.9           20574           12964           11074
v  k                    9.9051e-08         0.83249       0.0065018       0.0080993
v  epsilon              5.3451e-05           30654          38.281          4.9292
v  TurbVisc             6.2442e-13         0.14181      0.00048463       0.0064143
v  CourantNb             0.0017781          920.58          8.7758          1.8347
v  FourierNb              0.025134      2.3653e+05          21.888         0.31222
v  total_pressure       4.9178e+05      5.2057e+05      5.1296e+05      5.1107e+05
v  Local Time Step           0.001         0.06699       0.0010902          0.0012


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.84153      2.3656e+05          30.664           2.147


 TIME FOR THE TIME STEP              186:        0.64261E+02

===============================================================


 INSTANT    0.187000000E+01   TIME STEP NUMBER             187
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.126056331E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699534164E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38317E+01 0.21370E+01
   Friction velocity        uet   :  0.90233E-02 0.61323E+01
   Friction velocity        uk    :  0.90269E-02 0.61323E+01
   Dimensionless distance   yplus :  0.56188E-03 0.84572E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2830
   Nb of faces within the viscous sub-layer     :      28544
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31528E+01      20   0.28388E-01   0.58080E+00 0.14152E+02 
c  Velocity[X]                                      0.15830E+00 
c  Velocity[Y]                                      0.19636E+00 
c  Velocity[Z]                                      0.22614E+00 
c  Pressure     0.11657E-01     298   0.23921E-01   0.79351E-01 0.44814E+00 
c  k            0.39193E-01      11   0.79206E-04   0.79249E-04 0.17273E+02 
c  epsilon      0.22617E+03       8   0.15775E-03   0.65059E+04 0.42427E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00039002                             7
a  epsilon                -0.35946                            19
a  Local Time Step      4.2277e-08                        255533


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6986           5.734          0.4703        0.078403
v  Velocity[Y]             -7.5097          7.0246         0.23634         0.18687
v  Velocity[Z]             -11.178          9.2757        -0.20294     -0.00072591
v  ǁVelocityǁ           0.00018834          12.608           1.391          1.5903
v  Pressure                -8198.8           20575           12964           11075
v  k                    9.6534e-08         0.83492       0.0064988       0.0080993
v  epsilon              5.2285e-05           31232          38.263          4.9255
v  TurbVisc             5.6523e-13         0.14181      0.00048427       0.0064146
v  CourantNb             0.0047413          924.09          8.7797          1.8352
v  FourierNb              0.025134      2.3653e+05          21.888         0.31196
v  total_pressure        4.918e+05      5.2057e+05      5.1296e+05      5.1108e+05
v  Local Time Step           0.001        0.073689         0.00109       0.0011981


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73459      2.3716e+05          30.667          2.1472


 TIME FOR THE TIME STEP              187:        0.69527E+02

===============================================================


 INSTANT    0.188000000E+01   TIME STEP NUMBER             188
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.292265244E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699466291E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42248E+01 0.21358E+01
   Friction velocity        uet   :  0.75770E-02 0.51948E+01
   Friction velocity        uk    :  0.75304E-02 0.51948E+01
   Dimensionless distance   yplus :  0.46299E-03 0.84382E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2827
   Nb of faces within the viscous sub-layer     :      28528
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31528E+01      19   0.28402E-01   0.56712E+00 0.13985E+02 
c  Velocity[X]                                      0.16527E+00 
c  Velocity[Y]                                      0.19561E+00 
c  Velocity[Z]                                      0.20624E+00 
c  Pressure     0.11716E-01     351   0.24033E-01   0.79723E-01 0.70861E+00 
c  k            0.39191E-01      14   0.91016E-04   0.85598E-04 0.17991E+02 
c  epsilon      0.22486E+03      11   0.24666E-03   0.83153E+04 0.48057E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003575                             7
a  epsilon                -0.39727                            19
a  Local Time Step      4.2277e-08                        255503


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6964          5.7665         0.47013        0.078372
v  Velocity[Y]             -7.6873          6.9894          0.2366         0.18683
v  Velocity[Z]             -11.458          9.2749         -0.2031     -0.00068399
v  ǁVelocityǁ           3.2647e-05          12.726          1.3913          1.5906
v  Pressure                -8136.7           20583           12965           11082
v  k                    9.2895e-08          0.8359       0.0065062       0.0081011
v  epsilon              5.1077e-05           30839           38.36          4.9294
v  TurbVisc             5.8885e-13         0.14181      0.00048415        0.006415
v  CourantNb             0.0042742          907.12          8.7807          1.8356
v  FourierNb              0.025133      2.3653e+05          21.888         0.31183
v  total_pressure       4.9186e+05      5.2058e+05      5.1297e+05      5.1108e+05
v  Local Time Step           0.001        0.078586       0.0010898       0.0011962


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67373      2.3668e+05          30.669          2.1475


 TIME FOR THE TIME STEP              188:        0.69323E+02

===============================================================


 INSTANT    0.189000000E+01   TIME STEP NUMBER             189
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.234920785E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699468184E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40914E+01 0.21396E+01
   Friction velocity        uet   :  0.99143E-02 0.57265E+01
   Friction velocity        uk    :  0.99136E-02 0.57265E+01
   Dimensionless distance   yplus :  0.73071E-03 0.84218E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2833
   Nb of faces within the viscous sub-layer     :      28518
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31531E+01      19   0.28904E-01   0.57901E+00 0.14126E+02 
c  Velocity[X]                                      0.16938E+00 
c  Velocity[Y]                                      0.19687E+00 
c  Velocity[Z]                                      0.21276E+00 
c  Pressure     0.11779E-01     332   0.24083E-01   0.80052E-01 0.47685E+00 
c  k            0.39196E-01      11   0.11945E-03   0.11502E-03 0.20867E+02 
c  epsilon      0.22604E+03       8   0.34056E-03   0.13418E+05 0.60949E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00037032                             8
a  epsilon                -0.35816                            18
a  Local Time Step      4.2277e-08                        255460


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6964           5.732         0.47006        0.078325
v  Velocity[Y]             -7.5034          7.0054         0.23677         0.18681
v  Velocity[Z]             -11.216          9.2862        -0.20325     -0.00062018
v  ǁVelocityǁ           0.00022657          12.594          1.3916          1.5909
v  Pressure                -8027.2           20587           12967           11081
v  k                    9.0544e-08         0.83564        0.006501       0.0081027
v  epsilon              5.0114e-05           31338          38.236           4.931
v  TurbVisc             6.0651e-13         0.14181        0.000484       0.0064153
v  CourantNb             0.0012165          943.53           8.781           1.836
v  FourierNb              0.025133      2.3653e+05          21.888         0.31168
v  total_pressure       4.9197e+05      5.2059e+05      5.1297e+05      5.1108e+05
v  Local Time Step           0.001        0.073686       0.0010895       0.0011948


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5735      2.3673e+05          30.669          2.1477


 TIME FOR THE TIME STEP              189:        0.66024E+02

===============================================================


 INSTANT    0.190000000E+01   TIME STEP NUMBER             190
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.253485697E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699405343E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42803E+01 0.21294E+01
   Friction velocity        uet   :  0.12048E-01 0.67597E+01
   Friction velocity        uk    :  0.12043E-01 0.67597E+01
   Dimensionless distance   yplus :  0.48926E-03 0.84216E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2826
   Nb of faces within the viscous sub-layer     :      28524
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31529E+01      18   0.28976E-01   0.58842E+00 0.14254E+02 
c  Velocity[X]                                      0.16858E+00 
c  Velocity[Y]                                      0.20531E+00 
c  Velocity[Z]                                      0.21453E+00 
c  Pressure     0.11816E-01     276   0.24156E-01   0.80372E-01 0.51142E+00 
c  k            0.39192E-01      11   0.90803E-04   0.74695E-04 0.16776E+02 
c  epsilon      0.22493E+03       7   0.21142E-03   0.71695E+04 0.44614E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00039188                             8
a  epsilon                -0.38262                            21
a  Local Time Step      4.2277e-08                        255413


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6813          5.7659         0.47013        0.078307
v  Velocity[Y]             -7.8689          7.0025           0.237         0.18674
v  Velocity[Z]             -11.421          9.2826         -0.2035     -0.00063936
v  ǁVelocityǁ           0.00016893          12.744           1.392          1.5911
v  Pressure                  -7937           20589           12969           11084
v  k                    8.7925e-08         0.83562       0.0064968       0.0081029
v  epsilon              4.9232e-05           30550          38.178           4.927
v  TurbVisc             5.7495e-13         0.14181      0.00048392       0.0064156
v  CourantNb            0.00044723          914.29          8.7762          1.8364
v  FourierNb              0.025133      2.3653e+05          21.888         0.31158
v  total_pressure       4.9206e+05      5.2059e+05      5.1297e+05      5.1108e+05
v  Local Time Step           0.001        0.081054       0.0010894       0.0011946


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59366       2.368e+05          30.664           2.148


 TIME FOR THE TIME STEP              190:        0.63156E+02

===============================================================


 INSTANT    0.191000000E+01   TIME STEP NUMBER             191
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.147827913E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699387435E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41200E+01 0.21385E+01
   Friction velocity        uet   :  0.11532E-01 0.63296E+01
   Friction velocity        uk    :  0.11529E-01 0.63296E+01
   Dimensionless distance   yplus :  0.66480E-03 0.84207E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2836
   Nb of faces within the viscous sub-layer     :      28512
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31530E+01      18   0.28703E-01   0.58206E+00 0.14168E+02 
c  Velocity[X]                                      0.16990E+00 
c  Velocity[Y]                                      0.19622E+00 
c  Velocity[Z]                                      0.21593E+00 
c  Pressure     0.11605E-01     339   0.23760E-01   0.78841E-01 0.40210E+00 
c  k            0.39191E-01      10   0.11008E-03   0.93240E-04 0.18718E+02 
c  epsilon      0.22477E+03      11   0.24038E-03   0.72430E+04 0.44877E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00039097                             9
a  epsilon                -0.37203                            19
a  Local Time Step      4.2277e-08                        255421


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6897          5.7074         0.47027        0.078275
v  Velocity[Y]             -7.9965          6.9748         0.23717         0.18672
v  Velocity[Z]             -11.166          9.2788        -0.20367     -0.00063803
v  ǁVelocityǁ           0.00019817           12.46          1.3924          1.5914
v  Pressure                -7803.4           20592           12971           11085
v  k                    6.3877e-08         0.83315       0.0065035       0.0081047
v  epsilon               4.821e-05           31332          38.326          4.9287
v  TurbVisc             5.7464e-13         0.14181       0.0004838       0.0064159
v  CourantNb              0.002906          1037.6          8.7824          1.8369
v  FourierNb              0.025132      2.3653e+05          21.888         0.31158
v  total_pressure        4.922e+05      5.2059e+05      5.1297e+05      5.1108e+05
v  Local Time Step           0.001        0.077716       0.0010894       0.0011942


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82377      2.3714e+05           30.67          2.1485


 TIME FOR THE TIME STEP              191:        0.71374E+02

===============================================================


 INSTANT    0.192000000E+01   TIME STEP NUMBER             192
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.177040753E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699358594E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42355E+01 0.21368E+01
   Friction velocity        uet   :  0.12631E-01 0.51647E+01
   Friction velocity        uk    :  0.12626E-01 0.51647E+01
   Dimensionless distance   yplus :  0.56373E-03 0.84199E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2829
   Nb of faces within the viscous sub-layer     :      28508
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31531E+01      23   0.28480E-01   0.57636E+00 0.14094E+02 
c  Velocity[X]                                      0.16822E+00 
c  Velocity[Y]                                      0.19097E+00 
c  Velocity[Z]                                      0.21717E+00 
c  Pressure     0.11791E-01     277   0.24000E-01   0.80050E-01 0.50948E+00 
c  k            0.39194E-01       9   0.84620E-04   0.93362E-04 0.18828E+02 
c  epsilon      0.22533E+03      10   0.21442E-03   0.10580E+05 0.54281E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00038225                             9
a  epsilon                -0.36604                            18
a  Local Time Step      4.2277e-08                        255402


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6888          5.6655         0.47047        0.078259
v  Velocity[Y]             -7.8045          6.9663         0.23735         0.18669
v  Velocity[Z]             -11.394          9.2984        -0.20377     -0.00063732
v  ǁVelocityǁ           5.3581e-05          12.636          1.3929          1.5918
v  Pressure                -7708.2           20597           12972           11089
v  k                    8.4456e-08         0.83719        0.006495        0.008106
v  epsilon              4.7341e-05           30862          38.097          4.9285
v  TurbVisc             5.6449e-13         0.14181      0.00048372       0.0064163
v  CourantNb             0.0037163          897.58          8.7819          1.8373
v  FourierNb              0.025132      2.3653e+05          21.888         0.31156
v  total_pressure       4.9229e+05       5.206e+05      5.1297e+05      5.1109e+05
v  Local Time Step           0.001        0.085488       0.0010894       0.0011942


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0281      2.3658e+05          30.669          2.1488


 TIME FOR THE TIME STEP              192:        0.59068E+02

===============================================================


 INSTANT    0.193000000E+01   TIME STEP NUMBER             193
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.679386281E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699353738E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36748E+01 0.21361E+01
   Friction velocity        uet   :  0.71753E-02 0.59725E+01
   Friction velocity        uk    :  0.71749E-02 0.59725E+01
   Dimensionless distance   yplus :  0.50584E-03 0.84187E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2830
   Nb of faces within the viscous sub-layer     :      28487
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31535E+01      19   0.28760E-01   0.58418E+00 0.14182E+02 
c  Velocity[X]                                      0.16946E+00 
c  Velocity[Y]                                      0.19572E+00 
c  Velocity[Z]                                      0.21899E+00 
c  Pressure     0.11672E-01     349   0.23780E-01   0.79197E-01 0.64529E+00 
c  k            0.39195E-01      10   0.10323E-03   0.97264E-04 0.19172E+02 
c  epsilon      0.22541E+03       9   0.24851E-03   0.11538E+05 0.56597E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00037956                             9
a  epsilon                -0.35877                            17
a  Local Time Step      4.2277e-08                        255384


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6923          5.6397         0.47051        0.078232
v  Velocity[Y]             -7.5495          7.0146          0.2375         0.18668
v  Velocity[Z]             -11.149          9.2871        -0.20389     -0.00063083
v  ǁVelocityǁ           0.00010194          12.416          1.3933          1.5921
v  Pressure                -7662.1           20597           12976           11095
v  k                    8.2849e-08         0.83368       0.0065033       0.0081086
v  epsilon              4.6395e-05           31150          38.251           4.934
v  TurbVisc             5.8666e-13         0.14181      0.00048368       0.0064167
v  CourantNb            7.4751e-05          904.37          8.7899          1.8378
v  FourierNb              0.025132      2.3653e+05          21.887         0.31146
v  total_pressure       4.9234e+05       5.206e+05      5.1298e+05       5.111e+05
v  Local Time Step           0.001        0.091551       0.0010893        0.001192


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0281      2.3675e+05          30.677          2.1492


 TIME FOR THE TIME STEP              193:        0.72232E+02

===============================================================


 INSTANT    0.194000000E+01   TIME STEP NUMBER             194
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.690993137E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699395748E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40464E+01 0.21355E+01
   Friction velocity        uet   :  0.67915E-02 0.50264E+01
   Friction velocity        uk    :  0.67911E-02 0.50264E+01
   Dimensionless distance   yplus :  0.51360E-03 0.84167E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2825
   Nb of faces within the viscous sub-layer     :      28487
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31541E+01      20   0.28218E-01   0.57836E+00 0.14093E+02 
c  Velocity[X]                                      0.17682E+00 
c  Velocity[Y]                                      0.19019E+00 
c  Velocity[Z]                                      0.21135E+00 
c  Pressure     0.11862E-01     443   0.24189E-01   0.80400E-01 0.62407E+00 
c  k            0.39197E-01       9   0.10353E-03   0.11843E-03 0.21143E+02 
c  epsilon      0.22545E+03       8   0.24484E-03   0.12622E+05 0.59249E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00040407                            12
a  epsilon                -0.34931                            25
a  Local Time Step      4.2277e-08                        255366


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6818          5.7073         0.47053        0.078222
v  Velocity[Y]             -7.6491          6.9902         0.23778         0.18662
v  Velocity[Z]             -11.441          9.7817        -0.20414     -0.00066328
v  ǁVelocityǁ           2.4702e-05          12.688          1.3938          1.5924
v  Pressure                -7637.8           20597           12980           11100
v  k                    8.1488e-08         0.83627       0.0065028       0.0081099
v  epsilon              4.5504e-05           30816          38.123          4.9327
v  TurbVisc             6.0161e-13         0.14181      0.00048381       0.0064171
v  CourantNb            0.00082272          860.33          8.7889          1.8382
v  FourierNb              0.025131      2.3653e+05          21.887         0.31148
v  total_pressure       4.9236e+05       5.206e+05      5.1298e+05       5.111e+05
v  Local Time Step           0.001         0.10071       0.0010892       0.0011917


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74881      2.3687e+05          30.676          2.1496


 TIME FOR THE TIME STEP              194:        0.70775E+02

===============================================================


 INSTANT    0.195000000E+01   TIME STEP NUMBER             195
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.876343803E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699485461E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39661E+01 0.21373E+01
   Friction velocity        uet   :  0.54818E-02 0.73660E+01
   Friction velocity        uk    :  0.54816E-02 0.73660E+01
   Dimensionless distance   yplus :  0.93990E-03 0.84166E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2831
   Nb of faces within the viscous sub-layer     :      28484
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31549E+01      20   0.28588E-01   0.56444E+00 0.13894E+02 
c  Velocity[X]                                      0.16108E+00 
c  Velocity[Y]                                      0.18969E+00 
c  Velocity[Z]                                      0.21367E+00 
c  Pressure     0.12269E-01     399   0.24968E-01   0.83152E-01 0.53419E+00 
c  k            0.39198E-01      11   0.90066E-04   0.97037E-04 0.18886E+02 
c  epsilon      0.22587E+03      12   0.28345E-03   0.18776E+05 0.72091E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00040122                             9
a  epsilon                -0.36792                            19
a  Local Time Step      4.2277e-08                        255376


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6828          5.7171          0.4708        0.078238
v  Velocity[Y]             -7.7472          6.9978          0.2381         0.18665
v  Velocity[Z]             -11.123          9.3119        -0.20434     -0.00072392
v  ǁVelocityǁ           2.3401e-05          12.583          1.3944          1.5927
v  Pressure                -7572.3           20606           12984           11103
v  k                    8.0078e-08         0.83454       0.0065142       0.0081112
v  epsilon              4.4543e-05           31230          38.531          4.9334
v  TurbVisc             5.7622e-13         0.14181      0.00048396       0.0064176
v  CourantNb              0.000541          895.11          8.7915          1.8386
v  FourierNb              0.025131      2.3653e+05          21.887         0.31158
v  total_pressure       4.9243e+05      5.2061e+05      5.1298e+05       5.111e+05
v  Local Time Step           0.001         0.11078       0.0010894        0.001192


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.93056      2.3663e+05          30.679          2.1502


 TIME FOR THE TIME STEP              195:        0.73237E+02

===============================================================


 INSTANT    0.196000000E+01   TIME STEP NUMBER             196
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.490140590E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699506129E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42371E+01 0.21394E+01
   Friction velocity        uet   :  0.54958E-02 0.55497E+01
   Friction velocity        uk    :  0.54955E-02 0.55497E+01
   Dimensionless distance   yplus :  0.56227E-03 0.84153E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2828
   Nb of faces within the viscous sub-layer     :      28477
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31554E+01      21   0.29582E-01   0.57344E+00 0.14020E+02 
c  Velocity[X]                                      0.16830E+00 
c  Velocity[Y]                                      0.18994E+00 
c  Velocity[Z]                                      0.21520E+00 
c  Pressure     0.12520E-01     313   0.25301E-01   0.84710E-01 0.43612E+00 
c  k            0.39192E-01      12   0.86907E-04   0.95998E-04 0.18976E+02 
c  epsilon      0.22417E+03      10   0.23046E-03   0.11576E+05 0.56759E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002667                             9
a  epsilon                -0.34216                            17
a  Local Time Step      4.2277e-08                        255349


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6782            5.69         0.47109         0.07825
v  Velocity[Y]             -7.8284               7          0.2384         0.18664
v  Velocity[Z]             -11.456          9.3208        -0.20459       -0.000753
v  ǁVelocityǁ           7.4518e-05          12.688          1.3949          1.5931
v  Pressure                -7519.1           20608           12985           11103
v  k                    1.4518e-08         0.83558        0.006509       0.0081129
v  epsilon              4.3757e-05           30964           38.25          4.9353
v  TurbVisc             5.7303e-13         0.14181      0.00048416        0.006418
v  CourantNb            0.00097225          1030.2           8.797          1.8392
v  FourierNb               0.02513      2.3653e+05          21.887         0.31168
v  total_pressure       4.9248e+05      5.2061e+05      5.1298e+05       5.111e+05
v  Local Time Step           0.001         0.12185       0.0010895       0.0011923


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.93791      2.3679e+05          30.684          2.1509


 TIME FOR THE TIME STEP              196:        0.66309E+02

===============================================================


 INSTANT    0.197000000E+01   TIME STEP NUMBER             197
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.276979318E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699517089E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41673E+01 0.21390E+01
   Friction velocity        uet   :  0.85095E-02 0.58408E+01
   Friction velocity        uk    :  0.85093E-02 0.58408E+01
   Dimensionless distance   yplus :  0.47520E-03 0.84141E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2829
   Nb of faces within the viscous sub-layer     :      28479
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31557E+01      18   0.29038E-01   0.58839E+00 0.14215E+02 
c  Velocity[X]                                      0.17216E+00 
c  Velocity[Y]                                      0.19260E+00 
c  Velocity[Z]                                      0.22363E+00 
c  Pressure     0.12450E-01     277   0.25353E-01   0.84376E-01 0.46318E+00 
c  k            0.39191E-01      10   0.91415E-04   0.76969E-04 0.17027E+02 
c  epsilon      0.22469E+03       8   0.23237E-03   0.77140E+04 0.46255E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022298                             8
a  epsilon                -0.28589                            19
a  Local Time Step      4.2277e-08                        255405


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6871          5.7213         0.47129        0.078298
v  Velocity[Y]             -7.6167          7.0137         0.23855         0.18665
v  Velocity[Z]             -11.091          9.2979        -0.20487     -0.00076517
v  ǁVelocityǁ           8.8928e-05           12.58          1.3955          1.5934
v  Pressure                -7501.5           20610           12985           11104
v  k                    1.5201e-09         0.83561       0.0065101       0.0081141
v  epsilon              4.3043e-05           31262          38.307          4.9357
v  TurbVisc             5.9887e-13         0.14181      0.00048421       0.0064183
v  CourantNb             0.0014376          1100.6          8.8032          1.8397
v  FourierNb               0.02513      2.3653e+05          21.887         0.31166
v  total_pressure        4.925e+05      5.2061e+05      5.1298e+05       5.111e+05
v  Local Time Step           0.001         0.10548       0.0010895       0.0011916


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64017      2.3723e+05           30.69          2.1514


 TIME FOR THE TIME STEP              197:        0.66532E+02

===============================================================


 INSTANT    0.198000000E+01   TIME STEP NUMBER             198
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.337499777E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699560212E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42363E+01 0.21385E+01
   Friction velocity        uet   :  0.12128E-01 0.61710E+01
   Friction velocity        uk    :  0.12128E-01 0.61710E+01
   Dimensionless distance   yplus :  0.78742E-03 0.84138E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2831
   Nb of faces within the viscous sub-layer     :      28464
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31563E+01      22   0.28623E-01   0.57515E+00 0.14054E+02 
c  Velocity[X]                                      0.16523E+00 
c  Velocity[Y]                                      0.19752E+00 
c  Velocity[Z]                                      0.21239E+00 
c  Pressure     0.12285E-01     320   0.25093E-01   0.83261E-01 0.48272E+00 
c  k            0.39190E-01       9   0.95398E-04   0.82056E-04 0.17604E+02 
c  epsilon      0.22433E+03       8   0.23887E-03   0.91858E+04 0.50516E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023283                             7
a  epsilon                -0.27832                            23
a  Local Time Step      4.2277e-08                        255420


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6978          5.7212         0.47145        0.078312
v  Velocity[Y]              -7.432          7.0357         0.23875         0.18665
v  Velocity[Z]             -11.468          9.3071        -0.20512     -0.00077204
v  ǁVelocityǁ           6.8447e-05          12.719           1.396          1.5937
v  Pressure                -7442.9           20611           12985           11105
v  k                    7.7497e-08         0.83535       0.0065141       0.0081154
v  epsilon              4.2384e-05           30911          38.334          4.9363
v  TurbVisc             2.3657e-13         0.14181      0.00048434       0.0064185
v  CourantNb             0.0016252          891.17          8.8074          1.8402
v  FourierNb               0.02513      2.3653e+05          21.887         0.31162
v  total_pressure       4.9256e+05      5.2061e+05      5.1298e+05      5.1111e+05
v  Local Time Step           0.001         0.11603       0.0010896       0.0011903


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52719      2.3672e+05          30.694          2.1518


 TIME FOR THE TIME STEP              198:        0.68366E+02

===============================================================


 INSTANT    0.199000000E+01   TIME STEP NUMBER             199
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.219677645E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699566801E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41126E+01 0.21366E+01
   Friction velocity        uet   :  0.88766E-02 0.73680E+01
   Friction velocity        uk    :  0.88764E-02 0.73680E+01
   Dimensionless distance   yplus :  0.76665E-03 0.84131E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2835
   Nb of faces within the viscous sub-layer     :      28463
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31567E+01      19   0.28977E-01   0.57700E+00 0.14075E+02 
c  Velocity[X]                                      0.17007E+00 
c  Velocity[Y]                                      0.18902E+00 
c  Velocity[Z]                                      0.21791E+00 
c  Pressure     0.11932E-01     265   0.24270E-01   0.80880E-01 0.47718E+00 
c  k            0.39183E-01       9   0.72981E-04   0.68379E-04 0.16071E+02 
c  epsilon      0.22275E+03       9   0.16491E-03   0.50515E+04 0.37533E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022569                             7
a  epsilon                -0.26995                            22
a  Local Time Step      4.2277e-08                        255458


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7004          5.7054         0.47156        0.078282
v  Velocity[Y]              -7.828          7.0343         0.23895         0.18665
v  Velocity[Z]             -11.157          9.3229        -0.20543     -0.00079345
v  ǁVelocityǁ           0.00018694           12.56          1.3964           1.594
v  Pressure                -7392.3           20613           12984           11107
v  k                    7.6863e-08         0.83676       0.0065086       0.0081165
v  epsilon              4.1746e-05           31190          38.207          4.9341
v  TurbVisc             5.6199e-13         0.14181      0.00048456       0.0064188
v  CourantNb               0.00183          887.46          8.8116          1.8407
v  FourierNb               0.02513      2.3653e+05          21.887         0.31152
v  total_pressure       4.9261e+05      5.2061e+05      5.1298e+05      5.1111e+05
v  Local Time Step           0.001        0.086348       0.0010896       0.0011884


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71178      2.3681e+05          30.698          2.1522


 TIME FOR THE TIME STEP              199:        0.72597E+02

===============================================================


 INSTANT    0.200000000E+01   TIME STEP NUMBER             200
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.203344963E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699594215E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42866E+01 0.21376E+01
   Friction velocity        uet   :  0.64170E-02 0.49578E+01
   Friction velocity        uk    :  0.63864E-02 0.49578E+01
   Dimensionless distance   yplus :  0.61975E-03 0.84122E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2829
   Nb of faces within the viscous sub-layer     :      28444
   Total number of wall faces                   :      41000
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        200, Physical time    0.20000E+01


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint/main
 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                            
  Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary
 End writing


 Time for restart files:    0.74298E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31571E+01      18   0.28349E-01   0.57399E+00 0.14043E+02 
c  Velocity[X]                                      0.18263E+00 
c  Velocity[Y]                                      0.18908E+00 
c  Velocity[Z]                                      0.20228E+00 
c  Pressure     0.11963E-01     195   0.24318E-01   0.80981E-01 0.42710E+00 
c  k            0.39181E-01      10   0.10446E-03   0.99758E-04 0.19396E+02 
c  epsilon      0.22194E+03      10   0.23235E-03   0.91419E+04 0.50429E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023109                             7
a  epsilon                -0.27455                            22
a  Local Time Step      4.2277e-08                        255459


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6906          5.7032         0.47179         0.07824
v  Velocity[Y]             -8.0098          7.0244         0.23917         0.18661
v  Velocity[Z]             -11.419          9.3226        -0.20579     -0.00078868
v  ǁVelocityǁ           5.8655e-05          12.668          1.3969          1.5943
v  Pressure                -7379.1           20609           12984           11108
v  k                    7.6392e-08         0.83719       0.0065289       0.0081186
v  epsilon               4.113e-05           30942          38.404          4.9423
v  TurbVisc             5.7678e-13         0.14181      0.00048481        0.006419
v  CourantNb             0.0027537          897.57          8.8144           1.841
v  FourierNb               0.02513      2.3653e+05          21.886         0.31157
v  total_pressure       4.9262e+05      5.2061e+05      5.1298e+05      5.1111e+05
v  Local Time Step           0.001        0.094983       0.0010898       0.0011888


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68125      2.3655e+05          30.701          2.1526


 TIME FOR THE TIME STEP              200:        0.73555E+02

===============================================================


 INSTANT    0.201000000E+01   TIME STEP NUMBER             201
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.215737897E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640810E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41873E+01 0.21357E+01
   Friction velocity        uet   :  0.11934E-01 0.39676E+01
   Friction velocity        uk    :  0.11933E-01 0.39676E+01
   Dimensionless distance   yplus :  0.45628E-03 0.84122E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2836
   Nb of faces within the viscous sub-layer     :      28441
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31676E+01      18   0.28764E-01   0.19369E+03 0.20314E+03 
c  Velocity[X]                                      0.79108E+01 
c  Velocity[Y]                                      0.15679E+02 
c  Velocity[Z]                                      0.17010E+03 
c  Pressure     0.30194E-01    5244   0.96859E+00   0.20081E+00 0.83051E+03 
c  k            0.43649E-01      19   0.86818E-03   0.26000E-02 0.93106E+02 
c  epsilon      0.22367E+03      15   0.78063E-03   0.30448E+05 0.93692E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.8632e-05                             2
a  epsilon                 -0.1607                            12
a  Local Time Step      4.2277e-08                        255496


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.5715           6.993         0.55251         0.10414
v  Velocity[Y]             -9.4488          8.2935         0.33968         0.24361
v  Velocity[Z]             -12.411          10.054        -0.22343       0.0011079
v  ǁVelocityǁ            0.0037214          14.352          1.5839          1.9941
v  Pressure                 307.36      1.9168e+05      1.0177e+05           98119
v  k                    7.6286e-08         0.81087       0.0066914       0.0084034
v  epsilon               4.072e-05           29505          39.043          5.0507
v  TurbVisc              5.851e-13         0.14181      0.00048503       0.0064192
v  CourantNb             0.0019106          901.11          8.8155          1.8415
v  FourierNb               0.02513      2.3653e+05          21.887         0.31169
v  total_pressure       5.0031e+05      6.9168e+05      6.0177e+05      5.9812e+05
v  Local Time Step           0.001         0.10448         0.00109       0.0011883


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0282      2.3665e+05          30.702          2.1532


 TIME FOR THE TIME STEP              201:        0.37963E+03

===============================================================


 INSTANT    0.202000000E+01   TIME STEP NUMBER             202
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.184243894E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989549181E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60008E+01 0.23192E+01
   Friction velocity        uet   :  0.10803E-01 0.17936E+02
   Friction velocity        uk    :  0.13713E-01 0.17936E+02
   Dimensionless distance   yplus :  0.20295E-02 0.95087E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3681
   Nb of faces within the viscous sub-layer     :      26147
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.53015E+01      38   0.26089E-01   0.64199E+02 0.10883E+03 
c  Velocity[X]                                      0.38716E+01 
c  Velocity[Y]                                      0.79481E+01 
c  Velocity[Z]                                      0.52379E+02 
c  Pressure     0.14617E+00    1757   0.21179E+00   0.89024E+00 0.47294E+03 
c  k            0.51032E-01      23   0.29713E-02   0.24825E-01 0.25189E+03 
c  epsilon      0.49567E+03      21   0.48984E-02   0.92970E+07 0.76685E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.9406e-06                             1
a  epsilon               -0.044291                             1
a  Local Time Step      4.2277e-08                        268806


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6273          6.5697         0.59657         0.11412
v  Velocity[Y]             -9.3171           8.835         0.38348         0.27244
v  Velocity[Z]             -13.008          10.497        -0.22608       0.0028409
v  ǁVelocityǁ           0.00030892          14.788          1.6792          2.2079
v  Pressure                 144.02      1.2623e+05           70147           65663
v  k                    7.5046e-08          1.4009       0.0091639       0.0092333
v  epsilon              3.9953e-05           87838          82.923          7.6155
v  TurbVisc             6.2281e-13          0.1571      0.00049582       0.0066393
v  CourantNb             0.0044154            1717          10.461          2.2999
v  FourierNb              0.022226      2.3654e+05          21.777         0.28518
v  total_pressure       5.0014e+05      6.2623e+05      5.7015e+05      5.6566e+05
v  Local Time Step           0.001        0.024021       0.0010192       0.0010577


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42669      2.3696e+05          32.238          2.5851


 TIME FOR THE TIME STEP              202:        0.16591E+03

===============================================================


 INSTANT    0.203000000E+01   TIME STEP NUMBER             203
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.665515440E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989160412E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66026E+01 0.24865E+01
   Friction velocity        uet   :  0.20085E-01 0.18619E+02
   Friction velocity        uk    :  0.20084E-01 0.18619E+02
   Dimensionless distance   yplus :  0.12590E-02 0.10011E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3874
   Nb of faces within the viscous sub-layer     :      25832
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54028E+01      37   0.24711E-01   0.68486E+01 0.34963E+02 
c  Velocity[X]                                      0.15437E+01 
c  Velocity[Y]                                      0.27785E+01 
c  Velocity[Z]                                      0.25265E+01 
c  Pressure     0.51173E-01    3759   0.42710E+00   0.28975E+00 0.15302E+04 
c  k            0.53311E-01      19   0.19319E-02   0.11659E-01 0.16748E+03 
c  epsilon      0.44297E+03      14   0.37300E-02   0.51781E+07 0.83100E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0018006                            42
a  epsilon                 -20.792                            72
a  Local Time Step      4.2277e-08                        265910


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6307          6.8638         0.61205         0.11385
v  Velocity[Y]             -8.3063          10.252         0.38152         0.27442
v  Velocity[Z]             -14.151          10.658        -0.23178      1.2807e-06
v  ǁVelocityǁ            0.0011051          16.009          1.7191          2.2323
v  Pressure                -4721.9           43517           28621           23972
v  k                    6.9165e-08          1.0253       0.0084806       0.0095527
v  epsilon              3.9239e-05           64684          62.211          6.9111
v  TurbVisc             6.0062e-13         0.16447      0.00050375       0.0067578
v  CourantNb             0.0022166          3080.3          10.423          2.3216
v  FourierNb              0.022225      2.3654e+05          21.788         0.28631
v  total_pressure       4.9528e+05      5.4352e+05      5.2862e+05      5.2397e+05
v  Local Time Step           0.001          0.0217       0.0010222        0.001061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54058      2.3726e+05           32.21          2.6079


 TIME FOR THE TIME STEP              203:        0.27986E+03

===============================================================


 INSTANT    0.204000000E+01   TIME STEP NUMBER             204
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.428329504E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989969621E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.78899E+01 0.24811E+01
   Friction velocity        uet   :  0.12413E-01 0.20682E+02
   Friction velocity        uk    :  0.12276E-01 0.20682E+02
   Dimensionless distance   yplus :  0.18375E-02 0.99878E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3947
   Nb of faces within the viscous sub-layer     :      25774
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.49683E+01      34   0.26077E-01   0.80734E+01 0.38559E+02 
c  Velocity[X]                                      0.11759E+01 
c  Velocity[Y]                                      0.25323E+01 
c  Velocity[Z]                                      0.43652E+01 
c  Pressure     0.81508E-01    2277   0.25762E+00   0.43905E+00 0.10451E+04 
c  k            0.55057E-01      19   0.44354E-03   0.24133E-02 0.76017E+02 
c  epsilon      0.43026E+03      16   0.14673E-02   0.10569E+07 0.34294E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.7738e-05                            17
a  epsilon                -0.24983                            27
a  Local Time Step      4.2277e-08                        265692


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.6673          7.0423         0.61559         0.11179
v  Velocity[Y]             -9.6674          10.945         0.36513         0.26768
v  Velocity[Z]             -14.928          11.014        -0.23604      -0.0021472
v  ǁVelocityǁ            0.0002822          16.799          1.7362          2.1933
v  Pressure                 -20360           25838           13620          9305.9
v  k                    1.2756e-08           1.266       0.0091087       0.0098547
v  epsilon              3.8407e-05      1.2017e+05          73.755          7.2351
v  TurbVisc              6.769e-13         0.16698       0.0005043       0.0068409
v  CourantNb            0.00033707          3246.7          10.631          2.3428
v  FourierNb              0.022224      2.3654e+05          21.792         0.28711
v  total_pressure       4.7964e+05      5.2584e+05      5.1362e+05      5.0931e+05
v  Local Time Step           0.001        0.015467       0.0010243       0.0010635


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50876      2.3787e+05          32.423          2.6299


 TIME FOR THE TIME STEP              204:        0.19534E+03

===============================================================


 INSTANT    0.205000000E+01   TIME STEP NUMBER             205
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.319651693E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989840348E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87041E+01 0.26490E+01
   Friction velocity        uet   :  0.12604E-01 0.18910E+02
   Friction velocity        uk    :  0.12602E-01 0.18910E+02
   Dimensionless distance   yplus :  0.20134E-02 0.98419E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3980
   Nb of faces within the viscous sub-layer     :      25823
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46974E+01      35   0.29569E-01   0.58960E+01 0.33234E+02 
c  Velocity[X]                                      0.10802E+01 
c  Velocity[Y]                                      0.21857E+01 
c  Velocity[Z]                                      0.26301E+01 
c  Pressure     0.56384E-01    1590   0.94287E-01   0.29213E+00 0.19574E+03 
c  k            0.56474E-01      19   0.31217E-03   0.17233E-02 0.63093E+02 
c  epsilon      0.43328E+03      17   0.96485E-03   0.60182E+06 0.25819E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -4.586e-06                             8
a  epsilon                 -1.6641                             6
a  Local Time Step      4.2277e-08                        265550


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.7228          7.7068         0.62035          0.1111
v  Velocity[Y]             -10.012          11.905         0.35379         0.26333
v  Velocity[Z]             -15.746          11.521        -0.23613      -0.0020682
v  ǁVelocityǁ           0.00029347          17.625          1.7537          2.1694
v  Pressure                 -18024           28887           16573           12553
v  k                    1.1375e-08           1.025       0.0093991        0.010049
v  epsilon              2.2568e-05           53224          76.299          7.3176
v  TurbVisc             7.2035e-13         0.16786      0.00051349       0.0069307
v  CourantNb             0.0021281          2322.8           10.84          2.3592
v  FourierNb              0.022222      2.3653e+05          21.799         0.28804
v  total_pressure       4.8198e+05      5.2889e+05      5.1657e+05      5.1255e+05
v  Local Time Step           0.001        0.016819       0.0010269       0.0010669


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40237      2.3886e+05          32.639          2.6472


 TIME FOR THE TIME STEP              205:        0.16171E+03

===============================================================


 INSTANT    0.206000000E+01   TIME STEP NUMBER             206
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.109558894E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989087425E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96677E+01 0.26853E+01
   Friction velocity        uet   :  0.11114E-01 0.18755E+02
   Friction velocity        uk    :  0.11114E-01 0.18755E+02
   Dimensionless distance   yplus :  0.22129E-02 0.97643E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4016
   Nb of faces within the viscous sub-layer     :      25817
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.46643E+01      35   0.30885E-01   0.41986E+01 0.27972E+02 
c  Velocity[X]                                      0.96027E+00 
c  Velocity[Y]                                      0.18623E+01 
c  Velocity[Z]                                      0.13760E+01 
c  Pressure     0.33680E-01    2203   0.81643E-01   0.16921E+00 0.27884E+03 
c  k            0.57662E-01      24   0.32484E-03   0.15221E-02 0.58144E+02 
c  epsilon      0.43631E+03      14   0.11596E-02   0.88701E+06 0.29670E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.9148e-05                             4
a  epsilon               -0.019883                             1
a  Local Time Step      4.2277e-08                        265306


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.8026          7.8052         0.62812         0.11128
v  Velocity[Y]             -11.029          12.118         0.35044         0.26277
v  Velocity[Z]             -16.355           12.03        -0.23412      -0.0012926
v  ǁVelocityǁ           0.00099568          18.212          1.7759          2.1714
v  Pressure                 -12513           35396           22705           18734
v  k                    3.9543e-09          1.4852       0.0097643        0.010219
v  epsilon              1.3602e-05      1.2292e+05           83.06          7.4578
v  TurbVisc             7.3527e-13         0.16827      0.00052114       0.0070262
v  CourantNb             0.0018995          2085.6           11.04          2.3733
v  FourierNb              0.022221      2.3654e+05          21.807         0.28898
v  total_pressure       4.8749e+05       5.354e+05       5.227e+05      5.1873e+05
v  Local Time Step           0.001        0.018256       0.0010293       0.0010701


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52642      2.3838e+05          32.847          2.6623


 TIME FOR THE TIME STEP              206:        0.19620E+03

===============================================================


 INSTANT    0.207000000E+01   TIME STEP NUMBER             207
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.247477927E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989266863E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10378E+02 0.27673E+01
   Friction velocity        uet   :  0.21515E-01 0.18235E+02
   Friction velocity        uk    :  0.21583E-01 0.18235E+02
   Dimensionless distance   yplus :  0.17105E-02 0.97622E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4053
   Nb of faces within the viscous sub-layer     :      25752
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47225E+01      35   0.31665E-01   0.38902E+01 0.26750E+02 
c  Velocity[X]                                      0.84557E+00 
c  Velocity[Y]                                      0.16806E+01 
c  Velocity[Z]                                      0.13640E+01 
c  Pressure     0.32190E-01    1184   0.71448E-01   0.15763E+00 0.11088E+03 
c  k            0.58757E-01      18   0.29139E-03   0.12353E-02 0.51473E+02 
c  epsilon      0.43929E+03      19   0.93867E-03   0.50039E+06 0.21856E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.9469e-06                             1
a  epsilon               -0.046841                             7
a  Local Time Step      4.2277e-08                        265151


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.8821          8.5806         0.63702         0.11138
v  Velocity[Y]             -11.275           12.53         0.35146         0.26384
v  Velocity[Z]               -17.3          12.582         -0.2328     -0.00067936
v  ǁVelocityǁ           0.00077413          19.499          1.7996          2.1835
v  Pressure                 -10118           38648           25468           21452
v  k                    2.3517e-09          1.1917        0.010079        0.010383
v  epsilon              1.8191e-05           88105           88.44          7.6085
v  TurbVisc             8.3663e-13         0.16853       0.0005297       0.0071233
v  CourantNb             0.0007792          1807.9          11.221          2.3873
v  FourierNb               0.02222      2.3654e+05          21.814         0.28974
v  total_pressure       4.8988e+05      5.3865e+05      5.2547e+05      5.2145e+05
v  Local Time Step           0.001        0.020082       0.0010315       0.0010729


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45646      2.3684e+05          33.035          2.6771


 TIME FOR THE TIME STEP              207:        0.12732E+03

===============================================================


 INSTANT    0.208000000E+01   TIME STEP NUMBER             208
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.475877257E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989529378E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93217E+01 0.27715E+01
   Friction velocity        uet   :  0.19795E-01 0.20145E+02
   Friction velocity        uk    :  0.19742E-01 0.20145E+02
   Dimensionless distance   yplus :  0.25705E-02 0.97789E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4114
   Nb of faces within the viscous sub-layer     :      25675
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47658E+01      34   0.33021E-01   0.35709E+01 0.25490E+02 
c  Velocity[X]                                      0.75584E+00 
c  Velocity[Y]                                      0.15315E+01 
c  Velocity[Z]                                      0.12835E+01 
c  Pressure     0.31715E-01     752   0.59293E-01   0.15132E+00 0.64965E+01 
c  k            0.59761E-01      21   0.51414E-03   0.12489E-02 0.50965E+02 
c  epsilon      0.45448E+03      15   0.10747E-02   0.65255E+06 0.23892E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0051955                             7
a  epsilon                 -33.812                             7
a  Local Time Step      4.2277e-08                        265028


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.9175          8.9151         0.64459         0.11114
v  Velocity[Y]             -11.071          12.683         0.35328         0.26479
v  Velocity[Z]             -18.062          12.909        -0.23357     -0.00050981
v  ǁVelocityǁ           3.4704e-05          20.325          1.8219          2.1939
v  Pressure                 -10368           38678           25445           21405
v  k                    2.8602e-08          1.3974        0.010443         0.01054
v  epsilon              2.8916e-05      1.0479e+05          93.667          7.7675
v  TurbVisc             1.7007e-13         0.16869      0.00053708       0.0072184
v  CourantNb             0.0012963          1772.9          11.427          2.4004
v  FourierNb              0.022221      2.3654e+05           21.82         0.29036
v  total_pressure       4.8963e+05      5.3868e+05      5.2545e+05       5.214e+05
v  Local Time Step           0.001        0.021401       0.0010335       0.0010755


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48888      2.3831e+05          33.247          2.6908


 TIME FOR THE TIME STEP              208:        0.93749E+02

===============================================================


 INSTANT    0.209000000E+01   TIME STEP NUMBER             209
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.227214265E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989284012E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99136E+01 0.27875E+01
   Friction velocity        uet   :  0.40211E-02 0.21071E+02
   Friction velocity        uk    :  0.40210E-02 0.21071E+02
   Dimensionless distance   yplus :  0.26887E-02 0.97877E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4165
   Nb of faces within the viscous sub-layer     :      25587
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47761E+01      36   0.33017E-01   0.33263E+01 0.24494E+02 
c  Velocity[X]                                      0.69641E+00 
c  Velocity[Y]                                      0.14584E+01 
c  Velocity[Z]                                      0.11715E+01 
c  Pressure     0.29843E-01    1355   0.52919E-01   0.13948E+00 0.27105E+02 
c  k            0.60619E-01      15   0.23057E-03   0.10766E-02 0.46621E+02 
c  epsilon      0.46256E+03      12   0.74784E-03   0.49179E+06 0.20255E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1936e-05                             1
a  epsilon                 -1.0968                             5
a  Local Time Step      4.2277e-08                        264995


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.0355           9.144         0.65075          0.1108
v  Velocity[Y]             -11.189          12.218         0.35452         0.26512
v  Velocity[Z]             -18.661          13.336        -0.23637     -0.00058207
v  ǁVelocityǁ           0.00024143          20.952          1.8413          2.2005
v  Pressure                 -11201           38082           24745           20738
v  k                    6.3796e-08          1.3239        0.010652        0.010689
v  epsilon              3.4231e-05           96344          96.696          7.9239
v  TurbVisc             9.1679e-13         0.16876      0.00054439       0.0073101
v  CourantNb            0.00082484          2861.5          11.619          2.4118
v  FourierNb              0.022222      2.3654e+05          21.826         0.29104
v  total_pressure        4.888e+05      5.3808e+05      5.2474e+05      5.2074e+05
v  Local Time Step           0.001        0.023165       0.0010353       0.0010782


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39948       2.394e+05          33.445          2.7029


 TIME FOR THE TIME STEP              209:        0.12562E+03

===============================================================


 INSTANT    0.210000000E+01   TIME STEP NUMBER             210
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.224203456E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989439049E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99220E+01 0.28453E+01
   Friction velocity        uet   :  0.10760E-01 0.23251E+02
   Friction velocity        uk    :  0.10759E-01 0.23251E+02
   Dimensionless distance   yplus :  0.19407E-02 0.97870E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4215
   Nb of faces within the viscous sub-layer     :      25476
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47734E+01      35   0.33596E-01   0.30620E+01 0.23452E+02 
c  Velocity[X]                                      0.67930E+00 
c  Velocity[Y]                                      0.13026E+01 
c  Velocity[Z]                                      0.10801E+01 
c  Pressure     0.29146E-01    1217   0.48985E-01   0.13355E+00 0.15490E+02 
c  k            0.61392E-01      16   0.23505E-03   0.98925E-03 0.44239E+02 
c  epsilon      0.48767E+03      14   0.72697E-03   0.58362E+06 0.21316E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00074872                            14
a  epsilon                 -8.1324                            19
a  Local Time Step      4.2277e-08                        265036


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.1372          9.4829         0.65538         0.11059
v  Velocity[Y]             -11.563          11.969         0.35537         0.26518
v  Velocity[Z]             -18.715          13.459        -0.24112     -0.00080671
v  ǁVelocityǁ            5.207e-05          21.162          1.8588          2.2049
v  Pressure                 -11786           37700           24316           20364
v  k                    6.2458e-08          1.3625        0.010994        0.010821
v  epsilon               3.348e-05      1.0227e+05          102.71          8.0677
v  TurbVisc             9.5159e-13          0.1688      0.00055055       0.0073981
v  CourantNb             0.0025263          3366.8          11.787          2.4223
v  FourierNb              0.022224      2.3654e+05          21.829         0.29172
v  total_pressure       4.8821e+05       5.377e+05      5.2432e+05      5.2036e+05
v  Local Time Step           0.001        0.024784       0.0010369       0.0010812


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.26148       2.399e+05          33.616           2.714


 TIME FOR THE TIME STEP              210:        0.11918E+03

===============================================================


 INSTANT    0.211000000E+01   TIME STEP NUMBER             211
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.165903795E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989521018E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11054E+02 0.28798E+01
   Friction velocity        uet   :  0.75787E-02 0.23826E+02
   Friction velocity        uk    :  0.75784E-02 0.23826E+02
   Dimensionless distance   yplus :  0.30402E-02 0.97839E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4243
   Nb of faces within the viscous sub-layer     :      25394
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47704E+01      35   0.34661E-01   0.28693E+01 0.22659E+02 
c  Velocity[X]                                      0.63208E+00 
c  Velocity[Y]                                      0.12135E+01 
c  Velocity[Z]                                      0.10237E+01 
c  Pressure     0.28218E-01     904   0.46357E-01   0.12712E+00 0.26194E+01 
c  k            0.61972E-01      17   0.26593E-03   0.80886E-03 0.39656E+02 
c  epsilon      0.48128E+03      12   0.61299E-03   0.40809E+06 0.17629E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.4843e-06                             3
a  epsilon                -0.70977                             6
a  Local Time Step      4.2277e-08                        265137


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.2023          9.3506         0.65927         0.11054
v  Velocity[Y]             -11.493          12.402          0.3555         0.26518
v  Velocity[Z]             -18.623          13.502        -0.24663     -0.00099495
v  ǁVelocityǁ           0.00018162          21.042          1.8742          2.2085
v  Pressure                 -12089           37636           24220           20322
v  k                    6.1365e-08          1.3638        0.011155        0.010938
v  epsilon              3.2784e-05      1.0277e+05          104.78          8.1673
v  TurbVisc             5.9104e-13         0.16881      0.00055723       0.0074824
v  CourantNb            0.00019535          4200.5          11.949          2.4318
v  FourierNb              0.022227      2.3654e+05          21.833         0.29237
v  total_pressure       4.8791e+05      5.3764e+05      5.2422e+05      5.2032e+05
v  Local Time Step           0.001        0.026757       0.0010383       0.0010847


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45108      2.4074e+05          33.782          2.7242


 TIME FOR THE TIME STEP              211:        0.10404E+03

===============================================================


 INSTANT    0.212000000E+01   TIME STEP NUMBER             212
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.409491647E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989675431E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98360E+01 0.28734E+01
   Friction velocity        uet   :  0.76388E-02 0.23561E+02
   Friction velocity        uk    :  0.76384E-02 0.23561E+02
   Dimensionless distance   yplus :  0.30064E-02 0.97808E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4276
   Nb of faces within the viscous sub-layer     :      25312
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47714E+01      36   0.35310E-01   0.27892E+01 0.22327E+02 
c  Velocity[X]                                      0.63398E+00 
c  Velocity[Y]                                      0.11540E+01 
c  Velocity[Z]                                      0.10012E+01 
c  Pressure     0.28221E-01     754   0.44622E-01   0.12548E+00 0.24337E+01 
c  k            0.62468E-01      29   0.41732E-03   0.10760E-02 0.45364E+02 
c  epsilon      0.48047E+03      26   0.10110E-02   0.89478E+06 0.25363E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -9.699e-06                             5
a  epsilon                 -1.0378                             7
a  Local Time Step      4.2276e-08                        265403


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.2717           9.447         0.66214         0.11052
v  Velocity[Y]             -11.387          11.217         0.35538         0.26513
v  Velocity[Z]              -18.22          13.435        -0.25254      -0.0010651
v  ǁVelocityǁ           0.00022415          20.706           1.888           2.212
v  Pressure                 -12354           37638           24209           20352
v  k                    5.3993e-08          1.4482        0.011482        0.011047
v  epsilon               3.209e-05      1.0265e+05          110.37          8.2938
v  TurbVisc             8.7249e-13         0.16882       0.0005624        0.007563
v  CourantNb             0.0019406            4534          12.084            2.44
v  FourierNb              0.022229      2.3654e+05          21.834         0.29302
v  total_pressure       4.8765e+05      5.3764e+05      5.2421e+05      5.2035e+05
v  Local Time Step           0.001        0.027125       0.0010393       0.0010888


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52813      2.4107e+05          33.918           2.733


 TIME FOR THE TIME STEP              212:        0.93358E+02

===============================================================


 INSTANT    0.213000000E+01   TIME STEP NUMBER             213
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.111809019E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989503337E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10699E+02 0.28789E+01
   Friction velocity        uet   :  0.10999E-01 0.25333E+02
   Friction velocity        uk    :  0.10998E-01 0.25333E+02
   Dimensionless distance   yplus :  0.32325E-02 0.97810E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4307
   Nb of faces within the viscous sub-layer     :      25235
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47736E+01      38   0.35981E-01   0.27243E+01 0.22046E+02 
c  Velocity[X]                                      0.65350E+00 
c  Velocity[Y]                                      0.10831E+01 
c  Velocity[Z]                                      0.98770E+00 
c  Pressure     0.26920E-01     679   0.42682E-01   0.11856E+00 0.23201E+01 
c  k            0.62901E-01      17   0.18754E-03   0.76189E-03 0.37897E+02 
c  epsilon      0.48588E+03      16   0.77075E-03   0.40664E+06 0.16981E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0778e-05                             5
a  epsilon                 -0.3616                             6
a  Local Time Step      4.2277e-08                        265718


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.3326          8.9611         0.66459         0.11053
v  Velocity[Y]              -11.09          11.935         0.35535         0.26509
v  Velocity[Z]             -17.325          13.409        -0.25897      -0.0010454
v  ǁVelocityǁ           0.00018701          19.666          1.9008          2.2153
v  Pressure                 -12632           37642           24200           20379
v  k                    6.0042e-08          1.5276        0.011606        0.011144
v  epsilon               3.149e-05      1.0247e+05          112.32          8.3663
v  TurbVisc             8.0154e-13         0.16883      0.00056824       0.0076398
v  CourantNb             0.0032831          4347.6            12.2          2.4472
v  FourierNb              0.022232      2.3654e+05          21.835         0.29357
v  total_pressure       4.8737e+05      5.3764e+05       5.242e+05      5.2038e+05
v  Local Time Step           0.001        0.029837       0.0010401       0.0010935


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67078      2.4089e+05          34.035          2.7408


 TIME FOR THE TIME STEP              213:        0.94395E+02

===============================================================


 INSTANT    0.214000000E+01   TIME STEP NUMBER             214
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.345413513E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989444832E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87251E+01 0.28876E+01
   Friction velocity        uet   :  0.86531E-02 0.24685E+02
   Friction velocity        uk    :  0.86520E-02 0.24685E+02
   Dimensionless distance   yplus :  0.31499E-02 0.97803E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4332
   Nb of faces within the viscous sub-layer     :      25170
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47756E+01      29   0.35670E-01   0.25762E+01 0.21399E+02 
c  Velocity[X]                                      0.62201E+00 
c  Velocity[Y]                                      0.10450E+01 
c  Velocity[Z]                                      0.90917E+00 
c  Pressure     0.26286E-01     668   0.40217E-01   0.11477E+00 0.14972E+01 
c  k            0.63247E-01      18   0.16938E-03   0.59110E-03 0.33152E+02 
c  epsilon      0.48533E+03      18   0.52149E-03   0.28508E+06 0.14057E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.7514e-05                             8
a  epsilon                 -1.9468                            10
a  Local Time Step      4.2276e-08                        266023


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.3989          8.8295         0.66615         0.11057
v  Velocity[Y]             -11.408          10.944         0.35542         0.26498
v  Velocity[Z]              -17.22          13.421        -0.26512      -0.0011499
v  ǁVelocityǁ           0.00020949          19.504          1.9126          2.2183
v  Pressure                 -12859           37626           24192           20385
v  k                    5.9786e-08          1.5358         0.01171        0.011233
v  epsilon              3.0937e-05      1.0346e+05          113.66          8.4321
v  TurbVisc             8.3465e-13         0.16883      0.00057259       0.0077125
v  CourantNb             0.0046866          3908.5          12.304          2.4538
v  FourierNb              0.022234      2.3654e+05          21.835         0.29409
v  total_pressure       4.8714e+05      5.3763e+05      5.2419e+05      5.2038e+05
v  Local Time Step           0.001        0.032821       0.0010406       0.0010984


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63122      2.4045e+05          34.138          2.7479


 TIME FOR THE TIME STEP              214:        0.87909E+02

===============================================================


 INSTANT    0.215000000E+01   TIME STEP NUMBER             215
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.970920306E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989547873E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97541E+01 0.28638E+01
   Friction velocity        uet   :  0.15047E-01 0.24589E+02
   Friction velocity        uk    :  0.14887E-01 0.24589E+02
   Dimensionless distance   yplus :  0.31375E-02 0.97811E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4352
   Nb of faces within the viscous sub-layer     :      25082
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47774E+01      33   0.35821E-01   0.25411E+01 0.21226E+02 
c  Velocity[X]                                      0.60736E+00 
c  Velocity[Y]                                      0.98167E+00 
c  Velocity[Z]                                      0.95203E+00 
c  Pressure     0.25744E-01     593   0.37958E-01   0.11140E+00 0.15771E+01 
c  k            0.63573E-01      16   0.21390E-03   0.91358E-03 0.41046E+02 
c  epsilon      0.48838E+03      13   0.53742E-03   0.48234E+06 0.17954E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -8.275e-05                             6
a  epsilon                -0.74216                             4
a  Local Time Step      4.2278e-08                        266441


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5017          8.7106         0.66748         0.11053
v  Velocity[Y]             -11.725          12.152         0.35532         0.26483
v  Velocity[Z]             -16.794          13.428        -0.27115      -0.0012941
v  ǁVelocityǁ            0.0001641          19.052          1.9234          2.2212
v  Pressure                 -13002           37620           24184           20390
v  k                    5.9808e-08          1.5194        0.011914        0.011319
v  epsilon              3.0457e-05      1.0119e+05          116.69          8.5439
v  TurbVisc             8.4828e-13         0.16883      0.00057734       0.0077817
v  CourantNb             0.0028223          3548.5          12.395            2.46
v  FourierNb              0.022237      2.3653e+05          21.834         0.29458
v  total_pressure         4.87e+05      5.3762e+05      5.2418e+05      5.2039e+05
v  Local Time Step           0.001        0.036103       0.0010408       0.0011033


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69713      2.4008e+05          34.229          2.7545


 TIME FOR THE TIME STEP              215:        0.88081E+02

===============================================================


 INSTANT    0.216000000E+01   TIME STEP NUMBER             216
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.900749926E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989586205E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85900E+01 0.28783E+01
   Friction velocity        uet   :  0.13982E-01 0.23691E+02
   Friction velocity        uk    :  0.13981E-01 0.23691E+02
   Dimensionless distance   yplus :  0.30229E-02 0.97821E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4380
   Nb of faces within the viscous sub-layer     :      25022
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47788E+01      31   0.36816E-01   0.24392E+01 0.20778E+02 
c  Velocity[X]                                      0.58359E+00 
c  Velocity[Y]                                      0.94374E+00 
c  Velocity[Z]                                      0.91184E+00 
c  Pressure     0.25088E-01     826   0.36596E-01   0.10776E+00 0.18863E+01 
c  k            0.63826E-01      17   0.30316E-03   0.54710E-03 0.31613E+02 
c  epsilon      0.48713E+03      24   0.44439E-03   0.23374E+06 0.12542E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.9239e-05                             4
a  epsilon                -0.93893                             7
a  Local Time Step      4.2276e-08                        266762


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5322          8.7553         0.66857         0.11055
v  Velocity[Y]             -11.712          10.972         0.35518         0.26463
v  Velocity[Z]             -16.996          13.301        -0.27673      -0.0013275
v  ǁVelocityǁ           0.00037071          19.248          1.9337          2.2237
v  Pressure                 -13165           37590           24141           20366
v  k                    2.5823e-08          1.5111        0.011994        0.011394
v  epsilon              3.0019e-05       1.032e+05          117.56          8.5699
v  TurbVisc              8.213e-13         0.16883      0.00058246       0.0078469
v  CourantNb             0.0051722          3091.4          12.463          2.4658
v  FourierNb               0.02224      2.3654e+05          21.833         0.29497
v  total_pressure       4.8683e+05      5.3759e+05      5.2414e+05      5.2037e+05
v  Local Time Step           0.001        0.039713        0.001041       0.0011078


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6034      2.3907e+05          34.296          2.7608


 TIME FOR THE TIME STEP              216:        0.98571E+02

===============================================================


 INSTANT    0.217000000E+01   TIME STEP NUMBER             217
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.199803722E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989583011E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98333E+01 0.28601E+01
   Friction velocity        uet   :  0.19413E-01 0.23249E+02
   Friction velocity        uk    :  0.19412E-01 0.23249E+02
   Dimensionless distance   yplus :  0.29666E-02 0.97832E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4398
   Nb of faces within the viscous sub-layer     :      24932
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47792E+01      30   0.38028E-01   0.24528E+01 0.20793E+02 
c  Velocity[X]                                      0.58243E+00 
c  Velocity[Y]                                      0.94005E+00 
c  Velocity[Z]                                      0.93037E+00 
c  Pressure     0.24780E-01     467   0.35488E-01   0.10584E+00 0.15438E+01 
c  k            0.64073E-01      16   0.21143E-03   0.76272E-03 0.37173E+02 
c  epsilon      0.49190E+03      12   0.57676E-03   0.32059E+06 0.14408E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.6845e-05                             7
a  epsilon                 -1.8226                             6
a  Local Time Step      4.2277e-08                        267050


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5711           8.647         0.66977         0.11059
v  Velocity[Y]             -10.775           11.92         0.35525          0.2645
v  Velocity[Z]             -16.454          13.227        -0.28144      -0.0012728
v  ǁVelocityǁ           0.00054723          18.695          1.9436           2.226
v  Pressure                 -13277           37594           24140           20366
v  k                    1.2256e-08          1.5184        0.012142        0.011468
v  epsilon              6.8742e-06      1.0389e+05          120.05          8.6669
v  TurbVisc             8.7953e-13         0.16883      0.00058581       0.0079084
v  CourantNb                     0          3023.6          12.538          2.4712
v  FourierNb              0.022242      2.3654e+05          21.832         0.29537
v  total_pressure       4.8672e+05      5.3759e+05      5.2414e+05      5.2037e+05
v  Local Time Step           0.001        0.043685       0.0010409       0.0011116


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46206      2.3862e+05           34.37          2.7665


 TIME FOR THE TIME STEP              217:        0.80652E+02

===============================================================


 INSTANT    0.218000000E+01   TIME STEP NUMBER             218
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.469467097E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989477523E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88830E+01 0.28692E+01
   Friction velocity        uet   :  0.23954E-01 0.20330E+02
   Friction velocity        uk    :  0.23950E-01 0.20330E+02
   Dimensionless distance   yplus :  0.25941E-02 0.97830E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4417
   Nb of faces within the viscous sub-layer     :      24872
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47789E+01      29   0.36884E-01   0.24682E+01 0.20839E+02 
c  Velocity[X]                                      0.60431E+00 
c  Velocity[Y]                                      0.95261E+00 
c  Velocity[Z]                                      0.91132E+00 
c  Pressure     0.24734E-01     464   0.34502E-01   0.10494E+00 0.15097E+01 
c  k            0.64281E-01      14   0.14909E-03   0.52718E-03 0.30726E+02 
c  epsilon      0.49559E+03      15   0.53853E-03   0.18868E+06 0.10988E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012226                            10
a  epsilon                 -12.049                            11
a  Local Time Step      4.2276e-08                        267303


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6113          8.4616         0.67088         0.11065
v  Velocity[Y]             -10.844          10.993          0.3557         0.26444
v  Velocity[Z]             -16.474          13.257         -0.2854      -0.0011662
v  ǁVelocityǁ           0.00041889          18.628          1.9526          2.2283
v  Pressure                 -13340           37602           24140           20373
v  k                    6.9493e-10          1.5068         0.01226        0.011532
v  epsilon              2.9374e-05      1.0323e+05          121.77          8.7115
v  TurbVisc             8.9022e-13         0.16883      0.00059011       0.0079663
v  CourantNb             0.0015019          2515.9          12.601          2.4763
v  FourierNb              0.022245      2.3654e+05           21.83         0.29544
v  total_pressure       4.8666e+05       5.376e+05      5.2414e+05      5.2037e+05
v  Local Time Step           0.001        0.048053       0.0010406       0.0011134


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52362      2.3814e+05          34.431          2.7718


 TIME FOR THE TIME STEP              218:        0.85026E+02

===============================================================


 INSTANT    0.219000000E+01   TIME STEP NUMBER             219
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.658919416E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989413634E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98135E+01 0.28502E+01
   Friction velocity        uet   :  0.19361E-01 0.18779E+02
   Friction velocity        uk    :  0.19357E-01 0.18779E+02
   Dimensionless distance   yplus :  0.23962E-02 0.97854E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4427
   Nb of faces within the viscous sub-layer     :      24813
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47794E+01      33   0.36874E-01   0.23686E+01 0.20403E+02 
c  Velocity[X]                                      0.57321E+00 
c  Velocity[Y]                                      0.91105E+00 
c  Velocity[Z]                                      0.88436E+00 
c  Pressure     0.23999E-01     850   0.33866E-01   0.10182E+00 0.31362E+01 
c  k            0.64486E-01      17   0.16968E-03   0.49396E-03 0.29567E+02 
c  epsilon      0.50749E+03      11   0.47693E-03   0.18529E+06 0.10790E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00027652                            10
a  epsilon                 -5.0481                             9
a  Local Time Step      4.2276e-08                        267585


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -3.618           8.629          0.6719         0.11066
v  Velocity[Y]             -11.874          12.216          0.3562          0.2644
v  Velocity[Z]             -16.263          13.238        -0.28859      -0.0010727
v  ǁVelocityǁ           0.00033137          18.493          1.9611          2.2306
v  Pressure                 -13320           37702           24206           20435
v  k                    1.1486e-09          1.5007        0.012345        0.011592
v  epsilon              1.3533e-06      1.0043e+05          123.28          8.7646
v  TurbVisc             1.2134e-13         0.16883      0.00059335       0.0080207
v  CourantNb             0.0020335          2322.5           12.66          2.4812
v  FourierNb              0.022248      2.3654e+05          21.829         0.29527
v  total_pressure       4.8668e+05       5.377e+05      5.2421e+05      5.2043e+05
v  Local Time Step           0.001        0.052859       0.0010399       0.0011119


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45794      2.3732e+05          34.489          2.7765


 TIME FOR THE TIME STEP              219:        0.96285E+02

===============================================================


 INSTANT    0.220000000E+01   TIME STEP NUMBER             220
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.299728857E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989316056E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10009E+02 0.28493E+01
   Friction velocity        uet   :  0.11783E-01 0.15729E+02
   Friction velocity        uk    :  0.11778E-01 0.15729E+02
   Dimensionless distance   yplus :  0.19830E-02 0.97857E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4433
   Nb of faces within the viscous sub-layer     :      24765
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47797E+01      36   0.36852E-01   0.23696E+01 0.20403E+02 
c  Velocity[X]                                      0.56042E+00 
c  Velocity[Y]                                      0.91951E+00 
c  Velocity[Z]                                      0.88972E+00 
c  Pressure     0.24457E-01     384   0.34111E-01   0.10343E+00 0.13109E+01 
c  k            0.64638E-01      15   0.14847E-03   0.51377E-03 0.30055E+02 
c  epsilon      0.50772E+03      14   0.65708E-03   0.28406E+06 0.13240E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028093                             9
a  epsilon                 -10.954                            11
a  Local Time Step      4.2276e-08                        267868


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5668          8.3348         0.67327         0.11072
v  Velocity[Y]             -12.341          11.119         0.35688         0.26432
v  Velocity[Z]             -16.215          13.262        -0.29122     -0.00085857
v  ǁVelocityǁ           0.00060697          18.327          1.9694          2.2327
v  Pressure                 -13428           37728           24209           20434
v  k                    6.0747e-08          1.4985        0.012462        0.011648
v  epsilon              2.9026e-05      1.0109e+05          125.57          8.8113
v  TurbVisc             9.0964e-13         0.16883      0.00059669       0.0080719
v  CourantNb             0.0029979          1838.6          12.717          2.4859
v  FourierNb               0.02225      2.3654e+05          21.827         0.29504
v  total_pressure       4.8657e+05      5.3773e+05      5.2421e+05      5.2043e+05
v  Local Time Step           0.001        0.053182       0.0010392       0.0011101


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77013      2.3707e+05          34.545           2.781


 TIME FOR THE TIME STEP              220:        0.74074E+02

===============================================================


 INSTANT    0.221000000E+01   TIME STEP NUMBER             221
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.190576708E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989211436E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98284E+01 0.28288E+01
   Friction velocity        uet   :  0.17007E-01 0.14935E+02
   Friction velocity        uk    :  0.16815E-01 0.14935E+02
   Dimensionless distance   yplus :  0.19057E-02 0.97864E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4453
   Nb of faces within the viscous sub-layer     :      24702
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47797E+01      31   0.37322E-01   0.23471E+01 0.20293E+02 
c  Velocity[X]                                      0.55405E+00 
c  Velocity[Y]                                      0.92580E+00 
c  Velocity[Z]                                      0.86724E+00 
c  Pressure     0.24087E-01    1118   0.33734E-01   0.10164E+00 0.62145E+01 
c  k            0.64805E-01      15   0.18283E-03   0.58683E-03 0.32140E+02 
c  epsilon      0.51837E+03      12   0.57455E-03   0.32401E+06 0.14043E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001404                            10
a  epsilon                 -7.5316                            13
a  Local Time Step      4.2276e-08                        268142


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5385          8.5126         0.67473         0.11082
v  Velocity[Y]             -12.351          11.992         0.35759         0.26429
v  Velocity[Z]             -16.266          13.324        -0.29396     -0.00090054
v  ǁVelocityǁ           0.00022256          18.216          1.9771           2.235
v  Pressure                 -13387           37956           24388           20582
v  k                    6.0335e-08          1.4866        0.012557        0.011701
v  epsilon              1.3033e-05           99489          126.51          8.8731
v  TurbVisc             8.7672e-13         0.16883      0.00059999       0.0081199
v  CourantNb             0.0094111          2193.5          12.784          2.4905
v  FourierNb              0.022252      2.3654e+05          21.826         0.29478
v  total_pressure       4.8661e+05      5.3796e+05      5.2439e+05      5.2058e+05
v  Local Time Step           0.001        0.054058       0.0010386       0.0011083


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58723      2.3738e+05           34.61          2.7852


 TIME FOR THE TIME STEP              221:        0.10108E+03

===============================================================


 INSTANT    0.222000000E+01   TIME STEP NUMBER             222
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.308002728E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989505247E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10018E+02 0.28393E+01
   Friction velocity        uet   :  0.91788E-02 0.13186E+02
   Friction velocity        uk    :  0.91780E-02 0.13186E+02
   Dimensionless distance   yplus :  0.16825E-02 0.97896E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4463
   Nb of faces within the viscous sub-layer     :      24631
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47813E+01      29   0.36902E-01   0.23588E+01 0.20310E+02 
c  Velocity[X]                                      0.54962E+00 
c  Velocity[Y]                                      0.95252E+00 
c  Velocity[Z]                                      0.85666E+00 
c  Pressure     0.24260E-01     499   0.33488E-01   0.10193E+00 0.12967E+01 
c  k            0.64913E-01      13   0.19406E-03   0.47132E-03 0.28635E+02 
c  epsilon      0.51372E+03      12   0.43281E-03   0.19305E+06 0.10900E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00013091                            10
a  epsilon                 -7.2202                             8
a  Local Time Step      4.2276e-08                        268299


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5258          8.2779         0.67568         0.11083
v  Velocity[Y]              -12.47          11.158          0.3581         0.26432
v  Velocity[Z]             -16.085          13.267        -0.29609      -0.0010239
v  ǁVelocityǁ           0.00046315          17.997          1.9834          2.2371
v  Pressure                 -13491           37987           24390           20577
v  k                    6.0123e-08          1.4263        0.012569        0.011751
v  epsilon              1.4837e-05      1.0072e+05          126.17           8.902
v  TurbVisc             8.7693e-13         0.16883      0.00060295       0.0081649
v  CourantNb             0.0012135          2323.6          12.845          2.4952
v  FourierNb              0.022254      2.3654e+05          21.826         0.29446
v  total_pressure       4.8651e+05      5.3799e+05      5.2439e+05      5.2058e+05
v  Local Time Step           0.001        0.048178       0.0010378       0.0011047


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62399      2.3706e+05          34.671          2.7897


 TIME FOR THE TIME STEP              222:        0.67155E+02

===============================================================


 INSTANT    0.223000000E+01   TIME STEP NUMBER             223
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.140462521E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989416423E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97341E+01 0.28396E+01
   Friction velocity        uet   :  0.11089E-01 0.11050E+02
   Friction velocity        uk    :  0.11086E-01 0.11050E+02
   Dimensionless distance   yplus :  0.14100E-02 0.97918E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4460
   Nb of faces within the viscous sub-layer     :      24565
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47809E+01      32   0.37048E-01   0.23604E+01 0.20310E+02 
c  Velocity[X]                                      0.56141E+00 
c  Velocity[Y]                                      0.95679E+00 
c  Velocity[Z]                                      0.84217E+00 
c  Pressure     0.24297E-01     474   0.33346E-01   0.10179E+00 0.12614E+01 
c  k            0.65043E-01      14   0.15514E-03   0.52021E-03 0.30141E+02 
c  epsilon      0.52103E+03      13   0.43432E-03   0.18658E+06 0.10622E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0038936                            17
a  epsilon                 -63.962                            12
a  Local Time Step      4.2276e-08                        268396


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5195          8.3973         0.67654         0.11082
v  Velocity[Y]              -12.17          12.077         0.35838          0.2644
v  Velocity[Z]             -16.154          13.259        -0.29763      -0.0010905
v  ǁVelocityǁ           0.00029083           17.92          1.9889          2.2389
v  Pressure                 -13613           38040           24389           20576
v  k                    6.0011e-08          1.4143        0.012663        0.011801
v  epsilon              2.9153e-05      1.0001e+05          127.12          8.9656
v  TurbVisc             8.6757e-13         0.16883      0.00060583       0.0082071
v  CourantNb             0.0054637          2138.4          12.895           2.499
v  FourierNb              0.022256      2.3654e+05          21.824          0.2942
v  total_pressure       4.8639e+05      5.3804e+05      5.2439e+05      5.2058e+05
v  Local Time Step           0.001        0.049046       0.0010372       0.0011022


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51707      2.3781e+05          34.719          2.7932


 TIME FOR THE TIME STEP              223:        0.84410E+02

===============================================================


 INSTANT    0.224000000E+01   TIME STEP NUMBER             224
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.181272390E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989446598E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98447E+01 0.28380E+01
   Friction velocity        uet   :  0.13610E-01 0.11305E+02
   Friction velocity        uk    :  0.13369E-01 0.11305E+02
   Dimensionless distance   yplus :  0.10159E-02 0.97931E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4466
   Nb of faces within the viscous sub-layer     :      24506
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47809E+01      28   0.37752E-01   0.23489E+01 0.20261E+02 
c  Velocity[X]                                      0.55933E+00 
c  Velocity[Y]                                      0.95743E+00 
c  Velocity[Z]                                      0.83214E+00 
c  Pressure     0.23901E-01     453   0.32978E-01   0.99868E-01 0.14027E+01 
c  k            0.65141E-01      13   0.57058E-03   0.60253E-03 0.32335E+02 
c  epsilon      0.52615E+03      11   0.39832E-03   0.16242E+06 0.99335E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00042554                            13
a  epsilon                 -4.5539                             9
a  Local Time Step      4.2276e-08                        268508


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5179          8.2455         0.67741         0.11098
v  Velocity[Y]             -11.098          11.249          0.3582         0.26443
v  Velocity[Z]             -16.083          13.367        -0.29885      -0.0010929
v  ǁVelocityǁ            0.0001323           18.04          1.9942          2.2405
v  Pressure                 -13754           38087           24388           20579
v  k                    6.0059e-08            1.42        0.012702        0.011845
v  epsilon              1.3851e-05      1.0006e+05          127.39          8.9862
v  TurbVisc             8.6477e-13         0.16883      0.00060952       0.0082468
v  CourantNb              0.002875          2062.9          12.936          2.5027
v  FourierNb              0.022258      2.3654e+05          21.824         0.29401
v  total_pressure       4.8625e+05      5.3809e+05      5.2439e+05      5.2058e+05
v  Local Time Step           0.001        0.047428       0.0010368          0.0011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63952      2.3783e+05           34.76          2.7967


 TIME FOR THE TIME STEP              224:        0.74526E+02

===============================================================


 INSTANT    0.225000000E+01   TIME STEP NUMBER             225
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.274604108E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989385137E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97177E+01 0.28278E+01
   Friction velocity        uet   :  0.11414E-01 0.10834E+02
   Friction velocity        uk    :  0.11401E-01 0.10834E+02
   Dimensionless distance   yplus :  0.12424E-02 0.97969E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4462
   Nb of faces within the viscous sub-layer     :      24446
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47805E+01      31   0.37765E-01   0.23393E+01 0.20213E+02 
c  Velocity[X]                                      0.56329E+00 
c  Velocity[Y]                                      0.95449E+00 
c  Velocity[Z]                                      0.82152E+00 
c  Pressure     0.24118E-01     476   0.32847E-01   0.10072E+00 0.14159E+01 
c  k            0.65191E-01      14   0.29531E-03   0.50634E-03 0.29531E+02 
c  epsilon      0.51345E+03      13   0.56028E-03   0.17286E+06 0.10239E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0030412                            17
a  epsilon                  -25.89                             9
a  Local Time Step      4.2276e-08                        268613


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5265          8.3709          0.6782         0.11116
v  Velocity[Y]             -10.879          12.038         0.35762         0.26448
v  Velocity[Z]             -16.188          13.442        -0.30075      -0.0011236
v  ǁVelocityǁ           0.00014233           17.94          1.9993          2.2422
v  Pressure                 -13863           38138           24383           20588
v  k                     6.031e-08          1.4186        0.012753        0.011887
v  epsilon               2.978e-05           99460          128.12          9.0271
v  TurbVisc             8.7575e-13         0.16883      0.00061263       0.0082839
v  CourantNb             0.0013297          2019.6          12.974           2.506
v  FourierNb              0.022259      2.3654e+05          21.823         0.29388
v  total_pressure       4.8614e+05      5.3814e+05      5.2438e+05      5.2059e+05
v  Local Time Step           0.001        0.052171       0.0010365       0.0010983


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70014      2.3753e+05          34.797          2.7999


 TIME FOR THE TIME STEP              225:        0.80947E+02

===============================================================


 INSTANT    0.226000000E+01   TIME STEP NUMBER             226
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.114817854E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989446448E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98809E+01 0.28446E+01
   Friction velocity        uet   :  0.98450E-02 0.10821E+02
   Friction velocity        uk    :  0.98446E-02 0.10821E+02
   Dimensionless distance   yplus :  0.12424E-02 0.97990E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4448
   Nb of faces within the viscous sub-layer     :      24402
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47807E+01      29   0.37182E-01   0.23177E+01 0.20104E+02 
c  Velocity[X]                                      0.55759E+00 
c  Velocity[Y]                                      0.95190E+00 
c  Velocity[Z]                                      0.80823E+00 
c  Pressure     0.23482E-01     487   0.31974E-01   0.97782E-01 0.13446E+01 
c  k            0.65274E-01      12   0.28320E-03   0.50023E-03 0.29278E+02 
c  epsilon      0.52024E+03      12   0.45012E-03   0.16020E+06 0.98422E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00040423                            13
a  epsilon                 -1.1298                             7
a  Local Time Step      4.2276e-08                        268724


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5446          8.2775         0.67882         0.11134
v  Velocity[Y]             -11.834          11.056         0.35669         0.26452
v  Velocity[Z]             -16.119          13.555        -0.30203      -0.0012124
v  ǁVelocityǁ           0.00020705          17.979          2.0039          2.2438
v  Pressure                 -13936           38193           24378           20594
v  k                    6.0736e-08          1.4291        0.012776        0.011927
v  epsilon              3.0325e-05      1.0099e+05          127.94          9.0521
v  TurbVisc               8.69e-13         0.16883      0.00061569       0.0083187
v  CourantNb             0.0024356          1951.3          13.009          2.5094
v  FourierNb              0.022261      2.3654e+05          21.823         0.29384
v  total_pressure       4.8606e+05      5.3819e+05      5.2438e+05      5.2059e+05
v  Local Time Step           0.001        0.057388       0.0010362       0.0010973


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62344      2.3783e+05          34.832          2.8032


 TIME FOR THE TIME STEP              226:        0.85419E+02

===============================================================


 INSTANT    0.227000000E+01   TIME STEP NUMBER             227
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.235976274E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989438214E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97631E+01 0.28380E+01
   Friction velocity        uet   :  0.13573E-01 0.11209E+02
   Friction velocity        uk    :  0.13572E-01 0.11209E+02
   Dimensionless distance   yplus :  0.14303E-02 0.98013E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4441
   Nb of faces within the viscous sub-layer     :      24320
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47808E+01      29   0.36504E-01   0.22838E+01 0.19956E+02 
c  Velocity[X]                                      0.57467E+00 
c  Velocity[Y]                                      0.90305E+00 
c  Velocity[Z]                                      0.80609E+00 
c  Pressure     0.23362E-01     460   0.31599E-01   0.97391E-01 0.13137E+01 
c  k            0.65348E-01      14   0.24878E-03   0.43058E-03 0.26997E+02 
c  epsilon      0.52182E+03      16   0.34265E-03   0.12769E+06 0.87605E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0031934                            17
a  epsilon                   -34.5                            10
a  Local Time Step      4.2276e-08                        268835


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5767          8.3671         0.67964         0.11144
v  Velocity[Y]             -12.318          11.672         0.35582         0.26456
v  Velocity[Z]             -16.208          13.625        -0.30343      -0.0013278
v  ǁVelocityǁ           0.00054887          17.975          2.0083          2.2453
v  Pressure                 -14027           38248           24372           20601
v  k                    6.1457e-08          1.4229        0.012823        0.011965
v  epsilon              3.1007e-05           99845          128.01          9.0966
v  TurbVisc             8.7014e-13         0.16883      0.00061876       0.0083512
v  CourantNb            0.00092348          1976.4          13.039          2.5124
v  FourierNb              0.022262      2.3654e+05          21.823          0.2937
v  total_pressure       4.8597e+05      5.3825e+05      5.2437e+05       5.206e+05
v  Local Time Step           0.001        0.063127       0.0010358       0.0010959


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71097       2.379e+05          34.862          2.8061


 TIME FOR THE TIME STEP              227:        0.84244E+02

===============================================================


 INSTANT    0.228000000E+01   TIME STEP NUMBER             228
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.913992735E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989538091E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99080E+01 0.28412E+01
   Friction velocity        uet   :  0.14246E-01 0.11212E+02
   Friction velocity        uk    :  0.14245E-01 0.11212E+02
   Dimensionless distance   yplus :  0.93345E-03 0.98050E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4443
   Nb of faces within the viscous sub-layer     :      24241
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47817E+01      32   0.37756E-01   0.23036E+01 0.20031E+02 
c  Velocity[X]                                      0.54376E+00 
c  Velocity[Y]                                      0.91781E+00 
c  Velocity[Z]                                      0.84207E+00 
c  Pressure     0.23158E-01     524   0.31450E-01   0.96450E-01 0.13839E+01 
c  k            0.65407E-01      12   0.54640E-03   0.51579E-03 0.29537E+02 
c  epsilon      0.52201E+03      11   0.68542E-03   0.22208E+06 0.11506E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00040406                            13
a  epsilon                 -1.2493                             9
a  Local Time Step      4.2276e-08                        268968


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5942          8.3027         0.68035         0.11153
v  Velocity[Y]               -12.5          10.917         0.35496          0.2645
v  Velocity[Z]             -16.151          13.698        -0.30467      -0.0015075
v  ǁVelocityǁ           0.00012871          18.186          2.0129          2.2469
v  Pressure                 -14083           38301           24363           20606
v  k                    6.2385e-08          1.4313        0.012896        0.012001
v  epsilon               1.728e-05      1.0053e+05          129.45          9.1274
v  TurbVisc             8.6814e-13         0.16883      0.00062184       0.0083816
v  CourantNb             0.0034864            1960          13.062          2.5155
v  FourierNb              0.022262      2.3654e+05          21.822         0.29366
v  total_pressure       4.8592e+05       5.383e+05      5.2436e+05      5.2061e+05
v  Local Time Step           0.001         0.06313       0.0010355       0.0010948


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64338       2.378e+05          34.884          2.8092


 TIME FOR THE TIME STEP              228:        0.94724E+02

===============================================================


 INSTANT    0.229000000E+01   TIME STEP NUMBER             229
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.734914913E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989678188E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98011E+01 0.28234E+01
   Friction velocity        uet   :  0.15620E-01 0.10760E+02
   Friction velocity        uk    :  0.15611E-01 0.10760E+02
   Dimensionless distance   yplus :  0.13730E-02 0.98077E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4443
   Nb of faces within the viscous sub-layer     :      24173
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47828E+01      32   0.38088E-01   0.23327E+01 0.20149E+02 
c  Velocity[X]                                      0.55212E+00 
c  Velocity[Y]                                      0.91753E+00 
c  Velocity[Z]                                      0.86308E+00 
c  Pressure     0.23512E-01     776   0.31560E-01   0.97791E-01 0.13650E+01 
c  k            0.65448E-01      11   0.12259E-03   0.34524E-03 0.24188E+02 
c  epsilon      0.51973E+03      10   0.30981E-03   0.96136E+05 0.75832E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00033185                            13
a  epsilon                -0.68103                             8
a  Local Time Step      4.2276e-08                        269153


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5858          8.4148         0.68152         0.11164
v  Velocity[Y]             -11.842          11.627         0.35443         0.26453
v  Velocity[Z]             -16.319          13.727        -0.30548      -0.0017493
v  ǁVelocityǁ           0.00050116          18.046          2.0175          2.2483
v  Pressure                 -14102           38329           24343           20604
v  k                    4.4676e-08          1.4189        0.012907        0.012035
v  epsilon              1.7338e-05           99055          128.75          9.1409
v  TurbVisc             8.7448e-13         0.16883       0.0006248         0.00841
v  CourantNb             0.0024945          1855.5          13.082          2.5188
v  FourierNb              0.022263      2.3654e+05          21.823          0.2936
v  total_pressure        4.859e+05      5.3833e+05      5.2434e+05       5.206e+05
v  Local Time Step           0.001        0.064146       0.0010353       0.0010948


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44526      2.3759e+05          34.904          2.8124


 TIME FOR THE TIME STEP              229:        0.10072E+03

===============================================================


 INSTANT    0.230000000E+01   TIME STEP NUMBER             230
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.307616056E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.990037951E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10056E+02 0.28508E+01
   Friction velocity        uet   :  0.19855E-01 0.13645E+02
   Friction velocity        uk    :  0.19853E-01 0.13645E+02
   Dimensionless distance   yplus :  0.14237E-02 0.98111E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4433
   Nb of faces within the viscous sub-layer     :      24131
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47838E+01      26   0.38003E-01   0.23020E+01 0.20015E+02 
c  Velocity[X]                                      0.54372E+00 
c  Velocity[Y]                                      0.88657E+00 
c  Velocity[Z]                                      0.87174E+00 
c  Pressure     0.23131E-01     739   0.30881E-01   0.96306E-01 0.70911E+01 
c  k            0.65483E-01      12   0.11382E-03   0.32678E-03 0.23633E+02 
c  epsilon      0.51842E+03      10   0.32013E-03   0.82229E+05 0.70069E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00033068                            11
a  epsilon                 -1.2278                             7
a  Local Time Step      4.2276e-08                        269331


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6001          8.3483         0.68218         0.11166
v  Velocity[Y]             -10.774          10.727         0.35368         0.26447
v  Velocity[Z]             -16.235          13.747        -0.30616      -0.0016769
v  ǁVelocityǁ           0.00082114            18.2          2.0212          2.2492
v  Pressure                 -14314           38146           24125           20431
v  k                    6.4999e-08          1.4401        0.012935        0.012065
v  epsilon              6.2675e-06      1.0179e+05          129.13          9.1619
v  TurbVisc             8.8662e-13         0.16883      0.00062744       0.0084365
v  CourantNb             0.0010722          2019.8          13.107           2.522
v  FourierNb              0.022264      2.3654e+05          21.822         0.29353
v  total_pressure       4.8569e+05      5.3815e+05      5.2412e+05      5.2043e+05
v  Local Time Step           0.001         0.07056       0.0010348       0.0010935


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61033      2.3722e+05          34.929          2.8155


 TIME FOR THE TIME STEP              230:        0.97092E+02

===============================================================


 INSTANT    0.231000000E+01   TIME STEP NUMBER             231
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.348226759E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989854598E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99104E+01 0.28475E+01
   Friction velocity        uet   :  0.15291E-01 0.12573E+02
   Friction velocity        uk    :  0.15289E-01 0.12573E+02
   Dimensionless distance   yplus :  0.15210E-02 0.98153E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4426
   Nb of faces within the viscous sub-layer     :      24090
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47830E+01      30   0.37456E-01   0.22890E+01 0.19953E+02 
c  Velocity[X]                                      0.55014E+00 
c  Velocity[Y]                                      0.89759E+00 
c  Velocity[Z]                                      0.84127E+00 
c  Pressure     0.23221E-01     421   0.31251E-01   0.96762E-01 0.10247E+01 
c  k            0.65525E-01      16   0.23014E-03   0.41737E-03 0.26587E+02 
c  epsilon      0.51985E+03      13   0.49732E-03   0.18433E+06 0.10434E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00033525                            12
a  epsilon                 -0.6231                             7
a  Local Time Step      4.2276e-08                        269452


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6237          8.5674          0.6827         0.11161
v  Velocity[Y]             -11.508           11.45           0.353         0.26436
v  Velocity[Z]             -16.405          13.723        -0.30704      -0.0016807
v  ǁVelocityǁ           0.00042263           18.32          2.0246          2.2502
v  Pressure                 -14291           38205           24117           20434
v  k                    6.7063e-08          1.4353        0.012976        0.012094
v  epsilon              3.4641e-05      1.0094e+05          130.44          9.1931
v  TurbVisc              8.947e-13         0.16883      0.00062961       0.0084613
v  CourantNb             0.0086905          1945.8           13.12          2.5244
v  FourierNb              0.022264      2.3654e+05          21.822         0.29347
v  total_pressure       4.8571e+05      5.3821e+05      5.2412e+05      5.2043e+05
v  Local Time Step           0.001        0.077616       0.0010345       0.0010941


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75945       2.375e+05          34.942          2.8178


 TIME FOR THE TIME STEP              231:        0.75073E+02

===============================================================


 INSTANT    0.232000000E+01   TIME STEP NUMBER             232
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.134036596E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989754195E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10168E+02 0.28484E+01
   Friction velocity        uet   :  0.22965E-01 0.13496E+02
   Friction velocity        uk    :  0.22961E-01 0.13496E+02
   Dimensionless distance   yplus :  0.14907E-02 0.98182E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4423
   Nb of faces within the viscous sub-layer     :      24047
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47837E+01      26   0.37550E-01   0.22575E+01 0.19828E+02 
c  Velocity[X]                                      0.54317E+00 
c  Velocity[Y]                                      0.89309E+00 
c  Velocity[Z]                                      0.82123E+00 
c  Pressure     0.22930E-01     600   0.30963E-01   0.95829E-01 0.11969E+01 
c  k            0.65563E-01      12   0.54391E-03   0.42563E-03 0.26787E+02 
c  epsilon      0.52119E+03      10   0.30431E-03   0.13082E+06 0.88121E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00025673                            10
a  epsilon                 -1.0587                             6
a  Local Time Step      4.2276e-08                        269599


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6093          8.3556         0.68379         0.11163
v  Velocity[Y]             -12.497          10.846         0.35232         0.26432
v  Velocity[Z]             -16.367          13.737        -0.30712      -0.0016316
v  ǁVelocityǁ           0.00033056          18.457          2.0281          2.2511
v  Pressure                 -14259           38215           24081           20422
v  k                    9.7317e-09          1.4342        0.012974        0.012119
v  epsilon              2.8536e-05      1.0084e+05          129.61          9.1957
v  TurbVisc             9.0317e-13         0.16883      0.00063171       0.0084843
v  CourantNb            0.00074233          2202.6          13.139          2.5267
v  FourierNb              0.022265      2.3654e+05          21.822         0.29338
v  total_pressure       4.8574e+05      5.3822e+05      5.2408e+05      5.2042e+05
v  Local Time Step           0.001        0.085378       0.0010342       0.0010936


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85568      2.3671e+05           34.96          2.8201


 TIME FOR THE TIME STEP              232:        0.89181E+02

===============================================================


 INSTANT    0.233000000E+01   TIME STEP NUMBER             233
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.106187247E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989652616E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10084E+02 0.28370E+01
   Friction velocity        uet   :  0.20899E-01 0.10483E+02
   Friction velocity        uk    :  0.20805E-01 0.10483E+02
   Dimensionless distance   yplus :  0.13377E-02 0.98220E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4422
   Nb of faces within the viscous sub-layer     :      24004
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47845E+01      26   0.38000E-01   0.22733E+01 0.19883E+02 
c  Velocity[X]                                      0.54213E+00 
c  Velocity[Y]                                      0.89502E+00 
c  Velocity[Z]                                      0.83613E+00 
c  Pressure     0.23238E-01     416   0.31615E-01   0.97110E-01 0.10479E+01 
c  k            0.65598E-01      14   0.13139E-03   0.39339E-03 0.25717E+02 
c  epsilon      0.52281E+03      20   0.34408E-03   0.10519E+06 0.78618E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002938                            10
a  epsilon                 -2.6481                            12
a  Local Time Step      4.2276e-08                        269720


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6266           8.604         0.68475         0.11165
v  Velocity[Y]             -12.855          10.977         0.35153         0.26427
v  Velocity[Z]             -16.516          13.773        -0.30737      -0.0016475
v  ǁVelocityǁ           0.00076811          18.535          2.0316          2.2521
v  Pressure                 -14167           38248           24076           20428
v  k                    5.0304e-08          1.4336         0.01304        0.012145
v  epsilon              9.3328e-06      1.0063e+05          130.81          9.2306
v  TurbVisc             9.0405e-13         0.16883      0.00063346       0.0085056
v  CourantNb              0.000928          2172.1          13.159           2.529
v  FourierNb              0.022266      2.3654e+05          21.821         0.29337
v  total_pressure       4.8583e+05      5.3825e+05      5.2408e+05      5.2043e+05
v  Local Time Step           0.001        0.093916        0.001034       0.0010938


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61652      2.3693e+05           34.98          2.8224


 TIME FOR THE TIME STEP              233:        0.67333E+02

===============================================================


 INSTANT    0.234000000E+01   TIME STEP NUMBER             234
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.105950218E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989643300E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10324E+02 0.28499E+01
   Friction velocity        uet   :  0.17498E-01 0.10911E+02
   Friction velocity        uk    :  0.17495E-01 0.10911E+02
   Dimensionless distance   yplus :  0.13922E-02 0.98258E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4424
   Nb of faces within the viscous sub-layer     :      23959
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47860E+01      28   0.38715E-01   0.22230E+01 0.19664E+02 
c  Velocity[X]                                      0.54046E+00 
c  Velocity[Y]                                      0.86246E+00 
c  Velocity[Z]                                      0.82006E+00 
c  Pressure     0.22961E-01     630   0.31127E-01   0.95924E-01 0.10493E+01 
c  k            0.65624E-01      13   0.12518E-03   0.31098E-03 0.22881E+02 
c  epsilon      0.52366E+03      10   0.28514E-03   0.77586E+05 0.67590E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.3883e-05                             8
a  epsilon                -0.29071                             6
a  Local Time Step      4.2276e-08                        269814


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6345             8.4         0.68557         0.11172
v  Velocity[Y]             -12.707          10.836          0.3506         0.26422
v  Velocity[Z]             -16.451          13.806        -0.30745      -0.0016004
v  ǁVelocityǁ           0.00069897          18.394          2.0345          2.2528
v  Pressure                 -14111           38258           24053           20417
v  k                    7.6127e-08          1.4404        0.013062        0.012167
v  epsilon              3.9187e-05      1.0146e+05          130.76          9.2394
v  TurbVisc             8.9914e-13         0.16883      0.00063539       0.0085254
v  CourantNb             0.0026948          2271.2          13.182          2.5313
v  FourierNb              0.022267      2.3654e+05           21.82         0.29341
v  total_pressure       4.8589e+05      5.3826e+05      5.2405e+05      5.2042e+05
v  Local Time Step           0.001         0.10331       0.0010338       0.0010942


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62702      2.3704e+05          35.002          2.8247


 TIME FOR THE TIME STEP              234:        0.89250E+02

===============================================================


 INSTANT    0.235000000E+01   TIME STEP NUMBER             235
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.257024045E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989606262E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10205E+02 0.28328E+01
   Friction velocity        uet   :  0.48668E-02 0.85420E+01
   Friction velocity        uk    :  0.49118E-02 0.85420E+01
   Dimensionless distance   yplus :  0.10584E-02 0.98324E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4414
   Nb of faces within the viscous sub-layer     :      23914
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47869E+01      31   0.38086E-01   0.22399E+01 0.19729E+02 
c  Velocity[X]                                      0.55460E+00 
c  Velocity[Y]                                      0.87003E+00 
c  Velocity[Z]                                      0.81526E+00 
c  Pressure     0.23555E-01     853   0.31860E-01   0.98530E-01 0.14161E+01 
c  k            0.65661E-01      12   0.25418E-03   0.38503E-03 0.25527E+02 
c  epsilon      0.52524E+03      11   0.25389E-03   0.96273E+05 0.75121E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.3837e-05                             7
a  epsilon                -0.31857                             7
a  Local Time Step      4.2276e-08                        269909


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -3.636          8.5466         0.68637         0.11176
v  Velocity[Y]             -11.855          11.027         0.34988         0.26419
v  Velocity[Z]             -16.537          13.891        -0.30736      -0.0015167
v  ǁVelocityǁ           0.00072352          18.529           2.037          2.2536
v  Pressure                 -13976           38243           24018           20395
v  k                    8.0486e-08           1.422        0.013084        0.012191
v  epsilon              4.1121e-05           99547          130.74          9.2715
v  TurbVisc              9.172e-13         0.16883      0.00063731       0.0085438
v  CourantNb             0.0019999          2115.2          13.196          2.5331
v  FourierNb              0.022268      2.3654e+05          21.819         0.29336
v  total_pressure       4.8602e+05      5.3824e+05      5.2402e+05      5.2039e+05
v  Local Time Step           0.001         0.11364       0.0010335       0.0010939


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67901      2.3717e+05          35.015          2.8265


 TIME FOR THE TIME STEP              235:        0.10092E+03

===============================================================


 INSTANT    0.236000000E+01   TIME STEP NUMBER             236
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.126018699E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989566504E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10354E+02 0.28554E+01
   Friction velocity        uet   :  0.23250E-01 0.92043E+01
   Friction velocity        uk    :  0.23245E-01 0.92043E+01
   Dimensionless distance   yplus :  0.98353E-03 0.98387E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4418
   Nb of faces within the viscous sub-layer     :      23881
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47875E+01      26   0.36927E-01   0.22052E+01 0.19564E+02 
c  Velocity[X]                                      0.54118E+00 
c  Velocity[Y]                                      0.85552E+00 
c  Velocity[Z]                                      0.80846E+00 
c  Pressure     0.23696E-01     319   0.32537E-01   0.99180E-01 0.93008E+00 
c  k            0.65681E-01      12   0.56367E-03   0.36679E-03 0.24896E+02 
c  epsilon      0.52630E+03      11   0.26411E-03   0.97289E+05 0.75589E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.2775e-05                             7
a  epsilon                -0.28677                            10
a  Local Time Step      4.2276e-08                        269961


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6311          8.4483         0.68712         0.11183
v  Velocity[Y]             -12.281          11.164         0.34946         0.26414
v  Velocity[Z]             -16.581          13.824        -0.30773       -0.001498
v  ǁVelocityǁ            0.0012367          18.443          2.0396          2.2543
v  Pressure                 -13869           38247           24018           20395
v  k                    8.5614e-08          1.4433        0.013123         0.01221
v  epsilon              4.2957e-05      1.0201e+05          131.32          9.2728
v  TurbVisc             9.2449e-13         0.16883      0.00063909       0.0085609
v  CourantNb             0.0079396          2105.3          13.213           2.535
v  FourierNb              0.022269      2.3654e+05          21.819         0.29332
v  total_pressure       4.8613e+05      5.3825e+05      5.2402e+05       5.204e+05
v  Local Time Step           0.001        0.087932       0.0010332       0.0010925


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56107      2.3748e+05          35.032          2.8283


 TIME FOR THE TIME STEP              236:        0.71390E+02

===============================================================


 INSTANT    0.237000000E+01   TIME STEP NUMBER             237
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.614943971E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989506092E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10401E+02 0.28491E+01
   Friction velocity        uet   :  0.10707E-01 0.97577E+01
   Friction velocity        uk    :  0.10614E-01 0.97577E+01
   Dimensionless distance   yplus :  0.83641E-03 0.98457E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4408
   Nb of faces within the viscous sub-layer     :      23848
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47892E+01      27   0.37707E-01   0.20998E+01 0.19075E+02 
c  Velocity[X]                                      0.49758E+00 
c  Velocity[Y]                                      0.81791E+00 
c  Velocity[Z]                                      0.78436E+00 
c  Pressure     0.23288E-01     394   0.31695E-01   0.97486E-01 0.98018E+00 
c  k            0.65707E-01      13   0.10874E-03   0.28409E-03 0.21892E+02 
c  epsilon      0.52706E+03      10   0.36091E-03   0.11364E+06 0.81334E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.7749e-05                             7
a  epsilon                -0.38283                            11
a  Local Time Step      4.2276e-08                        270052


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6346          8.6635          0.6876         0.11182
v  Velocity[Y]             -12.516          10.931         0.34913         0.26413
v  Velocity[Z]             -16.607          13.669        -0.30783      -0.0014886
v  ǁVelocityǁ            0.0012139          18.786          2.0416          2.2551
v  Pressure                 -13745           38248           24015           20400
v  k                    3.5101e-09          1.4267        0.013154        0.012229
v  epsilon              4.4766e-05       1.007e+05          131.72          9.2947
v  TurbVisc             9.1553e-13         0.16883      0.00064088       0.0085767
v  CourantNb             0.0056069          1972.8          13.222          2.5369
v  FourierNb              0.022271      2.3654e+05          21.818         0.29326
v  total_pressure       4.8626e+05      5.3825e+05      5.2402e+05       5.204e+05
v  Local Time Step           0.001         0.04847       0.0010328       0.0010912


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59799      2.3756e+05           35.04          2.8301


 TIME FOR THE TIME STEP              237:        0.71892E+02

===============================================================


 INSTANT    0.238000000E+01   TIME STEP NUMBER             238
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.177894176E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989475291E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10456E+02 0.28534E+01
   Friction velocity        uet   :  0.17106E-01 0.92820E+01
   Friction velocity        uk    :  0.17086E-01 0.92820E+01
   Dimensionless distance   yplus :  0.11224E-02 0.98583E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4409
   Nb of faces within the viscous sub-layer     :      23835
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47901E+01      29   0.39301E-01   0.20802E+01 0.18987E+02 
c  Velocity[X]                                      0.51597E+00 
c  Velocity[Y]                                      0.79537E+00 
c  Velocity[Z]                                      0.76884E+00 
c  Pressure     0.23451E-01     364   0.31993E-01   0.98251E-01 0.98294E+00 
c  k            0.65719E-01      12   0.10093E-03   0.26654E-03 0.20789E+02 
c  epsilon      0.52611E+03      10   0.32882E-03   0.65326E+05 0.61682E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.2322e-05                             7
a  epsilon                -0.28256                             8
a  Local Time Step      4.2276e-08                        270171


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6081          8.5404         0.68814         0.11183
v  Velocity[Y]             -11.998          11.015         0.34916         0.26416
v  Velocity[Z]             -16.677          13.743        -0.30783      -0.0014717
v  ǁVelocityǁ            0.0011006          18.499          2.0439          2.2559
v  Pressure                 -13639           38246           24014           20406
v  k                    2.7694e-09          1.4453        0.013183        0.012246
v  epsilon              1.8374e-06      1.0207e+05          132.04          9.3009
v  TurbVisc              2.867e-14         0.16883      0.00064275       0.0085914
v  CourantNb             0.0023612          1961.5          13.228          2.5387
v  FourierNb              0.022273      2.3654e+05          21.818         0.29323
v  total_pressure       4.8636e+05      5.3825e+05      5.2401e+05      5.2041e+05
v  Local Time Step           0.001        0.052083       0.0010326       0.0010907


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4487      2.3738e+05          35.046           2.832


 TIME FOR THE TIME STEP              238:        0.76964E+02

===============================================================


 INSTANT    0.239000000E+01   TIME STEP NUMBER             239
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.262834877E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989523862E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10536E+02 0.28590E+01
   Friction velocity        uet   :  0.12323E-01 0.98345E+01
   Friction velocity        uk    :  0.12273E-01 0.98345E+01
   Dimensionless distance   yplus :  0.10534E-02 0.98782E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4416
   Nb of faces within the viscous sub-layer     :      23791
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47908E+01      29   0.38559E-01   0.20851E+01 0.18995E+02 
c  Velocity[X]                                      0.51025E+00 
c  Velocity[Y]                                      0.82679E+00 
c  Velocity[Z]                                      0.74810E+00 
c  Pressure     0.23544E-01     544   0.31958E-01   0.98561E-01 0.11135E+01 
c  k            0.65747E-01      11   0.10472E-03   0.33445E-03 0.23709E+02 
c  epsilon      0.52867E+03       9   0.22692E-03   0.71714E+05 0.64485E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.7418e-05                             7
a  epsilon                 -0.2674                             9
a  Local Time Step      4.2276e-08                        270267


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6024          8.6006         0.68844         0.11176
v  Velocity[Y]              -11.33          10.832         0.34944         0.26425
v  Velocity[Z]             -16.668          13.845        -0.30774      -0.0014049
v  ǁVelocityǁ            0.0011387          18.818          2.0459          2.2567
v  Pressure                 -13547           38241           24012           20412
v  k                    3.0724e-09          1.4274        0.013241        0.012265
v  epsilon              4.9227e-05      1.0125e+05          132.68          9.3287
v  TurbVisc             9.1757e-13         0.16883      0.00064445       0.0086051
v  CourantNb              0.009081            2070          13.245          2.5405
v  FourierNb              0.022276      2.3654e+05          21.817         0.29325
v  total_pressure       4.8645e+05      5.3824e+05      5.2401e+05      5.2041e+05
v  Local Time Step           0.001        0.057291       0.0010323       0.0010906


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71588      2.3782e+05          35.062          2.8338


 TIME FOR THE TIME STEP              239:        0.72435E+02

===============================================================


 INSTANT    0.240000000E+01   TIME STEP NUMBER             240
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.356369630E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989431982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10544E+02 0.28521E+01
   Friction velocity        uet   :  0.83748E-02 0.12012E+02
   Friction velocity        uk    :  0.83675E-02 0.12012E+02
   Dimensionless distance   yplus :  0.10178E-02 0.98892E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4435
   Nb of faces within the viscous sub-layer     :      23785
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47915E+01      26   0.37097E-01   0.20345E+01 0.18781E+02 
c  Velocity[X]                                      0.48913E+00 
c  Velocity[Y]                                      0.80472E+00 
c  Velocity[Z]                                      0.74066E+00 
c  Pressure     0.22858E-01     310   0.31046E-01   0.95633E-01 0.85520E+00 
c  k            0.65765E-01      11   0.90940E-04   0.24741E-03 0.20350E+02 
c  epsilon      0.52953E+03      11   0.17469E-03   0.42725E+05 0.49732E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.8174e-05                             8
a  epsilon                -0.36775                             7
a  Local Time Step      4.2276e-08                        270365


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5792          8.5542          0.6883          0.1117
v  Velocity[Y]              -11.68          10.897         0.35019         0.26423
v  Velocity[Z]             -16.703          13.864        -0.30797      -0.0014237
v  ǁVelocityǁ            0.0013108          18.559          2.0477          2.2574
v  Pressure                 -13408           38222           24012           20414
v  k                    2.9319e-09          1.4412        0.013247        0.012279
v  epsilon              3.3237e-05      1.0167e+05          132.68          9.3323
v  TurbVisc             9.1447e-13         0.16883      0.00064617       0.0086177
v  CourantNb              0.015308          1964.5          13.253          2.5425
v  FourierNb              0.022279      2.3654e+05          21.816         0.29319
v  total_pressure       4.8659e+05      5.3822e+05      5.2401e+05      5.2041e+05
v  Local Time Step           0.001         0.06302       0.0010322       0.0010905


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.8232      2.3775e+05          35.069          2.8356


 TIME FOR THE TIME STEP              240:        0.64079E+02

===============================================================


 INSTANT    0.241000000E+01   TIME STEP NUMBER             241
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.299920772E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441287E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10613E+02 0.28545E+01
   Friction velocity        uet   :  0.10244E-01 0.13764E+02
   Friction velocity        uk    :  0.10159E-01 0.13764E+02
   Dimensionless distance   yplus :  0.13975E-02 0.98912E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4433
   Nb of faces within the viscous sub-layer     :      23758
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47921E+01      26   0.37437E-01   0.19506E+01 0.18384E+02 
c  Velocity[X]                                      0.47839E+00 
c  Velocity[Y]                                      0.74245E+00 
c  Velocity[Z]                                      0.72974E+00 
c  Pressure     0.22861E-01     426   0.30771E-01   0.95697E-01 0.94392E+00 
c  k            0.65787E-01      13   0.97378E-04   0.29241E-03 0.22223E+02 
c  epsilon      0.53148E+03       9   0.29982E-03   0.10229E+06 0.76809E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.8028e-05                             8
a  epsilon                 -1.0544                             8
a  Local Time Step      4.2276e-08                        270390


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5816          8.5576         0.68811         0.11163
v  Velocity[Y]             -11.346          10.927         0.35144         0.26424
v  Velocity[Z]             -16.692          13.881        -0.30796      -0.0014691
v  ǁVelocityǁ            0.0014839           18.88          2.0498          2.2582
v  Pressure                 -13250           38210           24010           20421
v  k                    1.0162e-09          1.4352        0.013296        0.012294
v  epsilon              5.4994e-05       1.015e+05          133.41          9.3523
v  TurbVisc             9.2249e-13         0.16883       0.0006473       0.0086294
v  CourantNb              0.011415            2206          13.264          2.5441
v  FourierNb              0.022282      2.3654e+05          21.816          0.2932
v  total_pressure       4.8675e+05      5.3821e+05      5.2401e+05      5.2042e+05
v  Local Time Step           0.001        0.069322       0.0010321       0.0010909


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83205      2.3773e+05           35.08          2.8373


 TIME FOR THE TIME STEP              241:        0.77823E+02

===============================================================


 INSTANT    0.242000000E+01   TIME STEP NUMBER             242
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.817215294E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989446348E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.95272E+01 0.28534E+01
   Friction velocity        uet   :  0.10218E-01 0.13653E+02
   Friction velocity        uk    :  0.10215E-01 0.13653E+02
   Dimensionless distance   yplus :  0.15313E-02 0.98892E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4437
   Nb of faces within the viscous sub-layer     :      23753
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47925E+01      27   0.38140E-01   0.19297E+01 0.18279E+02 
c  Velocity[X]                                      0.48692E+00 
c  Velocity[Y]                                      0.73064E+00 
c  Velocity[Z]                                      0.71213E+00 
c  Pressure     0.22469E-01     395   0.30152E-01   0.94114E-01 0.93198E+00 
c  k            0.65812E-01      14   0.99781E-04   0.30213E-03 0.22450E+02 
c  epsilon      0.53595E+03      13   0.30712E-03   0.68952E+05 0.63020E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.7099e-06                             6
a  epsilon                -0.76237                             8
a  Local Time Step      4.2276e-08                        270482


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5706          8.5206         0.68773         0.11156
v  Velocity[Y]              -11.91          10.819         0.35269         0.26419
v  Velocity[Z]             -16.458          13.955         -0.3079      -0.0014777
v  ǁVelocityǁ            0.0019176          18.586          2.0519          2.2591
v  Pressure                 -13193           38195           24008           20430
v  k                    1.3153e-09           1.437        0.013322        0.012306
v  epsilon              1.2167e-05      1.0146e+05          133.57          9.3643
v  TurbVisc             4.7422e-13         0.16883      0.00064902       0.0086402
v  CourantNb             0.0024208          2345.4          13.273           2.546
v  FourierNb              0.022286      2.3654e+05          21.816         0.29328
v  total_pressure       4.8681e+05      5.3819e+05      5.2401e+05      5.2043e+05
v  Local Time Step           0.001        0.076255       0.0010322       0.0010901


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.8241      2.3737e+05          35.089          2.8393


 TIME FOR THE TIME STEP              242:        0.77025E+02

===============================================================


 INSTANT    0.243000000E+01   TIME STEP NUMBER             243
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.186474505E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989500392E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10355E+02 0.28636E+01
   Friction velocity        uet   :  0.18298E-01 0.13527E+02
   Friction velocity        uk    :  0.18271E-01 0.13527E+02
   Dimensionless distance   yplus :  0.13041E-02 0.98949E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4442
   Nb of faces within the viscous sub-layer     :      23743
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47930E+01      28   0.37797E-01   0.19299E+01 0.18266E+02 
c  Velocity[X]                                      0.48617E+00 
c  Velocity[Y]                                      0.72372E+00 
c  Velocity[Z]                                      0.71997E+00 
c  Pressure     0.22985E-01     436   0.30468E-01   0.96238E-01 0.90575E+00 
c  k            0.65842E-01      15   0.10079E-03   0.31805E-03 0.23175E+02 
c  epsilon      0.54073E+03      11   0.27227E-03   0.84628E+05 0.69761E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.7259e-05                             7
a  epsilon                -0.69504                             9
a  Local Time Step      4.2276e-08                        270518


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5554          8.5712         0.68722          0.1115
v  Velocity[Y]             -12.148          10.737         0.35424         0.26423
v  Velocity[Z]              -16.74          13.972        -0.30776      -0.0014419
v  ǁVelocityǁ            0.0018251          18.929           2.054            2.26
v  Pressure                 -13695           38177           24005           20436
v  k                    1.4925e-08           1.444        0.013335        0.012319
v  epsilon              3.6496e-05      1.0195e+05          133.57          9.3783
v  TurbVisc             9.1867e-13         0.16883      0.00065012         0.00865
v  CourantNb              0.002921          2333.5          13.287          2.5479
v  FourierNb               0.02229      2.3654e+05          21.816         0.29328
v  total_pressure        4.863e+05      5.3818e+05      5.2401e+05      5.2044e+05
v  Local Time Step           0.001        0.063669       0.0010321       0.0010898


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67979      2.3803e+05          35.103          2.8412


 TIME FOR THE TIME STEP              243:        0.77788E+02

===============================================================


 INSTANT    0.244000000E+01   TIME STEP NUMBER             244
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.175316408E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989532681E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96424E+01 0.28563E+01
   Friction velocity        uet   :  0.22657E-01 0.11012E+02
   Friction velocity        uk    :  0.22555E-01 0.11012E+02
   Dimensionless distance   yplus :  0.84256E-03 0.99037E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4425
   Nb of faces within the viscous sub-layer     :      23721
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47928E+01      28   0.37237E-01   0.19005E+01 0.18126E+02 
c  Velocity[X]                                      0.47696E+00 
c  Velocity[Y]                                      0.69868E+00 
c  Velocity[Z]                                      0.72491E+00 
c  Pressure     0.22093E-01     448   0.29276E-01   0.92616E-01 0.79672E+00 
c  k            0.65866E-01      14   0.10003E-03   0.27154E-03 0.21402E+02 
c  epsilon      0.54535E+03      15   0.29616E-03   0.10983E+06 0.79336E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.5947e-05                             8
a  epsilon                 -1.0388                            10
a  Local Time Step      4.2276e-08                        270557


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5508          8.5432         0.68718         0.11145
v  Velocity[Y]             -12.299          10.773         0.35557         0.26429
v  Velocity[Z]             -16.485          14.001        -0.30808      -0.0014804
v  ǁVelocityǁ            0.0019236          18.645          2.0564          2.2608
v  Pressure                 -14094           38162           24005           20432
v  k                    3.1802e-08          1.4392        0.013366         0.01233
v  epsilon              4.7944e-06      1.0132e+05          134.33          9.3869
v  TurbVisc             9.3244e-13         0.16883      0.00065105       0.0086591
v  CourantNb             0.0070607          2178.7          13.295          2.5496
v  FourierNb              0.022295      2.3654e+05          21.816         0.29324
v  total_pressure       4.8591e+05      5.3816e+05      5.2401e+05      5.2043e+05
v  Local Time Step           0.001        0.061716        0.001032       0.0010886


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.80984      2.3792e+05          35.111          2.8429


 TIME FOR THE TIME STEP              244:        0.75887E+02

===============================================================


 INSTANT    0.245000000E+01   TIME STEP NUMBER             245
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.236119351E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989480545E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10405E+02 0.28582E+01
   Friction velocity        uet   :  0.18964E-01 0.12457E+02
   Friction velocity        uk    :  0.18740E-01 0.12457E+02
   Dimensionless distance   yplus :  0.15895E-02 0.99097E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4434
   Nb of faces within the viscous sub-layer     :      23711
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47922E+01      28   0.37679E-01   0.18736E+01 0.17993E+02 
c  Velocity[X]                                      0.47763E+00 
c  Velocity[Y]                                      0.68911E+00 
c  Velocity[Z]                                      0.70685E+00 
c  Pressure     0.21874E-01     394   0.28724E-01   0.91619E-01 0.76754E+00 
c  k            0.65883E-01      14   0.11608E-03   0.25698E-03 0.20810E+02 
c  epsilon      0.54503E+03      10   0.28310E-03   0.77825E+05 0.66727E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.0339e-05                             8
a  epsilon                 -1.4188                            15
a  Local Time Step      4.2276e-08                        270566


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5697          8.5036         0.68682         0.11143
v  Velocity[Y]             -11.691          10.692          0.3566         0.26426
v  Velocity[Z]             -17.075          13.905        -0.30833      -0.0014748
v  ǁVelocityǁ            0.0023043          19.068          2.0587          2.2617
v  Pressure                 -14444           38159           24002           20438
v  k                    6.4727e-08          1.4439        0.013361        0.012341
v  epsilon               3.078e-06      1.0204e+05          133.98          9.4037
v  TurbVisc             9.3253e-13         0.16883      0.00065186       0.0086675
v  CourantNb             0.0082182          2227.3          13.315          2.5514
v  FourierNb              0.022299      2.3654e+05          21.816         0.29325
v  total_pressure       4.8556e+05      5.3816e+05        5.24e+05      5.2044e+05
v  Local Time Step           0.001        0.061117       0.0010319       0.0010881


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.80566      2.3793e+05           35.13          2.8447


 TIME FOR THE TIME STEP              245:        0.68717E+02

===============================================================


 INSTANT    0.246000000E+01   TIME STEP NUMBER             246
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.272460799E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989573250E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93442E+01 0.28608E+01
   Friction velocity        uet   :  0.20817E-01 0.10395E+02
   Friction velocity        uk    :  0.20565E-01 0.10395E+02
   Dimensionless distance   yplus :  0.13264E-02 0.99165E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4439
   Nb of faces within the viscous sub-layer     :      23683
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47919E+01      28   0.37115E-01   0.18390E+01 0.17812E+02 
c  Velocity[X]                                      0.47246E+00 
c  Velocity[Y]                                      0.66204E+00 
c  Velocity[Z]                                      0.70448E+00 
c  Pressure     0.21609E-01     259   0.28328E-01   0.90486E-01 0.73544E+00 
c  k            0.65850E-01      12   0.19900E-03   0.22873E-03 0.19551E+02 
c  epsilon      0.53031E+03      10   0.30388E-03   0.70257E+05 0.63625E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.7783e-05                             7
a  epsilon                 -1.2117                            12
a  Local Time Step      4.2276e-08                        270635


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5626          8.5656          0.6866         0.11144
v  Velocity[Y]             -11.236          10.614         0.35756         0.26429
v  Velocity[Z]              -16.61          13.985        -0.30862      -0.0014858
v  ǁVelocityǁ            0.0023477          18.727          2.0609          2.2627
v  Pressure                 -14775           38164           24002           20438
v  k                    1.2429e-07          1.4443        0.013397        0.012351
v  epsilon              4.2981e-05      1.0177e+05          134.46          9.4069
v  TurbVisc             9.3208e-13         0.16883      0.00065309       0.0086752
v  CourantNb             0.0047812          2279.9          13.324          2.5533
v  FourierNb              0.022304      2.3654e+05          21.816         0.29322
v  total_pressure       4.8522e+05      5.3816e+05        5.24e+05      5.2044e+05
v  Local Time Step           0.001        0.067228       0.0010318       0.0010879


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82867      2.3678e+05          35.139          2.8466


 TIME FOR THE TIME STEP              246:        0.72596E+02

===============================================================


 INSTANT    0.247000000E+01   TIME STEP NUMBER             247
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.114765836E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989461000E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10384E+02 0.28502E+01
   Friction velocity        uet   :  0.17582E-01 0.11125E+02
   Friction velocity        uk    :  0.17377E-01 0.11125E+02
   Dimensionless distance   yplus :  0.86858E-03 0.99202E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4441
   Nb of faces within the viscous sub-layer     :      23675
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47910E+01      25   0.37908E-01   0.17846E+01 0.17547E+02 
c  Velocity[X]                                      0.46010E+00 
c  Velocity[Y]                                      0.65300E+00 
c  Velocity[Z]                                      0.67151E+00 
c  Pressure     0.21388E-01     370   0.27874E-01   0.89481E-01 0.73254E+00 
c  k            0.65896E-01      11   0.21066E-03   0.22728E-03 0.19574E+02 
c  epsilon      0.54258E+03       8   0.19160E-03   0.58700E+05 0.57940E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010618                             9
a  epsilon                -0.92964                            13
a  Local Time Step      4.2276e-08                        270702


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5543            8.49         0.68647         0.11139
v  Velocity[Y]             -10.839          10.513         0.35831         0.26439
v  Velocity[Z]              -17.22          14.019        -0.30843      -0.0014011
v  ǁVelocityǁ             0.001675          19.243          2.0633          2.2636
v  Pressure                 -15004           38167           24002           20441
v  k                    2.2593e-07          1.4351        0.013392        0.012361
v  epsilon              2.1004e-05      1.0079e+05          134.14          9.4216
v  TurbVisc             9.3657e-13         0.16883      0.00065441       0.0086823
v  CourantNb              0.007846          2400.7          13.345          2.5551
v  FourierNb              0.022309      2.3654e+05          21.815         0.29318
v  total_pressure         4.85e+05      5.3817e+05        5.24e+05      5.2044e+05
v  Local Time Step           0.001        0.069901       0.0010317        0.001088


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71959      2.3827e+05           35.16          2.8483


 TIME FOR THE TIME STEP              247:        0.73870E+02

===============================================================


 INSTANT    0.248000000E+01   TIME STEP NUMBER             248
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.217005129E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989446580E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.90703E+01 0.28601E+01
   Friction velocity        uet   :  0.14991E-01 0.70717E+01
   Friction velocity        uk    :  0.14906E-01 0.70717E+01
   Dimensionless distance   yplus :  0.90236E-03 0.99243E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4442
   Nb of faces within the viscous sub-layer     :      23644
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47903E+01      26   0.37552E-01   0.17633E+01 0.17428E+02 
c  Velocity[X]                                      0.48134E+00 
c  Velocity[Y]                                      0.63465E+00 
c  Velocity[Z]                                      0.64732E+00 
c  Pressure     0.21043E-01     298   0.27539E-01   0.87872E-01 0.74666E+00 
c  k            0.65886E-01      14   0.21889E-03   0.27741E-03 0.21628E+02 
c  epsilon      0.53351E+03      11   0.29814E-03   0.73826E+05 0.65095E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.4049e-05                             7
a  epsilon                -0.66852                            11
a  Local Time Step      4.2276e-08                        270758


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -3.547          8.5878          0.6866         0.11138
v  Velocity[Y]             -11.504           10.47         0.35846         0.26444
v  Velocity[Z]             -16.703          14.092        -0.30866       -0.001278
v  ǁVelocityǁ            0.0023864          18.748          2.0657          2.2646
v  Pressure                 -15145           38157           24003           20442
v  k                    2.4243e-07          1.4402        0.013434        0.012373
v  epsilon              5.8526e-05      1.0182e+05          134.63          9.4403
v  TurbVisc             9.2245e-13         0.16883       0.0006559       0.0086889
v  CourantNb             0.0021434          2232.2          13.357           2.557
v  FourierNb              0.022313      2.3654e+05          21.815         0.29318
v  total_pressure       4.8485e+05      5.3816e+05        5.24e+05      5.2044e+05
v  Local Time Step           0.001        0.076891       0.0010316       0.0010884


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74933      2.3803e+05          35.172          2.8502


 TIME FOR THE TIME STEP              248:        0.65090E+02

===============================================================


 INSTANT    0.249000000E+01   TIME STEP NUMBER             249
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.588576258E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989344725E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10322E+02 0.28631E+01
   Friction velocity        uet   :  0.22578E-01 0.97457E+01
   Friction velocity        uk    :  0.22429E-01 0.97457E+01
   Dimensionless distance   yplus :  0.11781E-02 0.99268E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4433
   Nb of faces within the viscous sub-layer     :      23613
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47889E+01      27   0.37576E-01   0.17787E+01 0.17508E+02 
c  Velocity[X]                                      0.49150E+00 
c  Velocity[Y]                                      0.65497E+00 
c  Velocity[Z]                                      0.63222E+00 
c  Pressure     0.21197E-01     290   0.27631E-01   0.88587E-01 0.77046E+00 
c  k            0.65939E-01      11   0.27287E-03   0.26634E-03 0.21134E+02 
c  epsilon      0.54718E+03      10   0.26853E-03   0.87544E+05 0.70671E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.8712e-05                             7
a  epsilon                 -1.3411                            10
a  Local Time Step      4.2276e-08                        270847


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5471          8.4717         0.68662         0.11135
v  Velocity[Y]             -11.845          10.573         0.35864         0.26441
v  Velocity[Z]             -17.524          14.164         -0.3088      -0.0011087
v  ǁVelocityǁ            0.0021782          19.594          2.0682          2.2654
v  Pressure                 -15219           38166           24004           20445
v  k                    2.5458e-07          1.4422        0.013423        0.012384
v  epsilon              3.4027e-05      1.0179e+05          133.98          9.4535
v  TurbVisc             9.8114e-13         0.16883      0.00065744       0.0086949
v  CourantNb             0.0069759          2187.4           13.37          2.5589
v  FourierNb              0.022318      2.3654e+05          21.816         0.29318
v  total_pressure       4.8478e+05      5.3817e+05        5.24e+05      5.2044e+05
v  Local Time Step           0.001        0.076213       0.0010315       0.0010877


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69772      2.3767e+05          35.186          2.8521


 TIME FOR THE TIME STEP              249:        0.73643E+02

===============================================================


 INSTANT    0.250000000E+01   TIME STEP NUMBER             250
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.787881768E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989216675E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85774E+01 0.28579E+01
   Friction velocity        uet   :  0.20669E-01 0.83018E+01
   Friction velocity        uk    :  0.20597E-01 0.83018E+01
   Dimensionless distance   yplus :  0.87974E-03 0.99278E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4449
   Nb of faces within the viscous sub-layer     :      23619
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47888E+01      41   0.37639E-01   0.18337E+01 0.17771E+02 
c  Velocity[X]                                      0.48331E+00 
c  Velocity[Y]                                      0.65015E+00 
c  Velocity[Z]                                      0.70027E+00 
c  Pressure     0.21798E-01     429   0.28357E-01   0.91038E-01 0.82976E+00 
c  k            0.69796E-01      18   0.15240E-01   0.53342E-03 0.29899E+02 
c  epsilon      0.53261E+03      16   0.15058E+00   0.26030E+06 0.12162E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.7361e-05                            10
a  epsilon                -0.27017                            10
a  Local Time Step      4.2276e-08                        270909


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5537          8.5942         0.68711         0.11138
v  Velocity[Y]             -11.822          10.523         0.35841         0.26435
v  Velocity[Z]             -16.528          14.174        -0.30895     -0.00099856
v  ǁVelocityǁ            0.0016057          18.773          2.0706          2.2663
v  Pressure                 -15239           38173           24009           20448
v  k                    2.7049e-07           1.444        0.013442        0.012394
v  epsilon              7.9451e-05      1.0178e+05           134.4           9.502
v  TurbVisc             9.2647e-13          47.377      0.00082678       0.0088384
v  CourantNb             0.0064897          2184.1          13.387          2.5607
v  FourierNb              0.022322      2.3654e+05          21.818         0.29504
v  total_pressure       4.8476e+05      5.3817e+05      5.2401e+05      5.2045e+05
v  Local Time Step           0.001        0.069503       0.0010313       0.0010883


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78084       2.384e+05          35.205          2.8557


 TIME FOR THE TIME STEP              250:        0.78479E+02

===============================================================


 INSTANT    0.251000000E+01   TIME STEP NUMBER             251
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.140188291E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989026314E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10259E+02 0.28558E+01
   Friction velocity        uet   :  0.22832E-01 0.10187E+02
   Friction velocity        uk    :  0.22552E-01 0.10187E+02
   Dimensionless distance   yplus :  0.12999E-02 0.99275E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4447
   Nb of faces within the viscous sub-layer     :      23586
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47864E+01      23   0.37310E-01   0.18306E+01 0.17744E+02 
c  Velocity[X]                                      0.48294E+00 
c  Velocity[Y]                                      0.68088E+00 
c  Velocity[Z]                                      0.66683E+00 
c  Pressure     0.21388E-01     266   0.27792E-01   0.89252E-01 0.74179E+00 
c  k            0.65946E-01      12   0.28030E-03   0.49552E-03 0.28514E+02 
c  epsilon      0.54485E+03      15   0.58650E-03   0.27030E+06 0.12234E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.8604e-05                             8
a  epsilon                -0.15468                             8
a  Local Time Step      4.2276e-08                        271008


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5529          8.4017         0.68747         0.11144
v  Velocity[Y]             -11.237          10.478         0.35797         0.26429
v  Velocity[Z]             -17.458          14.222        -0.30926     -0.00082145
v  ǁVelocityǁ            0.0021175          19.522          2.0728          2.2671
v  Pressure                 -15186           38189           24011           20451
v  k                    1.3034e-07          1.4301        0.013455          0.0124
v  epsilon              2.9161e-05      1.0096e+05          134.51          9.4666
v  TurbVisc             9.5536e-13         0.16883       0.0006599       0.0087055
v  CourantNb             0.0079617          2655.2          13.407          2.5624
v  FourierNb              0.022326      2.3654e+05          21.816          0.2931
v  total_pressure       4.8481e+05      5.3819e+05      5.2401e+05      5.2045e+05
v  Local Time Step           0.001        0.073847       0.0010312       0.0010878


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83772       2.392e+05          35.223          2.8555


 TIME FOR THE TIME STEP              251:        0.62741E+02

===============================================================


 INSTANT    0.252000000E+01   TIME STEP NUMBER             252
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.753944291E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.988905881E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84315E+01 0.28581E+01
   Friction velocity        uet   :  0.24173E-01 0.88842E+01
   Friction velocity        uk    :  0.23873E-01 0.88842E+01
   Dimensionless distance   yplus :  0.89292E-03 0.99272E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4442
   Nb of faces within the viscous sub-layer     :      23574
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47856E+01      27   0.37982E-01   0.18644E+01 0.17914E+02 
c  Velocity[X]                                      0.49649E+00 
c  Velocity[Y]                                      0.69690E+00 
c  Velocity[Z]                                      0.67098E+00 
c  Pressure     0.21404E-01     570   0.27836E-01   0.89252E-01 0.84242E+00 
c  k            0.65908E-01      11   0.29481E-03   0.27039E-03 0.21281E+02 
c  epsilon      0.53059E+03       9   0.38707E-03   0.12248E+06 0.83982E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.1207e-05                             9
a  epsilon                  -1.416                            10
a  Local Time Step      4.2276e-08                        271072


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5557          8.5334         0.68778         0.11139
v  Velocity[Y]             -12.175          10.335         0.35733         0.26427
v  Velocity[Z]             -16.513          14.241        -0.30947      -0.0006696
v  ǁVelocityǁ            0.0016757          18.726          2.0747          2.2679
v  Pressure                 -15098           38208           24019           20455
v  k                    2.6082e-08          1.4432        0.013461        0.012407
v  epsilon              7.0722e-05      1.0173e+05           134.3          9.4655
v  TurbVisc             9.2424e-13         0.16883      0.00066119       0.0087101
v  CourantNb             0.0019965          2196.1          13.416          2.5641
v  FourierNb              0.022329      2.3654e+05          21.815         0.29317
v  total_pressure        4.849e+05      5.3821e+05      5.2402e+05      5.2046e+05
v  Local Time Step           0.001        0.081231       0.0010312       0.0010888


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70595      2.3874e+05          35.231          2.8572


 TIME FOR THE TIME STEP              252:        0.83922E+02

===============================================================


 INSTANT    0.253000000E+01   TIME STEP NUMBER             253
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.556761303E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.988672841E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10190E+02 0.28446E+01
   Friction velocity        uet   :  0.15477E-01 0.81397E+01
   Friction velocity        uk    :  0.15283E-01 0.81397E+01
   Dimensionless distance   yplus :  0.90981E-03 0.99254E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4441
   Nb of faces within the viscous sub-layer     :      23564
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47841E+01      28   0.38265E-01   0.18741E+01 0.17962E+02 
c  Velocity[X]                                      0.51148E+00 
c  Velocity[Y]                                      0.70404E+00 
c  Velocity[Z]                                      0.65861E+00 
c  Pressure     0.21867E-01     804   0.28385E-01   0.91277E-01 0.68625E+01 
c  k            0.65953E-01      13   0.26693E-03   0.22020E-03 0.19158E+02 
c  epsilon      0.54408E+03      10   0.26480E-03   0.72446E+05 0.64343E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.0843e-05                             8
a  epsilon                -0.32173                            11
a  Local Time Step      4.2276e-08                        271169


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5536          8.5246         0.68825         0.11145
v  Velocity[Y]             -12.367          10.385         0.35661         0.26433
v  Velocity[Z]             -17.425          14.145        -0.30962     -0.00089154
v  ǁVelocityǁ           0.00059523          19.445          2.0767           2.269
v  Pressure                 -14737           38434           24228           20629
v  k                    2.5181e-09          1.4337        0.013466        0.012415
v  epsilon              1.0507e-05      1.0091e+05          134.09          9.4742
v  TurbVisc             9.6601e-13         0.16883      0.00066264       0.0087144
v  CourantNb             0.0053137          2071.4          13.421          2.5655
v  FourierNb              0.022332      2.3654e+05          21.816         0.29319
v  total_pressure       4.8526e+05      5.3843e+05      5.2423e+05      5.2063e+05
v  Local Time Step           0.001        0.060275       0.0010311       0.0010885


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55037      2.3861e+05          35.236          2.8587


 TIME FOR THE TIME STEP              253:        0.90660E+02

===============================================================


 INSTANT    0.254000000E+01   TIME STEP NUMBER             254
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.605816866E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.988968918E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93117E+01 0.28584E+01
   Friction velocity        uet   :  0.24399E-01 0.85968E+01
   Friction velocity        uk    :  0.24337E-01 0.85968E+01
   Dimensionless distance   yplus :  0.13699E-03 0.99268E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4435
   Nb of faces within the viscous sub-layer     :      23529
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47853E+01      24   0.37895E-01   0.18514E+01 0.17844E+02 
c  Velocity[X]                                      0.48971E+00 
c  Velocity[Y]                                      0.67439E+00 
c  Velocity[Z]                                      0.68730E+00 
c  Pressure     0.21643E-01     286   0.28105E-01   0.90190E-01 0.76056E+00 
c  k            0.65919E-01      12   0.26987E-03   0.23485E-03 0.19824E+02 
c  epsilon      0.53155E+03      13   0.47873E-03   0.90595E+05 0.72126E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012747                            12
a  epsilon                 -2.4172                            21
a  Local Time Step      4.2276e-08                        271220


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5588          8.7161         0.68922         0.11151
v  Velocity[Y]             -12.151          10.445         0.35565         0.26434
v  Velocity[Z]             -16.786          14.197         -0.3098      -0.0011001
v  ǁVelocityǁ            0.0015345          19.065          2.0791          2.2703
v  Pressure                 -14480           38441           24228           20632
v  k                    1.0045e-08          1.4407          0.0135        0.012422
v  epsilon              1.4403e-05      1.0198e+05          134.93          9.4784
v  TurbVisc             9.1148e-13         0.16883      0.00066358       0.0087183
v  CourantNb             0.0014469          2027.2          13.432          2.5672
v  FourierNb              0.022333      2.3654e+05          21.816         0.29323
v  total_pressure       4.8552e+05      5.3844e+05      5.2423e+05      5.2063e+05
v  Local Time Step           0.001        0.064502       0.0010312       0.0010894


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62396       2.385e+05          35.248          2.8604


 TIME FOR THE TIME STEP              254:        0.71066E+02

===============================================================


 INSTANT    0.255000000E+01   TIME STEP NUMBER             255
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.170695841E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989279563E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10601E+02 0.28453E+01
   Friction velocity        uet   :  0.14331E-01 0.12370E+02
   Friction velocity        uk    :  0.14267E-01 0.12370E+02
   Dimensionless distance   yplus :  0.15785E-02 0.99274E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4442
   Nb of faces within the viscous sub-layer     :      23503
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47857E+01      24   0.37931E-01   0.18603E+01 0.17873E+02 
c  Velocity[X]                                      0.49463E+00 
c  Velocity[Y]                                      0.69014E+00 
c  Velocity[Z]                                      0.67558E+00 
c  Pressure     0.21954E-01     259   0.28472E-01   0.91628E-01 0.71573E+00 
c  k            0.65955E-01      11   0.24327E-03   0.21659E-03 0.19015E+02 
c  epsilon      0.54354E+03      11   0.29675E-03   0.88546E+05 0.71151E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010168                             6
a  epsilon                -0.36812                            19
a  Local Time Step      4.2276e-08                        271292


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5674          8.4125         0.68988         0.11164
v  Velocity[Y]             -12.392          10.402         0.35472         0.26434
v  Velocity[Z]             -17.328          14.213         -0.3101      -0.0012659
v  ǁVelocityǁ            0.0019191           19.36          2.0809          2.2715
v  Pressure                 -14163           38452           24225           20633
v  k                      1.34e-08          1.4227        0.013488        0.012431
v  epsilon                2.57e-05           99761          134.16          9.4855
v  TurbVisc             1.1239e-12         0.16883      0.00066406        0.008722
v  CourantNb             0.0013314          2095.6           13.45          2.5691
v  FourierNb              0.022334      2.3654e+05          21.816         0.29328
v  total_pressure       4.8584e+05      5.3845e+05      5.2422e+05      5.2063e+05
v  Local Time Step           0.001        0.060731       0.0010312       0.0010895


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82133      2.3821e+05          35.266          2.8624


 TIME FOR THE TIME STEP              255:        0.68924E+02

===============================================================


 INSTANT    0.256000000E+01   TIME STEP NUMBER             256
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.120846226E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989485798E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88943E+01 0.28525E+01
   Friction velocity        uet   :  0.20946E-01 0.83167E+01
   Friction velocity        uk    :  0.20887E-01 0.83167E+01
   Dimensionless distance   yplus :  0.47824E-03 0.99281E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4441
   Nb of faces within the viscous sub-layer     :      23458
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47860E+01      31   0.38163E-01   0.19236E+01 0.18181E+02 
c  Velocity[X]                                      0.49584E+00 
c  Velocity[Y]                                      0.72442E+00 
c  Velocity[Z]                                      0.70332E+00 
c  Pressure     0.22555E-01     284   0.29050E-01   0.93956E-01 0.73633E+00 
c  k            0.65914E-01      11   0.27098E-03   0.25269E-03 0.20570E+02 
c  epsilon      0.52824E+03       9   0.37050E-03   0.82058E+05 0.68754E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012512                            10
a  epsilon                 -1.6542                            14
a  Local Time Step      4.2276e-08                        271362


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5604          8.6938         0.69048         0.11173
v  Velocity[Y]              -12.67          10.475         0.35378         0.26437
v  Velocity[Z]             -16.813          14.256         -0.3108      -0.0014484
v  ǁVelocityǁ            0.0014821          19.083          2.0826          2.2725
v  Pressure                 -13833           38471           24221           20633
v  k                    1.9517e-08          1.4401        0.013516         0.01244
v  epsilon              6.1287e-06      1.0167e+05          134.56          9.4924
v  TurbVisc             8.6878e-13         0.16883      0.00066483       0.0087255
v  CourantNb             0.0038162          2102.9          13.457          2.5707
v  FourierNb              0.022334      2.3654e+05          21.816         0.29322
v  total_pressure       4.8617e+05      5.3847e+05      5.2422e+05      5.2063e+05
v  Local Time Step           0.001        0.066503       0.0010311       0.0010897


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91213      2.3864e+05          35.273           2.864


 TIME FOR THE TIME STEP              256:        0.65802E+02

===============================================================


 INSTANT    0.257000000E+01   TIME STEP NUMBER             257
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.327215942E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989660405E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10566E+02 0.28550E+01
   Friction velocity        uet   :  0.13005E-01 0.10218E+02
   Friction velocity        uk    :  0.12984E-01 0.10218E+02
   Dimensionless distance   yplus :  0.13038E-02 0.99293E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4441
   Nb of faces within the viscous sub-layer     :      23452
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47861E+01      25   0.37687E-01   0.18706E+01 0.17909E+02 
c  Velocity[X]                                      0.50351E+00 
c  Velocity[Y]                                      0.69046E+00 
c  Velocity[Z]                                      0.67666E+00 
c  Pressure     0.21730E-01     326   0.28429E-01   0.90552E-01 0.65985E+00 
c  k            0.65954E-01      11   0.26491E-03   0.19597E-03 0.18034E+02 
c  epsilon      0.54260E+03      11   0.28488E-03   0.55297E+05 0.56170E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001155                             6
a  epsilon                -0.68267                            13
a  Local Time Step      4.2276e-08                        271398


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5706          8.4543           0.691         0.11175
v  Velocity[Y]             -12.258          10.477         0.35275         0.26439
v  Velocity[Z]             -17.474          14.237        -0.31119      -0.0016275
v  ǁVelocityǁ            0.0018227          19.532          2.0844          2.2736
v  Pressure                 -13422           38469           24215           20635
v  k                    1.4044e-08          1.4339        0.013503        0.012447
v  epsilon              1.5275e-05      1.0119e+05          134.28          9.4966
v  TurbVisc             1.1368e-12         0.16883      0.00066565       0.0087288
v  CourantNb              0.014791          1733.8          13.466          2.5722
v  FourierNb              0.022334      2.3654e+05          21.816         0.29331
v  total_pressure       4.8658e+05      5.3847e+05      5.2422e+05      5.2063e+05
v  Local Time Step           0.001        0.067577        0.001031       0.0010901


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68622      2.3828e+05          35.282          2.8655


 TIME FOR THE TIME STEP              257:        0.69654E+02

===============================================================


 INSTANT    0.258000000E+01   TIME STEP NUMBER             258
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.229056076E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989905534E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87813E+01 0.28539E+01
   Friction velocity        uet   :  0.20148E-01 0.99018E+01
   Friction velocity        uk    :  0.20101E-01 0.99018E+01
   Dimensionless distance   yplus :  0.65125E-03 0.99300E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4438
   Nb of faces within the viscous sub-layer     :      23427
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47873E+01      24   0.37751E-01   0.18532E+01 0.17838E+02 
c  Velocity[X]                                      0.47649E+00 
c  Velocity[Y]                                      0.70146E+00 
c  Velocity[Z]                                      0.67522E+00 
c  Pressure     0.21774E-01     676   0.28330E-01   0.90598E-01 0.38132E+01 
c  k            0.65905E-01      14   0.26803E-03   0.22637E-03 0.19433E+02 
c  epsilon      0.52611E+03      11   0.33729E-03   0.14331E+06 0.90637E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012303                             5
a  epsilon                 -1.3556                            16
a  Local Time Step      4.2276e-08                        271381


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5651          8.7648         0.69123         0.11167
v  Velocity[Y]             -12.074          10.654         0.35167         0.26425
v  Velocity[Z]             -16.942          14.272        -0.31174      -0.0015358
v  ǁVelocityǁ            0.0015748          19.245           2.086          2.2745
v  Pressure                 -13440           38349           24092           20539
v  k                    4.1853e-08          1.4348        0.013542        0.012454
v  epsilon              3.5508e-05      1.0103e+05          135.09          9.4966
v  TurbVisc              8.665e-13         0.16883      0.00066628        0.008732
v  CourantNb              0.015176          1646.1          13.472          2.5738
v  FourierNb              0.022332      2.3654e+05          21.816         0.29351
v  total_pressure       4.8656e+05      5.3835e+05      5.2409e+05      5.2054e+05
v  Local Time Step           0.001        0.065254       0.0010313       0.0010914


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82753      2.3792e+05          35.288          2.8673


 TIME FOR THE TIME STEP              258:        0.85490E+02

===============================================================


 INSTANT    0.259000000E+01   TIME STEP NUMBER             259
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.789997934E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989827723E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10644E+02 0.28463E+01
   Friction velocity        uet   :  0.81770E-02 0.10649E+02
   Friction velocity        uk    :  0.81636E-02 0.10649E+02
   Dimensionless distance   yplus :  0.12352E-02 0.99290E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4435
   Nb of faces within the viscous sub-layer     :      23428
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47865E+01      26   0.37869E-01   0.18388E+01 0.17756E+02 
c  Velocity[X]                                      0.48915E+00 
c  Velocity[Y]                                      0.67342E+00 
c  Velocity[Z]                                      0.67627E+00 
c  Pressure     0.22145E-01     380   0.28766E-01   0.91947E-01 0.75876E+00 
c  k            0.65950E-01      13   0.26920E-03   0.26096E-03 0.20792E+02 
c  epsilon      0.54113E+03      13   0.46258E-03   0.12099E+06 0.82983E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011839                             7
a  epsilon                 -1.3418                            14
a  Local Time Step      4.2276e-08                        271366


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5884          8.4569         0.69156         0.11153
v  Velocity[Y]             -11.825          10.675          0.3509          0.2641
v  Velocity[Z]             -17.595          14.289        -0.31216      -0.0014731
v  ǁVelocityǁ            0.0010688          19.681          2.0877          2.2751
v  Pressure                 -13481           38364           24087           20534
v  k                    2.4932e-07          1.4267        0.013526        0.012461
v  epsilon              2.7739e-05      1.0037e+05          135.01          9.5101
v  TurbVisc             9.7502e-13         0.16883      0.00066704       0.0087348
v  CourantNb              0.013967          2167.8          13.487          2.5752
v  FourierNb               0.02233      2.3654e+05          21.817         0.29352
v  total_pressure       4.8652e+05      5.3836e+05      5.2409e+05      5.2053e+05
v  Local Time Step           0.001        0.066693       0.0010314       0.0010919


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76105      2.3808e+05          35.304          2.8687


 TIME FOR THE TIME STEP              259:        0.68108E+02

===============================================================


 INSTANT    0.260000000E+01   TIME STEP NUMBER             260
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.108045413E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989690778E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88378E+01 0.28686E+01
   Friction velocity        uet   :  0.13069E-01 0.83598E+01
   Friction velocity        uk    :  0.12935E-01 0.83598E+01
   Dimensionless distance   yplus :  0.75752E-03 0.99295E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4447
   Nb of faces within the viscous sub-layer     :      23417
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47866E+01      24   0.38397E-01   0.18159E+01 0.17648E+02 
c  Velocity[X]                                      0.50227E+00 
c  Velocity[Y]                                      0.64976E+00 
c  Velocity[Z]                                      0.66389E+00 
c  Pressure     0.21519E-01     413   0.27846E-01   0.89157E-01 0.73134E+00 
c  k            0.65911E-01      11   0.26858E-03   0.24377E-03 0.20073E+02 
c  epsilon      0.52578E+03       9   0.36168E-03   0.12469E+06 0.84552E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012202                             5
a  epsilon                -0.91029                            14
a  Local Time Step      4.2276e-08                        271364


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5909          8.7393         0.69194          0.1115
v  Velocity[Y]             -11.207          10.548         0.35025         0.26402
v  Velocity[Z]             -16.982          14.303        -0.31245      -0.0014125
v  ǁVelocityǁ           0.00067967           19.27          2.0893          2.2757
v  Pressure                 -13494           38372           24084           20535
v  k                    2.6926e-07          1.4519        0.013535        0.012467
v  epsilon              3.6313e-05      1.0293e+05          134.73          9.5098
v  TurbVisc             9.0379e-13         0.16883      0.00066727       0.0087375
v  CourantNb            0.00076315            2349           13.51          2.5764
v  FourierNb              0.022328      2.3654e+05          21.816         0.29371
v  total_pressure       4.8651e+05      5.3837e+05      5.2408e+05      5.2054e+05
v  Local Time Step           0.001        0.073362       0.0010315       0.0010934


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69846      2.3874e+05          35.326          2.8701


 TIME FOR THE TIME STEP              260:        0.66410E+02

===============================================================


 INSTANT    0.261000000E+01   TIME STEP NUMBER             261
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.404785787E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989576235E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10611E+02 0.28553E+01
   Friction velocity        uet   :  0.21368E-01 0.81804E+01
   Friction velocity        uk    :  0.21108E-01 0.81804E+01
   Dimensionless distance   yplus :  0.87750E-03 0.99289E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4452
   Nb of faces within the viscous sub-layer     :      23411
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47858E+01      25   0.37678E-01   0.18342E+01 0.17719E+02 
c  Velocity[X]                                      0.48817E+00 
c  Velocity[Y]                                      0.70762E+00 
c  Velocity[Z]                                      0.63844E+00 
c  Pressure     0.21423E-01     293   0.27769E-01   0.88676E-01 0.70117E+00 
c  k            0.65952E-01      13   0.27757E-03   0.23042E-03 0.19506E+02 
c  epsilon      0.54093E+03      12   0.26174E-03   0.95957E+05 0.73954E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012958                             6
a  epsilon                -0.90134                            13
a  Local Time Step      4.2276e-08                        271403


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5955           8.417         0.69224         0.11149
v  Velocity[Y]             -11.759          10.617         0.34973         0.26404
v  Velocity[Z]             -17.476          14.198        -0.31256      -0.0013526
v  ǁVelocityǁ           0.00029714          19.553          2.0906          2.2762
v  Pressure                 -13508           38367           24082           20536
v  k                      2.62e-07          1.4295         0.01353        0.012472
v  epsilon              5.8712e-06      1.0048e+05          134.55          9.5153
v  TurbVisc             9.9387e-13         0.16883      0.00066782         0.00874
v  CourantNb                0.0101          2370.7          13.513          2.5776
v  FourierNb              0.022325      2.3654e+05          21.816         0.29379
v  total_pressure       4.8649e+05      5.3837e+05      5.2408e+05      5.2054e+05
v  Local Time Step           0.001        0.074315       0.0010317        0.001094


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63841      2.3806e+05          35.329          2.8714


 TIME FOR THE TIME STEP              261:        0.73461E+02

===============================================================


 INSTANT    0.262000000E+01   TIME STEP NUMBER             262
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.453934612E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989418165E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88188E+01 0.28475E+01
   Friction velocity        uet   :  0.65908E-02 0.82253E+01
   Friction velocity        uk    :  0.66741E-02 0.82253E+01
   Dimensionless distance   yplus :  0.73631E-03 0.99300E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4447
   Nb of faces within the viscous sub-layer     :      23400
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47859E+01      29   0.37222E-01   0.17671E+01 0.17392E+02 
c  Velocity[X]                                      0.50205E+00 
c  Velocity[Y]                                      0.62189E+00 
c  Velocity[Z]                                      0.64319E+00 
c  Pressure     0.21434E-01     403   0.27632E-01   0.88601E-01 0.78066E+00 
c  k            0.65911E-01      12   0.29341E-03   0.26647E-03 0.21060E+02 
c  epsilon      0.52504E+03      14   0.50439E-03   0.10872E+06 0.78920E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012663                             5
a  epsilon                -0.46951                            13
a  Local Time Step      4.2276e-08                        271418


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5955          8.7079         0.69212         0.11149
v  Velocity[Y]             -12.506          10.648         0.34951           0.264
v  Velocity[Z]             -16.987          14.224        -0.31296      -0.0013146
v  ǁVelocityǁ           0.00016908           19.26          2.0916          2.2767
v  Pressure                 -13531           38373           24083           20540
v  k                     2.679e-07          1.4387         0.01355        0.012478
v  epsilon              1.6442e-05      1.0148e+05          135.23          9.5212
v  TurbVisc             9.4121e-13         0.16883      0.00066814       0.0087422
v  CourantNb                     0          2091.3          13.516          2.5787
v  FourierNb              0.022322      2.3654e+05          21.817         0.29388
v  total_pressure       4.8647e+05      5.3837e+05      5.2408e+05      5.2054e+05
v  Local Time Step           0.001        0.068078       0.0010319       0.0010946


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53585      2.3776e+05          35.333          2.8726


 TIME FOR THE TIME STEP              262:        0.77792E+02

===============================================================


 INSTANT    0.263000000E+01   TIME STEP NUMBER             263
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.927688540E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989306288E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10556E+02 0.28645E+01
   Friction velocity        uet   :  0.17498E-01 0.85439E+01
   Friction velocity        uk    :  0.17497E-01 0.85439E+01
   Dimensionless distance   yplus :  0.92634E-03 0.99297E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4440
   Nb of faces within the viscous sub-layer     :      23399
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47855E+01      23   0.37456E-01   0.17445E+01 0.17276E+02 
c  Velocity[X]                                      0.48435E+00 
c  Velocity[Y]                                      0.62508E+00 
c  Velocity[Z]                                      0.63504E+00 
c  Pressure     0.21215E-01     603   0.27478E-01   0.87518E-01 0.99346E+00 
c  k            0.65968E-01      13   0.26695E-03   0.24300E-03 0.20172E+02 
c  epsilon      0.54286E+03       8   0.30350E-03   0.10512E+06 0.77228E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012604                             7
a  epsilon                -0.86172                            14
a  Local Time Step      4.2276e-08                        271477


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -3.611          8.4462         0.69192         0.11159
v  Velocity[Y]             -12.491          10.714         0.34982         0.26406
v  Velocity[Z]              -17.51          14.291        -0.31297      -0.0012073
v  ǁVelocityǁ            0.0002688          19.537          2.0928          2.2771
v  Pressure                 -13483           38383           24092           20557
v  k                    2.5317e-07          1.4376        0.013549        0.012482
v  epsilon               5.613e-06      1.0203e+05          134.82          9.5297
v  TurbVisc             9.5916e-13         0.16883      0.00066835       0.0087443
v  CourantNb             0.0027511          2034.9          13.516          2.5794
v  FourierNb               0.02232      2.3654e+05          21.817         0.29398
v  total_pressure       4.8652e+05      5.3838e+05      5.2409e+05      5.2056e+05
v  Local Time Step           0.001        0.071023       0.0010321       0.0010953


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.27413      2.3817e+05          35.333          2.8734


 TIME FOR THE TIME STEP              263:        0.85285E+02

===============================================================


 INSTANT    0.264000000E+01   TIME STEP NUMBER             264
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.101032222E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989266950E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.90305E+01 0.28672E+01
   Friction velocity        uet   :  0.15657E-01 0.82943E+01
   Friction velocity        uk    :  0.15656E-01 0.82943E+01
   Dimensionless distance   yplus :  0.10584E-02 0.99307E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4451
   Nb of faces within the viscous sub-layer     :      23385
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47861E+01      24   0.37807E-01   0.17603E+01 0.17370E+02 
c  Velocity[X]                                      0.48300E+00 
c  Velocity[Y]                                      0.63415E+00 
c  Velocity[Z]                                      0.64312E+00 
c  Pressure     0.20719E-01     272   0.26633E-01   0.85345E-01 0.63562E+00 
c  k            0.65913E-01      12   0.27427E-03   0.26944E-03 0.21240E+02 
c  epsilon      0.52440E+03      11   0.32732E-03   0.95866E+05 0.74126E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012998                             6
a  epsilon                -0.53798                            13
a  Local Time Step      4.2276e-08                        271507


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6044          8.7467         0.69191         0.11168
v  Velocity[Y]             -11.991          10.953         0.34997         0.26401
v  Velocity[Z]             -17.075          14.245        -0.31281      -0.0011704
v  ǁVelocityǁ           0.00031473          19.355          2.0937          2.2774
v  Pressure                 -13486           38379           24092           20557
v  k                    2.5105e-07          1.4461         0.01357        0.012487
v  epsilon              7.9215e-06      1.0216e+05          135.07          9.5302
v  TurbVisc             8.9173e-13         0.16883      0.00066887       0.0087462
v  CourantNb                     0          2197.4           13.53          2.5805
v  FourierNb              0.022318      2.3654e+05          21.817         0.29414
v  total_pressure       4.8651e+05      5.3838e+05      5.2409e+05      5.2056e+05
v  Local Time Step           0.001        0.071957       0.0010323       0.0010964


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52384      2.3874e+05          35.347          2.8746


 TIME FOR THE TIME STEP              264:        0.72334E+02

===============================================================


 INSTANT    0.265000000E+01   TIME STEP NUMBER             265
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.176206298E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989269688E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10677E+02 0.28566E+01
   Friction velocity        uet   :  0.18160E-01 0.74779E+01
   Friction velocity        uk    :  0.18157E-01 0.74779E+01
   Dimensionless distance   yplus :  0.54043E-03 0.99314E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4446
   Nb of faces within the viscous sub-layer     :      23383
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47855E+01      24   0.38824E-01   0.17725E+01 0.17437E+02 
c  Velocity[X]                                      0.49218E+00 
c  Velocity[Y]                                      0.62078E+00 
c  Velocity[Z]                                      0.65955E+00 
c  Pressure     0.20500E-01     252   0.26295E-01   0.84510E-01 0.64548E+00 
c  k            0.65970E-01      12   0.27602E-03   0.24340E-03 0.20172E+02 
c  epsilon      0.54228E+03      12   0.44256E-03   0.11951E+06 0.82303E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012952                             7
a  epsilon                -0.50175                            14
a  Local Time Step      4.2276e-08                        271515


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5957          8.4363         0.69173         0.11163
v  Velocity[Y]             -11.484          10.771         0.35041         0.26387
v  Velocity[Z]             -17.448          14.214        -0.31267      -0.0012064
v  ǁVelocityǁ           0.00060794           19.47          2.0946          2.2775
v  Pressure                 -13443           38380           24093           20559
v  k                     2.792e-07          1.4415        0.013576         0.01249
v  epsilon              9.7844e-06      1.0173e+05          135.55           9.541
v  TurbVisc             9.1325e-13         0.16883       0.0006693       0.0087479
v  CourantNb             0.0015846          1950.1          13.536          2.5811
v  FourierNb              0.022316      2.3654e+05          21.817         0.29423
v  total_pressure       4.8656e+05      5.3838e+05      5.2409e+05      5.2056e+05
v  Local Time Step           0.001         0.06182       0.0010325       0.0010965


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55781      2.3832e+05          35.352          2.8754


 TIME FOR THE TIME STEP              265:        0.63343E+02

===============================================================


 INSTANT    0.266000000E+01   TIME STEP NUMBER             266
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.199318998E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989264325E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88830E+01 0.28659E+01
   Friction velocity        uet   :  0.45466E-02 0.71880E+01
   Friction velocity        uk    :  0.45458E-02 0.71880E+01
   Dimensionless distance   yplus :  0.84807E-03 0.99312E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4450
   Nb of faces within the viscous sub-layer     :      23373
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47855E+01      25   0.38508E-01   0.17919E+01 0.17531E+02 
c  Velocity[X]                                      0.48735E+00 
c  Velocity[Y]                                      0.61203E+00 
c  Velocity[Z]                                      0.69248E+00 
c  Pressure     0.21037E-01     274   0.26622E-01   0.86692E-01 0.67856E+00 
c  k            0.65926E-01      13   0.23656E-03   0.25530E-03 0.20640E+02 
c  epsilon      0.52532E+03      10   0.37075E-03   0.11816E+06 0.82257E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00013074                             7
a  epsilon                 -0.4826                            13
a  Local Time Step      4.2276e-08                        271552


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5953          8.7295         0.69163         0.11149
v  Velocity[Y]             -11.555          10.852         0.35077         0.26372
v  Velocity[Z]             -17.055          14.189        -0.31224      -0.0013186
v  ǁVelocityǁ            0.0012185          19.331          2.0952          2.2778
v  Pressure                 -13386           38374           24094           20559
v  k                    2.5468e-07          1.4451         0.01358        0.012495
v  epsilon              3.9484e-06      1.0227e+05          135.36          9.5374
v  TurbVisc             1.0027e-12         0.16883      0.00066977       0.0087495
v  CourantNb              0.007181          2049.9          13.543          2.5817
v  FourierNb              0.022315      2.3654e+05          21.817         0.29427
v  total_pressure       4.8661e+05      5.3837e+05      5.2409e+05      5.2056e+05
v  Local Time Step           0.001        0.056914       0.0010326       0.0010962


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67895      2.3756e+05          35.359           2.876


 TIME FOR THE TIME STEP              266:        0.68577E+02

===============================================================


 INSTANT    0.267000000E+01   TIME STEP NUMBER             267
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.139313579E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989244051E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10737E+02 0.28608E+01
   Friction velocity        uet   :  0.96374E-02 0.94673E+01
   Friction velocity        uk    :  0.96289E-02 0.94673E+01
   Dimensionless distance   yplus :  0.12080E-02 0.99289E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4453
   Nb of faces within the viscous sub-layer     :      23377
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47854E+01      25   0.38153E-01   0.17720E+01 0.17423E+02 
c  Velocity[X]                                      0.47159E+00 
c  Velocity[Y]                                      0.64887E+00 
c  Velocity[Z]                                      0.65155E+00 
c  Pressure     0.20369E-01     302   0.25878E-01   0.83914E-01 0.71583E+00 
c  k            0.65968E-01      10   0.28051E-03   0.25429E-03 0.20553E+02 
c  epsilon      0.54036E+03      10   0.25107E-03   0.86198E+05 0.69998E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012936                             7
a  epsilon                 -0.2252                            12
a  Local Time Step      4.2276e-08                        271529


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6082          8.2882         0.69135          0.1114
v  Velocity[Y]              -12.34          10.735         0.35126         0.26369
v  Velocity[Z]             -17.392          14.081        -0.31167       -0.001405
v  ǁVelocityǁ            0.0014658          19.401          2.0953          2.2779
v  Pressure                 -13368           38368           24096           20561
v  k                    2.5056e-07          1.4301        0.013569        0.012498
v  epsilon              8.9008e-06      1.0122e+05          135.02          9.5429
v  TurbVisc             8.9112e-13         0.16883      0.00067042       0.0087511
v  CourantNb              0.001978          2221.2          13.545          2.5822
v  FourierNb              0.022315      2.3654e+05          21.818         0.29422
v  total_pressure       4.8663e+05      5.3837e+05       5.241e+05      5.2056e+05
v  Local Time Step           0.001        0.062605       0.0010327       0.0010956


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81625      2.3749e+05          35.363          2.8765


 TIME FOR THE TIME STEP              267:        0.61817E+02

===============================================================


 INSTANT    0.268000000E+01   TIME STEP NUMBER             268
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.862202613E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989308214E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89011E+01 0.28557E+01
   Friction velocity        uet   :  0.14000E-01 0.79323E+01
   Friction velocity        uk    :  0.13987E-01 0.79323E+01
   Dimensionless distance   yplus :  0.10122E-02 0.99255E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4458
   Nb of faces within the viscous sub-layer     :      23379
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47853E+01      24   0.37780E-01   0.17238E+01 0.17199E+02 
c  Velocity[X]                                      0.46744E+00 
c  Velocity[Y]                                      0.61117E+00 
c  Velocity[Z]                                      0.64524E+00 
c  Pressure     0.20126E-01     328   0.25745E-01   0.82864E-01 0.69251E+00 
c  k            0.65927E-01      12   0.28817E-03   0.22886E-03 0.19486E+02 
c  epsilon      0.52530E+03      15   0.51176E-03   0.12389E+06 0.84177E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012251                             6
a  epsilon                 -1.1304                            12
a  Local Time Step      4.2276e-08                        271571


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6129          8.5687         0.69074         0.11136
v  Velocity[Y]             -12.244          11.575         0.35171         0.26371
v  Velocity[Z]             -16.822          14.131        -0.31108      -0.0014877
v  ǁVelocityǁ            0.0017529           19.04          2.0949           2.278
v  Pressure                 -13386           38371           24097           20563
v  k                    2.5755e-07          1.4485        0.013587          0.0125
v  epsilon              9.1467e-06      1.0225e+05          135.75          9.5403
v  TurbVisc             9.0701e-13         0.16883      0.00067122       0.0087525
v  CourantNb             0.0058922          2035.5          13.555          2.5826
v  FourierNb              0.022316      2.3654e+05          21.818         0.29431
v  total_pressure       4.8661e+05      5.3837e+05       5.241e+05      5.2056e+05
v  Local Time Step           0.001        0.068865       0.0010328       0.0010959


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7366       2.382e+05          35.373          2.8769


 TIME FOR THE TIME STEP              268:        0.75112E+02

===============================================================


 INSTANT    0.269000000E+01   TIME STEP NUMBER             269
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.115026347E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989442202E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10485E+02 0.28503E+01
   Friction velocity        uet   :  0.20016E-01 0.66948E+01
   Friction velocity        uk    :  0.19997E-01 0.66948E+01
   Dimensionless distance   yplus :  0.75185E-03 0.99223E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4459
   Nb of faces within the viscous sub-layer     :      23364
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47854E+01      27   0.38421E-01   0.17563E+01 0.17360E+02 
c  Velocity[X]                                      0.47223E+00 
c  Velocity[Y]                                      0.62201E+00 
c  Velocity[Z]                                      0.66205E+00 
c  Pressure     0.20436E-01     308   0.25931E-01   0.84117E-01 0.63214E+00 
c  k            0.65976E-01      13   0.26669E-03   0.27234E-03 0.21265E+02 
c  epsilon      0.54152E+03       9   0.29694E-03   0.12425E+06 0.84014E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011777                             7
a  epsilon                -0.74467                            12
a  Local Time Step      4.2276e-08                        271588


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6089           8.329         0.69041         0.11129
v  Velocity[Y]             -11.014          11.055         0.35216         0.26363
v  Velocity[Z]              -17.35          14.156        -0.31053      -0.0015873
v  ǁVelocityǁ             0.001543          19.323           2.095          2.2781
v  Pressure                 -13351           38370           24097           20565
v  k                    2.5905e-07          1.4317        0.013572        0.012504
v  epsilon              1.5621e-05      1.0085e+05          135.08          9.5474
v  TurbVisc             9.3665e-13         0.16883      0.00067166       0.0087538
v  CourantNb             0.0035432          2042.5          13.555          2.5827
v  FourierNb              0.022317      2.3654e+05          21.818         0.29438
v  total_pressure       4.8665e+05      5.3837e+05       5.241e+05      5.2056e+05
v  Local Time Step           0.001        0.075752        0.001033       0.0010966


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73863      2.3841e+05          35.373          2.8771


 TIME FOR THE TIME STEP              269:        0.63455E+02

===============================================================


 INSTANT    0.270000000E+01   TIME STEP NUMBER             270
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.273470669E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989550342E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89141E+01 0.28519E+01
   Friction velocity        uet   :  0.19558E-01 0.92128E+01
   Friction velocity        uk    :  0.19324E-01 0.92128E+01
   Dimensionless distance   yplus :  0.11756E-02 0.99184E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4462
   Nb of faces within the viscous sub-layer     :      23364
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47855E+01      28   0.38222E-01   0.17453E+01 0.17304E+02 
c  Velocity[X]                                      0.48470E+00 
c  Velocity[Y]                                      0.61276E+00 
c  Velocity[Z]                                      0.64786E+00 
c  Pressure     0.20886E-01     382   0.26516E-01   0.85985E-01 0.79748E+00 
c  k            0.65932E-01      15   0.26885E-03   0.25596E-03 0.20611E+02 
c  epsilon      0.52663E+03      12   0.30996E-03   0.11461E+06 0.81073E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001272                             6
a  epsilon                -0.11047                            11
a  Local Time Step      4.2276e-08                        271567


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5996          8.6335         0.69004         0.11125
v  Velocity[Y]             -11.283          11.755         0.35227         0.26356
v  Velocity[Z]             -16.988          14.165        -0.30969      -0.0016411
v  ǁVelocityǁ            0.0013128          19.218          2.0947          2.2781
v  Pressure                 -13348           38375           24095           20563
v  k                    2.5073e-07          1.4433        0.013575        0.012505
v  epsilon              2.8664e-05      1.0177e+05          135.13          9.5349
v  TurbVisc             9.3695e-13         0.16883      0.00067249       0.0087549
v  CourantNb             0.0054288          2326.2          13.549          2.5831
v  FourierNb              0.022318      2.3654e+05          21.818          0.2945
v  total_pressure       4.8665e+05      5.3837e+05      5.2409e+05      5.2056e+05
v  Local Time Step           0.001        0.083327       0.0010332       0.0010971


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77907       2.375e+05          35.367          2.8776


 TIME FOR THE TIME STEP              270:        0.75457E+02

===============================================================


 INSTANT    0.271000000E+01   TIME STEP NUMBER             271
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.936847241E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989511527E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10660E+02 0.28522E+01
   Friction velocity        uet   :  0.18174E-01 0.73567E+01
   Friction velocity        uk    :  0.18138E-01 0.73567E+01
   Dimensionless distance   yplus :  0.76864E-03 0.99121E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4468
   Nb of faces within the viscous sub-layer     :      23356
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47852E+01      25   0.37868E-01   0.16883E+01 0.17012E+02 
c  Velocity[X]                                      0.46668E+00 
c  Velocity[Y]                                      0.61038E+00 
c  Velocity[Z]                                      0.61127E+00 
c  Pressure     0.20897E-01     277   0.26182E-01   0.85972E-01 0.54552E+00 
c  k            0.65985E-01      14   0.27311E-03   0.23656E-03 0.19680E+02 
c  epsilon      0.54247E+03      12   0.45872E-03   0.12766E+06 0.85089E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012688                             6
a  epsilon                -0.15161                            12
a  Local Time Step      4.2276e-08                        271540


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5751          8.4588          0.6896         0.11126
v  Velocity[Y]             -11.817          11.226         0.35266         0.26352
v  Velocity[Z]             -17.204          14.011         -0.3093      -0.0016791
v  ǁVelocityǁ            0.0014775          19.163           2.095          2.2781
v  Pressure                 -13371           38373           24094           20565
v  k                    2.5675e-07          1.4311        0.013589        0.012509
v  epsilon              4.5047e-05      1.0064e+05          135.78          9.5485
v  TurbVisc             9.0165e-13         0.16883      0.00067318       0.0087561
v  CourantNb             0.0075234            1976          13.548          2.5833
v  FourierNb               0.02232      2.3654e+05          21.819         0.29452
v  total_pressure       4.8663e+05      5.3837e+05      5.2409e+05      5.2056e+05
v  Local Time Step           0.001        0.089979       0.0010333       0.0010969


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81277      2.3764e+05          35.367          2.8778


 TIME FOR THE TIME STEP              271:        0.70907E+02

===============================================================


 INSTANT    0.272000000E+01   TIME STEP NUMBER             272
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.250651649E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989687829E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.91572E+01 0.28539E+01
   Friction velocity        uet   :  0.17591E-02 0.61999E+01
   Friction velocity        uk    :  0.17592E-02 0.61999E+01
   Dimensionless distance   yplus :  0.79111E-03 0.99084E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4468
   Nb of faces within the viscous sub-layer     :      23348
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47851E+01      26   0.37924E-01   0.16846E+01 0.16996E+02 
c  Velocity[X]                                      0.44887E+00 
c  Velocity[Y]                                      0.60485E+00 
c  Velocity[Z]                                      0.63085E+00 
c  Pressure     0.20519E-01     645   0.25640E-01   0.84433E-01 0.16675E+01 
c  k            0.65961E-01      17   0.31092E-03   0.21351E-03 0.18733E+02 
c  epsilon      0.53051E+03      10   0.36790E-03   0.11979E+06 0.82700E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011733                             5
a  epsilon                -0.25018                             9
a  Local Time Step      4.2276e-08                        271491


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5673          8.6023         0.68914         0.11126
v  Velocity[Y]             -12.505          11.652         0.35242         0.26349
v  Velocity[Z]             -16.948          14.119        -0.30884      -0.0016486
v  ǁVelocityǁ            0.0014517          19.164          2.0947           2.278
v  Pressure                 -13414           38317           24044           20524
v  k                     2.573e-07          1.4493        0.013576        0.012511
v  epsilon              4.5678e-05       1.024e+05           135.2          9.5455
v  TurbVisc             9.3046e-13         0.16883      0.00067394       0.0087571
v  CourantNb              0.018406          1990.7          13.555          2.5835
v  FourierNb              0.022323      2.3654e+05          21.819         0.29456
v  total_pressure       4.8659e+05      5.3832e+05      5.2404e+05      5.2052e+05
v  Local Time Step           0.001         0.07216       0.0010334       0.0010978


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77599      2.3773e+05          35.374          2.8781


 TIME FOR THE TIME STEP              272:        0.78880E+02

===============================================================


 INSTANT    0.273000000E+01   TIME STEP NUMBER             273
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.158828377E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989629798E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10769E+02 0.28710E+01
   Friction velocity        uet   :  0.10749E-01 0.94055E+01
   Friction velocity        uk    :  0.10702E-01 0.94055E+01
   Dimensionless distance   yplus :  0.30364E-03 0.99010E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4464
   Nb of faces within the viscous sub-layer     :      23330
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47844E+01      25   0.38134E-01   0.16685E+01 0.16905E+02 
c  Velocity[X]                                      0.45770E+00 
c  Velocity[Y]                                      0.58929E+00 
c  Velocity[Z]                                      0.62150E+00 
c  Pressure     0.20108E-01     265   0.25241E-01   0.82618E-01 0.50746E+00 
c  k            0.66004E-01      12   0.26120E-03   0.19761E-03 0.17962E+02 
c  epsilon      0.54466E+03      11   0.25939E-03   0.90454E+05 0.71656E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011324                             6
a  epsilon                 -0.1168                            12
a  Local Time Step      4.2276e-08                        271485


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5576          8.3552         0.68901         0.11123
v  Velocity[Y]             -12.547           11.12         0.35251         0.26357
v  Velocity[Z]             -17.154          14.128        -0.30863      -0.0016314
v  ǁVelocityǁ            0.0011537          19.062          2.0949           2.278
v  Pressure                 -13401           38312           24043           20525
v  k                    2.4964e-07          1.4417        0.013589        0.012515
v  epsilon              6.3221e-05      1.0254e+05          135.25          9.5514
v  TurbVisc              9.276e-13         0.16883      0.00067472       0.0087581
v  CourantNb             0.0066628          2106.5           13.55          2.5835
v  FourierNb              0.022326      2.3654e+05          21.819         0.29466
v  total_pressure        4.866e+05      5.3831e+05      5.2404e+05      5.2052e+05
v  Local Time Step           0.001        0.079376       0.0010335       0.0010986


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70633      2.3764e+05          35.369          2.8782


 TIME FOR THE TIME STEP              273:        0.72979E+02

===============================================================


 INSTANT    0.274000000E+01   TIME STEP NUMBER             274
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.105332977E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989602970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.90327E+01 0.28657E+01
   Friction velocity        uet   :  0.18985E-01 0.73832E+01
   Friction velocity        uk    :  0.18755E-01 0.73832E+01
   Dimensionless distance   yplus :  0.94209E-03 0.98952E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4469
   Nb of faces within the viscous sub-layer     :      23305
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47846E+01      26   0.38382E-01   0.16669E+01 0.16890E+02 
c  Velocity[X]                                      0.45719E+00 
c  Velocity[Y]                                      0.59402E+00 
c  Velocity[Z]                                      0.61570E+00 
c  Pressure     0.20518E-01     703   0.26086E-01   0.84870E-01 0.12928E+01 
c  k            0.65968E-01      12   0.30486E-03   0.24279E-03 0.20108E+02 
c  epsilon      0.53151E+03      12   0.49168E-03   0.12168E+06 0.83429E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001216                             6
a  epsilon                -0.24622                            11
a  Local Time Step      4.2276e-08                        271489


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5592          8.5734         0.68864         0.11122
v  Velocity[Y]             -12.341          11.681          0.3523          0.2636
v  Velocity[Z]             -16.894          14.159        -0.30821       -0.001523
v  ǁVelocityǁ           0.00096775          19.096           2.095          2.2779
v  Pressure                 -13451           38266           24006           20497
v  k                    2.5805e-07          1.4427        0.013604        0.012517
v  epsilon              6.0881e-05      1.0184e+05          135.72           9.551
v  TurbVisc             9.0121e-13         0.16883      0.00067564        0.008759
v  CourantNb             0.0044047          2175.2          13.558          2.5837
v  FourierNb              0.022328      2.3654e+05          21.819          0.2948
v  total_pressure       4.8655e+05      5.3827e+05      5.2401e+05       5.205e+05
v  Local Time Step           0.001        0.085152       0.0010335       0.0010995


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82728      2.3802e+05          35.377          2.8785


 TIME FOR THE TIME STEP              274:        0.88107E+02

===============================================================


 INSTANT    0.275000000E+01   TIME STEP NUMBER             275
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.128292555E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989555140E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10707E+02 0.28627E+01
   Friction velocity        uet   :  0.17775E-01 0.68213E+01
   Friction velocity        uk    :  0.17755E-01 0.68213E+01
   Dimensionless distance   yplus :  0.87040E-03 0.98903E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4470
   Nb of faces within the viscous sub-layer     :      23293
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47838E+01      24   0.37864E-01   0.16971E+01 0.17051E+02 
c  Velocity[X]                                      0.46120E+00 
c  Velocity[Y]                                      0.59176E+00 
c  Velocity[Z]                                      0.64414E+00 
c  Pressure     0.21035E-01     380   0.26605E-01   0.87075E-01 0.55373E+00 
c  k            0.66019E-01      12   0.25988E-03   0.21508E-03 0.18901E+02 
c  epsilon      0.54697E+03       8   0.29627E-03   0.98799E+05 0.74880E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012185                             6
a  epsilon                -0.10015                            11
a  Local Time Step      4.2276e-08                        271459


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5642          8.3903          0.6887         0.11127
v  Velocity[Y]             -11.493          11.002         0.35214         0.26365
v  Velocity[Z]             -16.982          14.103        -0.30798      -0.0014055
v  ǁVelocityǁ           0.00082627          19.059          2.0955          2.2778
v  Pressure                 -13418           38267           24004           20499
v  k                    2.5912e-07           1.438        0.013595         0.01252
v  epsilon              6.9761e-05      1.0185e+05          135.15          9.5596
v  TurbVisc             9.3907e-13         0.16883      0.00067633       0.0087598
v  CourantNb               0.01532          2109.4          13.561          2.5838
v  FourierNb              0.022331      2.3654e+05           21.82         0.29475
v  total_pressure       4.8658e+05      5.3827e+05        5.24e+05       5.205e+05
v  Local Time Step           0.001        0.069025       0.0010334       0.0010995


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69941      2.3838e+05          35.381          2.8785


 TIME FOR THE TIME STEP              275:        0.74780E+02

===============================================================


 INSTANT    0.276000000E+01   TIME STEP NUMBER             276
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.192648762E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989524305E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.94496E+01 0.28670E+01
   Friction velocity        uet   :  0.21397E-01 0.74243E+01
   Friction velocity        uk    :  0.21392E-01 0.74243E+01
   Dimensionless distance   yplus :  0.77209E-03 0.98862E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4467
   Nb of faces within the viscous sub-layer     :      23283
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47840E+01      27   0.37911E-01   0.16781E+01 0.16965E+02 
c  Velocity[X]                                      0.46481E+00 
c  Velocity[Y]                                      0.59481E+00 
c  Velocity[Z]                                      0.61846E+00 
c  Pressure     0.20520E-01     231   0.26003E-01   0.85039E-01 0.55435E+00 
c  k            0.65979E-01      15   0.30888E-03   0.22140E-03 0.19085E+02 
c  epsilon      0.53433E+03      10   0.33488E-03   0.10533E+06 0.77472E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011128                             6
a  epsilon                -0.17968                            10
a  Local Time Step      4.2276e-08                        271412


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5685          8.5156         0.68859         0.11128
v  Velocity[Y]             -10.708          11.741         0.35163         0.26368
v  Velocity[Z]             -16.881          14.161        -0.30788      -0.0013199
v  ǁVelocityǁ           0.00053197          19.056          2.0957          2.2779
v  Pressure                 -13431           38269           24004           20497
v  k                    2.6053e-07          1.4474        0.013605        0.012521
v  epsilon              7.1605e-05       1.025e+05          135.41           9.553
v  TurbVisc               9.44e-13         0.16883      0.00067698       0.0087605
v  CourantNb             0.0076604          2246.3          13.571          2.5841
v  FourierNb              0.022334      2.3654e+05           21.82         0.29489
v  total_pressure       4.8657e+05      5.3827e+05        5.24e+05       5.205e+05
v  Local Time Step           0.001        0.054307       0.0010336       0.0011008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97977      2.3811e+05           35.39           2.879


 TIME FOR THE TIME STEP              276:        0.66029E+02

===============================================================


 INSTANT    0.277000000E+01   TIME STEP NUMBER             277
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.137457487E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989478929E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10817E+02 0.28621E+01
   Friction velocity        uet   :  0.17556E-01 0.68075E+01
   Friction velocity        uk    :  0.17548E-01 0.68075E+01
   Dimensionless distance   yplus :  0.86864E-03 0.98816E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4467
   Nb of faces within the viscous sub-layer     :      23278
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47832E+01      26   0.39356E-01   0.17002E+01 0.17069E+02 
c  Velocity[X]                                      0.45926E+00 
c  Velocity[Y]                                      0.59293E+00 
c  Velocity[Z]                                      0.64800E+00 
c  Pressure     0.21149E-01     336   0.26895E-01   0.87704E-01 0.56394E+00 
c  k            0.66021E-01      14   0.28196E-03   0.20775E-03 0.18385E+02 
c  epsilon      0.54774E+03      13   0.45444E-03   0.10705E+06 0.77862E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010936                             5
a  epsilon                -0.10081                            10
a  Local Time Step      4.2276e-08                        271415


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5634          8.3916          0.6886         0.11126
v  Velocity[Y]             -10.989          10.864           0.351         0.26372
v  Velocity[Z]             -16.948          14.196        -0.30826      -0.0013039
v  ǁVelocityǁ           0.00038596          19.052          2.0966          2.2779
v  Pressure                 -13459           38257           24004           20498
v  k                     2.534e-07          1.4355         0.01363        0.012523
v  epsilon              8.2611e-05      1.0121e+05          136.05          9.5644
v  TurbVisc             9.4548e-13         0.16883      0.00067758       0.0087611
v  CourantNb              0.009709            2352          13.575          2.5843
v  FourierNb              0.022336      2.3654e+05           21.82         0.29481
v  total_pressure       4.8654e+05      5.3826e+05        5.24e+05       5.205e+05
v  Local Time Step           0.001        0.053754       0.0010334       0.0011008


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88632      2.3883e+05          35.395          2.8791


 TIME FOR THE TIME STEP              277:        0.67021E+02

===============================================================


 INSTANT    0.278000000E+01   TIME STEP NUMBER             278
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.823191341E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989473863E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96747E+01 0.28653E+01
   Friction velocity        uet   :  0.13229E-01 0.70775E+01
   Friction velocity        uk    :  0.13226E-01 0.70775E+01
   Dimensionless distance   yplus :  0.90309E-03 0.98795E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4470
   Nb of faces within the viscous sub-layer     :      23262
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47833E+01      26   0.38465E-01   0.17057E+01 0.17088E+02 
c  Velocity[X]                                      0.45554E+00 
c  Velocity[Y]                                      0.61040E+00 
c  Velocity[Z]                                      0.63977E+00 
c  Pressure     0.21294E-01     211   0.27029E-01   0.88354E-01 0.53686E+00 
c  k            0.65979E-01      11   0.31793E-03   0.18578E-03 0.17519E+02 
c  epsilon      0.53569E+03       9   0.35366E-03   0.98835E+05 0.75025E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011804                             6
a  epsilon                -0.34465                            11
a  Local Time Step      4.2276e-08                        271437


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5665          8.4017         0.68928         0.11126
v  Velocity[Y]             -12.077          11.575         0.35031         0.26367
v  Velocity[Z]             -16.704          14.156        -0.30848      -0.0013016
v  ǁVelocityǁ           0.00016146          18.821          2.0973          2.2779
v  Pressure                 -13411           38256           24004           20498
v  k                    2.3341e-07          1.4475         0.01361        0.012523
v  epsilon              6.8115e-05      1.0256e+05          135.42           9.557
v  TurbVisc             9.4098e-13         0.16883      0.00067809       0.0087616
v  CourantNb             0.0086498          2336.5          13.578          2.5848
v  FourierNb              0.022338      2.3654e+05           21.82         0.29492
v  total_pressure       4.8659e+05      5.3826e+05        5.24e+05       5.205e+05
v  Local Time Step           0.001        0.058877       0.0010335        0.001102


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76333      2.3888e+05          35.397          2.8797


 TIME FOR THE TIME STEP              278:        0.67367E+02

===============================================================


 INSTANT    0.279000000E+01   TIME STEP NUMBER             279
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.402443450E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989403326E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10746E+02 0.28666E+01
   Friction velocity        uet   :  0.63293E-02 0.77249E+01
   Friction velocity        uk    :  0.63263E-02 0.77249E+01
   Dimensionless distance   yplus :  0.43231E-03 0.98771E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4468
   Nb of faces within the viscous sub-layer     :      23254
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47831E+01      24   0.37682E-01   0.16550E+01 0.16833E+02 
c  Velocity[X]                                      0.46094E+00 
c  Velocity[Y]                                      0.57935E+00 
c  Velocity[Z]                                      0.61467E+00 
c  Pressure     0.20089E-01     223   0.25597E-01   0.83312E-01 0.53083E+00 
c  k            0.66004E-01      13   0.23734E-03   0.21025E-03 0.18691E+02 
c  epsilon      0.54553E+03      14   0.23480E-03   0.72284E+05 0.64016E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011961                             5
a  epsilon                -0.72676                            12
a  Local Time Step      4.2276e-08                        271439


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5839          8.3504         0.68955         0.11123
v  Velocity[Y]             -12.365          10.806         0.34978         0.26361
v  Velocity[Z]             -17.006          14.029        -0.30918      -0.0012617
v  ǁVelocityǁ            0.0002639           19.08          2.0983           2.278
v  Pressure                 -13423           38261           24003           20499
v  k                    1.9973e-07          1.4359         0.01363        0.012524
v  epsilon              8.0022e-05        1.02e+05          135.55          9.5645
v  TurbVisc             9.2674e-13         0.16883      0.00067857       0.0087621
v  CourantNb             0.0048619            2251          13.572          2.5851
v  FourierNb              0.022339      2.3654e+05           21.82         0.29495
v  total_pressure       4.8658e+05      5.3826e+05        5.24e+05       5.205e+05
v  Local Time Step           0.001        0.054674       0.0010336       0.0011017


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69495      2.3798e+05          35.392            2.88


 TIME FOR THE TIME STEP              279:        0.63464E+02

===============================================================


 INSTANT    0.280000000E+01   TIME STEP NUMBER             280
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.542664172E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989374035E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93348E+01 0.28541E+01
   Friction velocity        uet   :  0.97533E-02 0.64051E+01
   Friction velocity        uk    :  0.97508E-02 0.64051E+01
   Dimensionless distance   yplus :  0.45821E-03 0.98779E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4465
   Nb of faces within the viscous sub-layer     :      23252
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47831E+01      25   0.37774E-01   0.16585E+01 0.16852E+02 
c  Velocity[X]                                      0.45171E+00 
c  Velocity[Y]                                      0.59301E+00 
c  Velocity[Z]                                      0.61373E+00 
c  Pressure     0.20460E-01     451   0.26088E-01   0.84898E-01 0.62741E+00 
c  k            0.66019E-01      12   0.15462E-03   0.29192E-03 0.22049E+02 
c  epsilon      0.55100E+03      14   0.46926E-03   0.11100E+06 0.79123E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001073                             6
a  epsilon                -0.21799                            13
a  Local Time Step      4.2276e-08                        271472


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5912           8.235         0.68973         0.11126
v  Velocity[Y]             -11.978          11.438         0.34915         0.26364
v  Velocity[Z]             -16.529          14.096        -0.30992      -0.0012093
v  ǁVelocityǁ           0.00036672          18.511           2.099          2.2781
v  Pressure                 -13492           38270           24005           20504
v  k                    1.5463e-07          1.4334        0.013645        0.012525
v  epsilon              7.3824e-05      1.0078e+05          136.18          9.5717
v  TurbVisc             1.0861e-12         0.16883      0.00067909       0.0087625
v  CourantNb             0.0024891          2430.3          13.585          2.5855
v  FourierNb               0.02234      2.3654e+05           21.82         0.29506
v  total_pressure       4.8651e+05      5.3827e+05        5.24e+05       5.205e+05
v  Local Time Step           0.001        0.060142       0.0010337       0.0011032


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64069      2.3795e+05          35.405          2.8806


 TIME FOR THE TIME STEP              280:        0.78101E+02

===============================================================


 INSTANT    0.281000000E+01   TIME STEP NUMBER             281
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.113211284E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989332501E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10519E+02 0.28473E+01
   Friction velocity        uet   :  0.10923E-01 0.74925E+01
   Friction velocity        uk    :  0.10920E-01 0.74925E+01
   Dimensionless distance   yplus :  0.95380E-03 0.98783E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4457
   Nb of faces within the viscous sub-layer     :      23237
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47831E+01      26   0.37881E-01   0.16484E+01 0.16797E+02 
c  Velocity[X]                                      0.43823E+00 
c  Velocity[Y]                                      0.59149E+00 
c  Velocity[Z]                                      0.61868E+00 
c  Pressure     0.20169E-01     311   0.25706E-01   0.83585E-01 0.55096E+00 
c  k            0.65977E-01      13   0.24452E-03   0.23567E-03 0.19842E+02 
c  epsilon      0.53593E+03      10   0.37402E-03   0.14920E+06 0.92026E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010691                             6
a  epsilon                -0.26626                            11
a  Local Time Step      4.2276e-08                        271505


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6147          8.3532         0.69043         0.11128
v  Velocity[Y]             -11.899          10.995         0.34857         0.26368
v  Velocity[Z]             -16.994          14.145        -0.31087      -0.0011293
v  ǁVelocityǁ           0.00045506          19.073          2.1004          2.2782
v  Pressure                 -13505           38271           24006           20504
v  k                    1.4561e-07          1.4265        0.013645        0.012525
v  epsilon              4.1664e-05      1.0074e+05          135.93          9.5716
v  TurbVisc             8.4438e-13         0.16883      0.00067919       0.0087628
v  CourantNb             0.0021759          2416.5           13.59          2.5861
v  FourierNb              0.022341      2.3654e+05           21.82         0.29523
v  total_pressure       4.8649e+05      5.3827e+05      5.2401e+05       5.205e+05
v  Local Time Step           0.001        0.066156       0.0010339       0.0011047


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.79477      2.3873e+05          35.409          2.8813


 TIME FOR THE TIME STEP              281:        0.73328E+02

===============================================================


 INSTANT    0.282000000E+01   TIME STEP NUMBER             282
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.123256039E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989233206E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96368E+01 0.28618E+01
   Friction velocity        uet   :  0.10598E-01 0.73901E+01
   Friction velocity        uk    :  0.10596E-01 0.73901E+01
   Dimensionless distance   yplus :  0.22643E-03 0.98801E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4466
   Nb of faces within the viscous sub-layer     :      23230
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47835E+01      25   0.38368E-01   0.16583E+01 0.16851E+02 
c  Velocity[X]                                      0.47239E+00 
c  Velocity[Y]                                      0.58254E+00 
c  Velocity[Z]                                      0.60335E+00 
c  Pressure     0.20117E-01     478   0.25331E-01   0.83398E-01 0.76601E+00 
c  k            0.65985E-01      11   0.23506E-03   0.25939E-03 0.20850E+02 
c  epsilon      0.54140E+03       9   0.27602E-03   0.10627E+06 0.77715E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001095                             5
a  epsilon                -0.42236                            12
a  Local Time Step      4.2276e-08                        271579


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6109          8.2696         0.69097         0.11138
v  Velocity[Y]             -10.983          11.481         0.34804         0.26373
v  Velocity[Z]             -16.617           14.19        -0.31185      -0.0010612
v  ǁVelocityǁ           0.00052867          18.574          2.1016          2.2784
v  Pressure                 -13516           38278           24014           20508
v  k                    1.6739e-07          1.4427        0.013628        0.012525
v  epsilon              7.0715e-05      1.0212e+05          135.38          9.5654
v  TurbVisc             9.3495e-13         0.16883      0.00067951       0.0087631
v  CourantNb             0.0014779          1984.1          13.597          2.5867
v  FourierNb              0.022341      2.3654e+05           21.82         0.29533
v  total_pressure       4.8648e+05      5.3828e+05      5.2401e+05      5.2051e+05
v  Local Time Step           0.001        0.072772        0.001034       0.0011058


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.79294      2.3814e+05          35.417          2.8821


 TIME FOR THE TIME STEP              282:        0.69095E+02

===============================================================


 INSTANT    0.283000000E+01   TIME STEP NUMBER             283
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.935026997E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989107371E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10634E+02 0.28478E+01
   Friction velocity        uet   :  0.10863E-01 0.77529E+01
   Friction velocity        uk    :  0.10861E-01 0.77529E+01
   Dimensionless distance   yplus :  0.98927E-03 0.98823E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4471
   Nb of faces within the viscous sub-layer     :      23225
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47828E+01      27   0.37700E-01   0.16856E+01 0.16996E+02 
c  Velocity[X]                                      0.45555E+00 
c  Velocity[Y]                                      0.61098E+00 
c  Velocity[Z]                                      0.61904E+00 
c  Pressure     0.20418E-01     302   0.25839E-01   0.84609E-01 0.52332E+00 
c  k            0.65998E-01      12   0.12734E-03   0.18839E-03 0.17741E+02 
c  epsilon      0.54484E+03      12   0.40718E-03   0.86671E+05 0.70059E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011416                             6
a  epsilon                -0.36446                            11
a  Local Time Step      4.2276e-08                        271592


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -3.617          8.3725         0.69161         0.11143
v  Velocity[Y]              -11.14          11.059         0.34778         0.26374
v  Velocity[Z]             -17.078          14.157        -0.31282     -0.00096377
v  ǁVelocityǁ           0.00079973          19.155           2.103          2.2785
v  Pressure                 -13499           38289           24016           20509
v  k                    1.5605e-07          1.4301        0.013663        0.012526
v  epsilon              7.2978e-05      1.0044e+05          136.21           9.574
v  TurbVisc             1.1431e-12         0.16883      0.00067957       0.0087633
v  CourantNb             0.0034131          2049.7          13.597          2.5874
v  FourierNb              0.022341      2.3654e+05           21.82         0.29527
v  total_pressure        4.865e+05      5.3829e+05      5.2402e+05      5.2051e+05
v  Local Time Step           0.001        0.080049        0.001034       0.0011057


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74528      2.3806e+05          35.417          2.8826


 TIME FOR THE TIME STEP              283:        0.58940E+02

===============================================================


 INSTANT    0.284000000E+01   TIME STEP NUMBER             284
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.156203840E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.988990443E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.95473E+01 0.28604E+01
   Friction velocity        uet   :  0.11321E-01 0.10022E+02
   Friction velocity        uk    :  0.11318E-01 0.10022E+02
   Dimensionless distance   yplus :  0.95900E-03 0.98857E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4470
   Nb of faces within the viscous sub-layer     :      23224
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47830E+01      24   0.37916E-01   0.16682E+01 0.16908E+02 
c  Velocity[X]                                      0.45126E+00 
c  Velocity[Y]                                      0.58296E+00 
c  Velocity[Z]                                      0.63401E+00 
c  Pressure     0.20400E-01     817   0.25743E-01   0.84519E-01 0.42963E+01 
c  k            0.65983E-01      11   0.96145E-04   0.21554E-03 0.18975E+02 
c  epsilon      0.54180E+03      10   0.29872E-03   0.95981E+05 0.73801E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.5075e-05                             7
a  epsilon                -0.24426                            10
a  Local Time Step      4.2276e-08                        271607


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6076           8.203         0.69225         0.11148
v  Velocity[Y]             -11.438          11.532         0.34749         0.26375
v  Velocity[Z]             -16.515          14.143        -0.31394      -0.0012071
v  ǁVelocityǁ           0.00097936          18.559          2.1042          2.2789
v  Pressure                 -13401           38429           24153           20616
v  k                    1.8089e-07          1.4416        0.013651        0.012526
v  epsilon              5.7794e-05        1.02e+05          135.68          9.5719
v  TurbVisc             8.4958e-13         0.16883      0.00067953       0.0087635
v  CourantNb             0.0017472          2041.3          13.605          2.5881
v  FourierNb              0.022341      2.3654e+05           21.82         0.29531
v  total_pressure        4.866e+05      5.3843e+05      5.2415e+05      5.2062e+05
v  Local Time Step           0.001        0.070351       0.0010339       0.0011056


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74118      2.3858e+05          35.425          2.8834


 TIME FOR THE TIME STEP              284:        0.86010E+02

===============================================================


 INSTANT    0.285000000E+01   TIME STEP NUMBER             285
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.220830248E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989157521E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10529E+02 0.28448E+01
   Friction velocity        uet   :  0.12948E-01 0.75537E+01
   Friction velocity        uk    :  0.12939E-01 0.75537E+01
   Dimensionless distance   yplus :  0.59080E-03 0.98894E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4472
   Nb of faces within the viscous sub-layer     :      23210
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47841E+01      23   0.37851E-01   0.16662E+01 0.16899E+02 
c  Velocity[X]                                      0.44737E+00 
c  Velocity[Y]                                      0.58718E+00 
c  Velocity[Z]                                      0.63169E+00 
c  Pressure     0.19623E-01     325   0.24866E-01   0.81204E-01 0.68615E+00 
c  k            0.65939E-01      13   0.22530E-03   0.20645E-03 0.18413E+02 
c  epsilon      0.52646E+03      10   0.23158E-03   0.75329E+05 0.65644E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.1424e-05                             7
a  epsilon                -0.79844                            11
a  Local Time Step      4.2276e-08                        271625


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5977          8.3818          0.6927         0.11158
v  Velocity[Y]             -12.101          10.913          0.3475         0.26377
v  Velocity[Z]             -17.173          13.981        -0.31486      -0.0013475
v  ǁVelocityǁ            0.0005958          19.248          2.1057          2.2793
v  Pressure                 -13383           38451           24154           20616
v  k                    2.0012e-07          1.4271        0.013663        0.012529
v  epsilon              7.3645e-05      1.0019e+05          135.72           9.576
v  TurbVisc             9.0874e-13         0.16883      0.00067957       0.0087637
v  CourantNb             0.0023377          1805.5          13.611           2.589
v  FourierNb              0.022341      2.3654e+05           21.82         0.29536
v  total_pressure       4.8662e+05      5.3845e+05      5.2415e+05      5.2062e+05
v  Local Time Step           0.001        0.077386       0.0010339       0.0011061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66153       2.382e+05          35.431          2.8844


 TIME FOR THE TIME STEP              285:        0.59524E+02

===============================================================


 INSTANT    0.286000000E+01   TIME STEP NUMBER             286
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.255024916E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989287157E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98545E+01 0.28596E+01
   Friction velocity        uet   :  0.18317E-01 0.73916E+01
   Friction velocity        uk    :  0.18303E-01 0.73916E+01
   Dimensionless distance   yplus :  0.89937E-03 0.98960E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4476
   Nb of faces within the viscous sub-layer     :      23203
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47844E+01      25   0.37839E-01   0.16420E+01 0.16776E+02 
c  Velocity[X]                                      0.45201E+00 
c  Velocity[Y]                                      0.57934E+00 
c  Velocity[Z]                                      0.61061E+00 
c  Pressure     0.19818E-01     423   0.25063E-01   0.81961E-01 0.74082E+00 
c  k            0.65948E-01      16   0.24640E-03   0.31225E-03 0.22760E+02 
c  epsilon      0.53143E+03      14   0.46092E-03   0.13024E+06 0.86083E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010237                             7
a  epsilon                -0.54015                            13
a  Local Time Step      4.2276e-08                        271647


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6005          8.2921         0.69309         0.11162
v  Velocity[Y]             -12.357          11.593         0.34747         0.26378
v  Velocity[Z]             -16.757          14.034        -0.31558      -0.0014126
v  ǁVelocityǁ           0.00054755           18.73          2.1069          2.2799
v  Pressure                 -13378           38456           24156           20618
v  k                    2.2603e-07          1.4491        0.013681        0.012531
v  epsilon              5.9299e-05      1.0223e+05          136.29          9.5824
v  TurbVisc             1.0062e-12         0.16883      0.00067962       0.0087639
v  CourantNb             0.0023397          2299.3          13.627          2.5896
v  FourierNb              0.022341      2.3654e+05          21.819         0.29548
v  total_pressure       4.8662e+05      5.3846e+05      5.2416e+05      5.2062e+05
v  Local Time Step           0.001        0.085125        0.001034       0.0011072


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0264      2.3739e+05          35.447          2.8851


 TIME FOR THE TIME STEP              286:        0.80372E+02

===============================================================


 INSTANT    0.287000000E+01   TIME STEP NUMBER             287
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.277393837E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989330692E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10813E+02 0.28531E+01
   Friction velocity        uet   :  0.19484E-01 0.69493E+01
   Friction velocity        uk    :  0.19471E-01 0.69493E+01
   Dimensionless distance   yplus :  0.67821E-03 0.98988E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4481
   Nb of faces within the viscous sub-layer     :      23200
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47850E+01      27   0.37845E-01   0.16629E+01 0.16871E+02 
c  Velocity[X]                                      0.45005E+00 
c  Velocity[Y]                                      0.56806E+00 
c  Velocity[Z]                                      0.64478E+00 
c  Pressure     0.20167E-01     219   0.25548E-01   0.83247E-01 0.56467E+00 
c  k            0.65968E-01      13   0.73940E-04   0.14909E-03 0.15417E+02 
c  epsilon      0.53405E+03      13   0.23661E-03   0.55620E+05 0.56298E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -9.779e-05                             7
a  epsilon                -0.93832                            13
a  Local Time Step      4.2276e-08                        271665


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5871          8.3924         0.69351         0.11165
v  Velocity[Y]              -12.48          10.946         0.34732         0.26378
v  Velocity[Z]             -17.289          13.943        -0.31601      -0.0014208
v  ǁVelocityǁ            0.0005758          19.353           2.108          2.2804
v  Pressure                 -13297           38444           24156           20617
v  k                    2.5194e-07          1.4273        0.013667        0.012535
v  epsilon              6.5848e-05      1.0063e+05           135.7          9.5883
v  TurbVisc             9.1352e-13         0.16883      0.00067946       0.0087641
v  CourantNb             0.0044012          2211.4          13.637          2.5906
v  FourierNb               0.02234      2.3654e+05          21.819         0.29556
v  total_pressure        4.867e+05      5.3844e+05      5.2416e+05      5.2062e+05
v  Local Time Step           0.001        0.093637       0.0010342       0.0011078


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0263      2.3827e+05          35.456          2.8861


 TIME FOR THE TIME STEP              287:        0.69476E+02

===============================================================


 INSTANT    0.288000000E+01   TIME STEP NUMBER             288
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.552619058E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989399795E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98264E+01 0.28389E+01
   Friction velocity        uet   :  0.60310E-02 0.64588E+01
   Friction velocity        uk    :  0.60067E-02 0.64588E+01
   Dimensionless distance   yplus :  0.82414E-03 0.99021E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4481
   Nb of faces within the viscous sub-layer     :      23187
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47855E+01      26   0.38643E-01   0.16867E+01 0.16985E+02 
c  Velocity[X]                                      0.44141E+00 
c  Velocity[Y]                                      0.62292E+00 
c  Velocity[Z]                                      0.62236E+00 
c  Pressure     0.20642E-01     323   0.26044E-01   0.85040E-01 0.74011E+00 
c  k            0.65967E-01      12   0.71874E-04   0.16485E-03 0.16356E+02 
c  epsilon      0.53206E+03      10   0.18112E-03   0.31048E+05 0.42028E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.6991e-05                             7
a  epsilon                -0.63037                            13
a  Local Time Step      4.2276e-08                        271684


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5887           8.111         0.69346         0.11168
v  Velocity[Y]             -11.841          11.464         0.34737         0.26379
v  Velocity[Z]             -16.517          13.997        -0.31624      -0.0014131
v  ǁVelocityǁ           0.00075293          18.386          2.1088          2.2809
v  Pressure                 -13291           38456           24158           20612
v  k                    2.6379e-07          1.4341        0.013688        0.012538
v  epsilon              5.2705e-05      1.0068e+05          135.86          9.5949
v  TurbVisc             9.1381e-13         0.16883      0.00067944       0.0087643
v  CourantNb             0.0082981          1935.3          13.647          2.5912
v  FourierNb              0.022339      2.3654e+05           21.82         0.29561
v  total_pressure       4.8671e+05      5.3846e+05      5.2416e+05      5.2061e+05
v  Local Time Step           0.001           0.103       0.0010341       0.0011088


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89724      2.3838e+05          35.466          2.8868


 TIME FOR THE TIME STEP              288:        0.53954E+02

===============================================================


 INSTANT    0.289000000E+01   TIME STEP NUMBER             289
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.406637898E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989374080E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10523E+02 0.28449E+01
   Friction velocity        uet   :  0.18212E-01 0.75359E+01
   Friction velocity        uk    :  0.18195E-01 0.75359E+01
   Dimensionless distance   yplus :  0.80358E-03 0.99057E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4476
   Nb of faces within the viscous sub-layer     :      23174
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47852E+01      25   0.38247E-01   0.17529E+01 0.17307E+02 
c  Velocity[X]                                      0.46472E+00 
c  Velocity[Y]                                      0.62612E+00 
c  Velocity[Z]                                      0.66200E+00 
c  Pressure     0.21339E-01     286   0.26957E-01   0.87671E-01 0.72397E+00 
c  k            0.65966E-01      13   0.37915E-03   0.17995E-03 0.17041E+02 
c  epsilon      0.53124E+03      15   0.40017E-03   0.60021E+05 0.58511E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.6913e-05                             7
a  epsilon                 -0.8326                            16
a  Local Time Step      4.2276e-08                        271671


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5838          8.4559         0.69307         0.11174
v  Velocity[Y]             -12.172          11.215         0.34792         0.26384
v  Velocity[Z]             -17.344          14.042        -0.31642       -0.001373
v  ǁVelocityǁ           0.00059019          19.431          2.1096          2.2812
v  Pressure                 -13280           38471           24159           20610
v  k                    2.6227e-07          1.4308        0.013699        0.012541
v  epsilon              5.4147e-05      1.0079e+05          136.42          9.5963
v  TurbVisc             9.5942e-13         0.16883      0.00067947       0.0087646
v  CourantNb              0.013472          2145.4          13.649          2.5919
v  FourierNb              0.022339      2.3654e+05           21.82         0.29558
v  total_pressure       4.8672e+05      5.3847e+05      5.2416e+05      5.2061e+05
v  Local Time Step           0.001          0.1133       0.0010341       0.0011091


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60421      2.3762e+05          35.468          2.8875


 TIME FOR THE TIME STEP              289:        0.63995E+02

===============================================================


 INSTANT    0.290000000E+01   TIME STEP NUMBER             290
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.265535994E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989326870E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10053E+02 0.28653E+01
   Friction velocity        uet   :  0.15324E-01 0.79261E+01
   Friction velocity        uk    :  0.15133E-01 0.79261E+01
   Dimensionless distance   yplus :  0.78285E-03 0.99079E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4482
   Nb of faces within the viscous sub-layer     :      23171
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47853E+01      22   0.37453E-01   0.17249E+01 0.17136E+02 
c  Velocity[X]                                      0.48708E+00 
c  Velocity[Y]                                      0.57825E+00 
c  Velocity[Z]                                      0.65959E+00 
c  Pressure     0.21130E-01     224   0.26676E-01   0.86668E-01 0.61927E+00 
c  k            0.65973E-01      13   0.98480E-04   0.18477E-03 0.17313E+02 
c  epsilon      0.53160E+03      10   0.25448E-03   0.66262E+05 0.61441E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.2651e-05                             6
a  epsilon                -0.60568                            13
a  Local Time Step      4.2276e-08                        271665


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5764          8.0796         0.69278         0.11193
v  Velocity[Y]             -12.495          11.524         0.34819          0.2639
v  Velocity[Z]             -16.521          14.027        -0.31656      -0.0012816
v  ǁVelocityǁ           0.00081684          18.372          2.1103          2.2815
v  Pressure                 -13237           38478           24160           20610
v  k                    2.6384e-07          1.4461        0.013687        0.012545
v  epsilon              5.5482e-05      1.0257e+05          135.94             9.6
v  TurbVisc             9.4126e-13         0.16883      0.00067927       0.0087649
v  CourantNb              0.015273          2337.4          13.652          2.5923
v  FourierNb              0.022338      2.3654e+05           21.82         0.29568
v  total_pressure       4.8676e+05      5.3848e+05      5.2416e+05      5.2061e+05
v  Local Time Step           0.001         0.12463       0.0010342       0.0011105


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57344      2.3716e+05          35.472           2.888


 TIME FOR THE TIME STEP              290:        0.62208E+02

===============================================================


 INSTANT    0.291000000E+01   TIME STEP NUMBER             291
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.169426686E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989281970E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10427E+02 0.28500E+01
   Friction velocity        uet   :  0.19289E-01 0.56655E+01
   Friction velocity        uk    :  0.19270E-01 0.56655E+01
   Dimensionless distance   yplus :  0.57428E-03 0.99088E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4485
   Nb of faces within the viscous sub-layer     :      23157
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47853E+01      25   0.38420E-01   0.16773E+01 0.16911E+02 
c  Velocity[X]                                      0.46170E+00 
c  Velocity[Y]                                      0.54188E+00 
c  Velocity[Z]                                      0.67369E+00 
c  Pressure     0.20538E-01     220   0.25849E-01   0.84123E-01 0.59876E+00 
c  k            0.65972E-01      14   0.95500E-04   0.15149E-03 0.15851E+02 
c  epsilon      0.52934E+03      10   0.19799E-03   0.45221E+05 0.50831E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.9375e-05                             6
a  epsilon                -0.17637                            12
a  Local Time Step      4.2276e-08                        271667


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5848          8.3599         0.69239         0.11209
v  Velocity[Y]             -12.378          11.158         0.34857         0.26395
v  Velocity[Z]             -17.211          13.932        -0.31666      -0.0011716
v  ǁVelocityǁ            0.0011726          19.266          2.1111          2.2817
v  Pressure                 -13156           38477           24161           20610
v  k                      2.55e-07          1.4242        0.013704        0.012549
v  epsilon              4.0475e-05           99980             136          9.6065
v  TurbVisc             9.4374e-13         0.16883       0.0006793       0.0087653
v  CourantNb              0.016584          2207.3          13.663          2.5929
v  FourierNb              0.022337      2.3654e+05           21.82          0.2956
v  total_pressure       4.8684e+05      5.3848e+05      5.2416e+05      5.2061e+05
v  Local Time Step           0.001         0.11077        0.001034       0.0011098


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62078      2.3839e+05          35.483          2.8885


 TIME FOR THE TIME STEP              291:        0.48017E+02

===============================================================


 INSTANT    0.292000000E+01   TIME STEP NUMBER             292
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.653238682E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989185446E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99492E+01 0.28487E+01
   Friction velocity        uet   :  0.15445E-01 0.69104E+01
   Friction velocity        uk    :  0.15375E-01 0.69104E+01
   Dimensionless distance   yplus :  0.81048E-03 0.99100E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4487
   Nb of faces within the viscous sub-layer     :      23148
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47849E+01      26   0.38054E-01   0.17481E+01 0.17285E+02 
c  Velocity[X]                                      0.46473E+00 
c  Velocity[Y]                                      0.61506E+00 
c  Velocity[Z]                                      0.66828E+00 
c  Pressure     0.20520E-01     364   0.25945E-01   0.83946E-01 0.63203E+00 
c  k            0.65974E-01      16   0.87272E-04   0.16510E-03 0.16547E+02 
c  epsilon      0.52946E+03      12   0.42674E-03   0.56857E+05 0.56932E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -6.76e-05                             6
a  epsilon                -0.53751                            11
a  Local Time Step      4.2276e-08                        271617


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5857          8.0195         0.69178         0.11197
v  Velocity[Y]             -11.762          11.712         0.34879         0.26391
v  Velocity[Z]             -16.574          13.983        -0.31664       -0.001102
v  ǁVelocityǁ            0.0010579          18.409          2.1112          2.2817
v  Pressure                 -13104           38484           24166           20610
v  k                    2.5778e-07          1.4462        0.013713        0.012551
v  epsilon              5.0273e-05      1.0197e+05          136.52          9.6124
v  TurbVisc             9.0364e-13         0.16883      0.00067938       0.0087657
v  CourantNb              0.010093          2152.5          13.668          2.5934
v  FourierNb              0.022335      2.3654e+05           21.82         0.29573
v  total_pressure        4.869e+05      5.3848e+05      5.2417e+05      5.2061e+05
v  Local Time Step           0.001         0.10884       0.0010342       0.0011107


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94819      2.3838e+05          35.488          2.8891


 TIME FOR THE TIME STEP              292:        0.57994E+02

===============================================================


 INSTANT    0.293000000E+01   TIME STEP NUMBER             293
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.192497717E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989085885E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10330E+02 0.28481E+01
   Friction velocity        uet   :  0.20149E-01 0.61539E+01
   Friction velocity        uk    :  0.19905E-01 0.61539E+01
   Dimensionless distance   yplus :  0.66933E-03 0.99100E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4481
   Nb of faces within the viscous sub-layer     :      23138
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47848E+01      25   0.38243E-01   0.17418E+01 0.17252E+02 
c  Velocity[X]                                      0.45316E+00 
c  Velocity[Y]                                      0.60011E+00 
c  Velocity[Z]                                      0.68852E+00 
c  Pressure     0.20924E-01     204   0.26024E-01   0.85542E-01 0.53297E+00 
c  k            0.65974E-01      13   0.10764E-03   0.15286E-03 0.15634E+02 
c  epsilon      0.53146E+03      12   0.24719E-03   0.66271E+05 0.61381E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.8275e-05                             7
a  epsilon                -0.43929                            10
a  Local Time Step      4.2276e-08                        271607


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5908          8.3175         0.69139         0.11186
v  Velocity[Y]             -12.096          11.432         0.34894         0.26377
v  Velocity[Z]             -17.186          14.057        -0.31666      -0.0010524
v  ǁVelocityǁ           0.00088361          19.219          2.1119          2.2819
v  Pressure                 -13072           38485           24168           20611
v  k                    2.6464e-07           1.428         0.01372        0.012553
v  epsilon               3.573e-05      1.0032e+05          136.37          9.6153
v  TurbVisc             9.3122e-13         0.16883      0.00067938        0.008766
v  CourantNb             0.0054592          2284.1           13.67          2.5936
v  FourierNb              0.022334      2.3654e+05           21.82         0.29578
v  total_pressure       4.8693e+05      5.3849e+05      5.2417e+05      5.2061e+05
v  Local Time Step           0.001         0.10512       0.0010343       0.0011111


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88621      2.3782e+05           35.49          2.8894


 TIME FOR THE TIME STEP              293:        0.63196E+02

===============================================================


 INSTANT    0.294000000E+01   TIME STEP NUMBER             294
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.139457398E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.988946833E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10182E+02 0.28561E+01
   Friction velocity        uet   :  0.23257E-01 0.75424E+01
   Friction velocity        uk    :  0.23069E-01 0.75424E+01
   Dimensionless distance   yplus :  0.96241E-03 0.99082E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4479
   Nb of faces within the viscous sub-layer     :      23133
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47845E+01      25   0.38123E-01   0.17967E+01 0.17515E+02 
c  Velocity[X]                                      0.46416E+00 
c  Velocity[Y]                                      0.60711E+00 
c  Velocity[Z]                                      0.72538E+00 
c  Pressure     0.20516E-01     410   0.25492E-01   0.84019E-01 0.78801E+00 
c  k            0.65965E-01      15   0.92246E-04   0.19341E-03 0.17560E+02 
c  epsilon      0.53036E+03       9   0.18718E-03   0.44210E+05 0.50221E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -7.362e-05                             6
a  epsilon               -0.096491                             9
a  Local Time Step      4.2276e-08                        271595


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5826          7.8861         0.69072         0.11179
v  Velocity[Y]             -11.782          11.627         0.34912         0.26374
v  Velocity[Z]             -16.548          14.048        -0.31646     -0.00098175
v  ǁVelocityǁ            0.0012307          18.347          2.1119          2.2819
v  Pressure                 -13000           38503           24188           20624
v  k                    2.5567e-07           1.441        0.013707        0.012554
v  epsilon              4.4842e-05      1.0169e+05          135.99          9.6141
v  TurbVisc             9.5577e-13         0.16883      0.00067973       0.0087662
v  CourantNb                     0          2245.6          13.679          2.5941
v  FourierNb              0.022333      2.3654e+05           21.82         0.29593
v  total_pressure         4.87e+05       5.385e+05      5.2419e+05      5.2062e+05
v  Local Time Step           0.001         0.10264       0.0010345       0.0011125


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.95426      2.3745e+05            35.5            2.89


 TIME FOR THE TIME STEP              294:        0.69811E+02

===============================================================


 INSTANT    0.295000000E+01   TIME STEP NUMBER             295
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.110035889E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.988892982E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10028E+02 0.28394E+01
   Friction velocity        uet   :  0.18899E-01 0.75021E+01
   Friction velocity        uk    :  0.18877E-01 0.75021E+01
   Dimensionless distance   yplus :  0.74238E-03 0.99040E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4478
   Nb of faces within the viscous sub-layer     :      23139
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47842E+01      26   0.37183E-01   0.17562E+01 0.17329E+02 
c  Velocity[X]                                      0.47160E+00 
c  Velocity[Y]                                      0.58895E+00 
c  Velocity[Z]                                      0.69569E+00 
c  Pressure     0.20599E-01     656   0.25563E-01   0.84291E-01 0.17117E+01 
c  k            0.65965E-01      12   0.34834E-03   0.19507E-03 0.17927E+02 
c  epsilon      0.53160E+03      13   0.42743E-03   0.72276E+05 0.64173E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.5537e-05                             5
a  epsilon                -0.81694                             9
a  Local Time Step      4.2276e-08                        271592


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5845          8.2736         0.68997         0.11175
v  Velocity[Y]             -12.261          11.396         0.34916         0.26372
v  Velocity[Z]              -17.09          14.045        -0.31669      -0.0010775
v  ǁVelocityǁ            0.0010929          19.111          2.1121          2.2821
v  Pressure                 -12890           38565           24242           20667
v  k                    2.5623e-07            1.43        0.013735        0.012554
v  epsilon              4.1111e-05      1.0035e+05          136.81          9.6148
v  TurbVisc             9.1144e-13         0.16883      0.00068008       0.0087664
v  CourantNb              0.010552            2227          13.684          2.5943
v  FourierNb              0.022331      2.3654e+05           21.82         0.29599
v  total_pressure       4.8711e+05      5.3856e+05      5.2424e+05      5.2067e+05
v  Local Time Step           0.001        0.098728       0.0010344       0.0011133


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60369       2.383e+05          35.504          2.8903


 TIME FOR THE TIME STEP              295:        0.61989E+02

===============================================================


 INSTANT    0.296000000E+01   TIME STEP NUMBER             296
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.361369811E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989179128E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10211E+02 0.28480E+01
   Friction velocity        uet   :  0.20799E-01 0.92217E+01
   Friction velocity        uk    :  0.20632E-01 0.92217E+01
   Dimensionless distance   yplus :  0.70611E-03 0.98997E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4474
   Nb of faces within the viscous sub-layer     :      23124
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47850E+01      24   0.37678E-01   0.17365E+01 0.17223E+02 
c  Velocity[X]                                      0.45508E+00 
c  Velocity[Y]                                      0.60042E+00 
c  Velocity[Z]                                      0.68099E+00 
c  Pressure     0.20652E-01     253   0.25782E-01   0.84534E-01 0.54030E+00 
c  k            0.65958E-01      14   0.21948E-03   0.21395E-03 0.18468E+02 
c  epsilon      0.53117E+03      10   0.26872E-03   0.63957E+05 0.60416E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.5194e-05                             6
a  epsilon                 -1.6918                            10
a  Local Time Step      4.2276e-08                        271554


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5742          7.8687         0.68937         0.11162
v  Velocity[Y]             -11.976          11.717         0.34887         0.26373
v  Velocity[Z]             -16.449          14.044          -0.317      -0.0011575
v  ǁVelocityǁ            0.0010908          18.219          2.1121          2.2823
v  Pressure                 -12871           38560           24244           20668
v  k                    2.6038e-07          1.4391        0.013713        0.012556
v  epsilon              4.4748e-05      1.0155e+05          136.03           9.619
v  TurbVisc             9.2073e-13         0.16883      0.00068029       0.0087665
v  CourantNb             0.0048448          2104.2          13.673          2.5947
v  FourierNb              0.022329      2.3654e+05           21.82          0.2961
v  total_pressure       4.8713e+05      5.3856e+05      5.2424e+05      5.2067e+05
v  Local Time Step           0.001          0.1086       0.0010346       0.0011144


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62119       2.378e+05          35.493          2.8908


 TIME FOR THE TIME STEP              296:        0.57001E+02

===============================================================


 INSTANT    0.297000000E+01   TIME STEP NUMBER             297
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.170222359E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989121908E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99739E+01 0.28443E+01
   Friction velocity        uet   :  0.16860E-01 0.79128E+01
   Friction velocity        uk    :  0.16728E-01 0.79128E+01
   Dimensionless distance   yplus :  0.10097E-02 0.98935E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4479
   Nb of faces within the viscous sub-layer     :      23116
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47850E+01      26   0.38728E-01   0.17206E+01 0.17139E+02 
c  Velocity[X]                                      0.45123E+00 
c  Velocity[Y]                                      0.61260E+00 
c  Velocity[Z]                                      0.65678E+00 
c  Pressure     0.20559E-01     259   0.25689E-01   0.84291E-01 0.52412E+00 
c  k            0.65960E-01      13   0.44136E-03   0.19177E-03 0.17846E+02 
c  epsilon      0.53163E+03      12   0.15039E-03   0.38570E+05 0.46944E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.8507e-05                             5
a  epsilon                -0.40222                             9
a  Local Time Step      4.2276e-08                        271547


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -3.585          8.2669         0.68887         0.11155
v  Velocity[Y]             -11.676          11.301         0.34881         0.26377
v  Velocity[Z]             -16.999          13.922        -0.31728      -0.0012459
v  ǁVelocityǁ            0.0010041          19.027          2.1125          2.2823
v  Pressure                 -12856           38555           24245           20668
v  k                    2.5233e-07          1.4258        0.013726        0.012557
v  epsilon              3.9301e-05           99910          136.12          9.6145
v  TurbVisc             9.4017e-13         0.16883      0.00068055       0.0087666
v  CourantNb              0.003617            2195          13.672           2.595
v  FourierNb              0.022327      2.3654e+05           21.82         0.29615
v  total_pressure       4.8714e+05      5.3856e+05      5.2425e+05      5.2067e+05
v  Local Time Step           0.001         0.11946       0.0010347       0.0011157


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56359      2.3754e+05          35.493          2.8911


 TIME FOR THE TIME STEP              297:        0.67819E+02

===============================================================


 INSTANT    0.298000000E+01   TIME STEP NUMBER             298
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.335969090E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989218293E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96987E+01 0.28557E+01
   Friction velocity        uet   :  0.66703E-02 0.70708E+01
   Friction velocity        uk    :  0.66597E-02 0.70708E+01
   Dimensionless distance   yplus :  0.90044E-03 0.98879E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4476
   Nb of faces within the viscous sub-layer     :      23110
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47849E+01      26   0.38006E-01   0.17251E+01 0.17145E+02 
c  Velocity[X]                                      0.45914E+00 
c  Velocity[Y]                                      0.62457E+00 
c  Velocity[Z]                                      0.64137E+00 
c  Pressure     0.21191E-01     226   0.26404E-01   0.86976E-01 0.50983E+00 
c  k            0.65953E-01      13   0.24403E-03   0.23954E-03 0.19908E+02 
c  epsilon      0.52983E+03      13   0.44107E-03   0.76422E+05 0.66114E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.1167e-05                             5
a  epsilon               -0.088929                             7
a  Local Time Step      4.2276e-08                        271539


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5728          7.9432         0.68846         0.11147
v  Velocity[Y]             -12.359          11.805         0.34862         0.26379
v  Velocity[Z]              -16.24          13.976        -0.31719      -0.0013249
v  ǁVelocityǁ            0.0012296          17.964          2.1128          2.2824
v  Pressure                 -12811           38554           24246           20669
v  k                     2.585e-07          1.4413        0.013727        0.012559
v  epsilon              3.7363e-05      1.0162e+05          136.47          9.6252
v  TurbVisc             9.1547e-13         0.16883      0.00068093       0.0087669
v  CourantNb             0.0032556          2167.7          13.679          2.5954
v  FourierNb              0.022326      2.3654e+05           21.82         0.29637
v  total_pressure       4.8719e+05      5.3855e+05      5.2425e+05      5.2067e+05
v  Local Time Step           0.001         0.13116       0.0010349       0.0011177


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.93894      2.3814e+05          35.499          2.8918


 TIME FOR THE TIME STEP              298:        0.61976E+02

===============================================================


 INSTANT    0.299000000E+01   TIME STEP NUMBER             299
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.619408633E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989295752E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10147E+02 0.28387E+01
   Friction velocity        uet   :  0.13949E-01 0.83419E+01
   Friction velocity        uk    :  0.13910E-01 0.83419E+01
   Dimensionless distance   yplus :  0.97954E-03 0.98806E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4474
   Nb of faces within the viscous sub-layer     :      23103
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47845E+01      25   0.37258E-01   0.17115E+01 0.17087E+02 
c  Velocity[X]                                      0.47011E+00 
c  Velocity[Y]                                      0.61551E+00 
c  Velocity[Z]                                      0.62592E+00 
c  Pressure     0.21248E-01     244   0.26464E-01   0.87285E-01 0.53888E+00 
c  k            0.65922E-01      15   0.28451E-03   0.17538E-03 0.17079E+02 
c  epsilon      0.51949E+03      12   0.28507E-03   0.87372E+05 0.70729E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.2401e-05                             5
a  epsilon                -0.15224                             6
a  Local Time Step      4.2276e-08                        271495


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5725           8.266          0.6883         0.11143
v  Velocity[Y]               -12.5          11.341         0.34859         0.26381
v  Velocity[Z]             -17.032           14.02        -0.31754      -0.0014165
v  ǁVelocityǁ             0.001234          19.053          2.1136          2.2824
v  Pressure                 -12811           38554           24245           20671
v  k                       2.5e-07          1.4266        0.013731        0.012559
v  epsilon              3.8984e-05      1.0006e+05          136.11           9.621
v  TurbVisc              9.417e-13         0.16883       0.0006813       0.0087672
v  CourantNb            0.00027806          2142.2          13.678          2.5956
v  FourierNb              0.022324      2.3654e+05           21.82         0.29655
v  total_pressure       4.8719e+05      5.3855e+05      5.2424e+05      5.2067e+05
v  Local Time Step           0.001         0.14428       0.0010351       0.0011195


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83864      2.3829e+05          35.499          2.8922


 TIME FOR THE TIME STEP              299:        0.61579E+02

===============================================================


 INSTANT    0.300000000E+01   TIME STEP NUMBER             300
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.150989265E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989377548E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98974E+01 0.28552E+01
   Friction velocity        uet   :  0.13102E-01 0.77788E+01
   Friction velocity        uk    :  0.13043E-01 0.77788E+01
   Dimensionless distance   yplus :  0.82986E-03 0.98737E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4474
   Nb of faces within the viscous sub-layer     :      23096
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.47847E+01      24   0.37765E-01   0.17321E+01 0.17192E+02 
c  Velocity[X]                                      0.44870E+00 
c  Velocity[Y]                                      0.62447E+00 
c  Velocity[Z]                                      0.65893E+00 
c  Pressure     0.21627E-01     235   0.26950E-01   0.88873E-01 0.52768E+00 
c  k            0.65906E-01      11   0.21328E-03   0.17974E-03 0.17209E+02 
c  epsilon      0.51596E+03      13   0.23497E-03   0.40644E+05 0.48371E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.8671e-05                             5
a  epsilon               -0.077902                             7
a  Local Time Step      4.2276e-08                        271409


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5718          7.8936         0.68856         0.11126
v  Velocity[Y]             -12.235          11.651         0.34839         0.26382
v  Velocity[Z]             -16.177          14.057        -0.31781      -0.0015141
v  ǁVelocityǁ            0.0012559          17.905          2.1145          2.2827
v  Pressure                 -12784           38559           24244           20674
v  k                    2.5169e-07          1.4411        0.013739        0.012561
v  epsilon              3.1567e-05      1.0174e+05          136.19          9.6195
v  TurbVisc             8.9727e-13         0.16883      0.00068167       0.0087673
v  CourantNb              0.011042          2307.1          13.678          2.5958
v  FourierNb              0.022322      2.3654e+05          21.821         0.29658
v  total_pressure       4.8722e+05      5.3856e+05      5.2424e+05      5.2067e+05
v  Local Time Step           0.001         0.15871       0.0010352         0.00112


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81712      2.3844e+05          35.499          2.8924


 TIME FOR THE TIME STEP              300:        0.67204E+02

===============================================================


 INSTANT    0.301000000E+01   TIME STEP NUMBER             301
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.154097536E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989468638E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10072E+02 0.28526E+01
   Friction velocity        uet   :  0.88251E-02 0.72422E+01
   Friction velocity        uk    :  0.88091E-02 0.72422E+01
   Dimensionless distance   yplus :  0.73138E-03 0.98645E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4475
   Nb of faces within the viscous sub-layer     :      23097
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.48172E+01      25   0.38741E-01   0.78734E+03 0.27498E+03 
c  Velocity[X]                                      0.31101E+02 
c  Velocity[Y]                                      0.63155E+02 
c  Velocity[Z]                                      0.69309E+03 
c  Pressure     0.54932E-01    2006   0.11165E+01   0.22089E+00 0.87821E+03 
c  k            0.81993E-01      27   0.10757E-02   0.18054E-01 0.15724E+03 
c  epsilon      0.51617E+03      21   0.62694E-03   0.19807E+06 0.10906E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon               -0.021407                             1
a  Local Time Step      4.2276e-08                        271387


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.3194          10.975         0.84822         0.16236
v  Velocity[Y]             -15.336          13.629         0.54532          0.3757
v  Velocity[Z]             -19.762          15.095        -0.35768       0.0031727
v  ǁVelocityǁ            0.0018877          22.922          2.4803          3.0645
v  Pressure                 579.18      3.9263e+05      2.0785e+05      2.0103e+05
v  k                    2.7577e-07          1.3232        0.014196        0.013386
v  epsilon              0.00025208           93241           140.2          9.9705
v  TurbVisc             9.1026e-13         0.16883      0.00068202       0.0087675
v  CourantNb              0.002073          2329.5          13.683          2.5963
v  FourierNb              0.022321      2.3654e+05          21.821         0.29674
v  total_pressure       5.0058e+05      8.9263e+05      7.0785e+05      7.0103e+05
v  Local Time Step           0.001         0.17305       0.0010353       0.0011213


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64168      2.3829e+05          35.504          2.8931


 TIME FOR THE TIME STEP              301:        0.17588E+03

===============================================================


 INSTANT    0.302000000E+01   TIME STEP NUMBER             302
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.261021827E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156447565E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14088E+02 0.32356E+01
   Friction velocity        uet   :  0.12271E-01 0.25506E+02
   Friction velocity        uk    :  0.12111E-01 0.25506E+02
   Dimensionless distance   yplus :  0.31926E-02 0.11669E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5626
   Nb of faces within the viscous sub-layer     :      21036
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.86584E+01      50   0.38076E-01   0.26548E+03 0.14029E+03 
c  Velocity[X]                                      0.16038E+02 
c  Velocity[Y]                                      0.31510E+02 
c  Velocity[Z]                                      0.21793E+03 
c  Pressure     0.28780E+00    1794   0.28143E+00   0.10395E+01 0.46546E+03 
c  k            0.94248E-01      25   0.20834E-02   0.58620E-01 0.24201E+03 
c  epsilon      0.11894E+04      20   0.59790E-02   0.57423E+08 0.81151E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.7597e-05                             1
a  epsilon               -0.028771                             1
a  Local Time Step      4.2276e-08                        276822


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.3723          10.408         0.93954          0.1828
v  Velocity[Y]             -13.076           15.17         0.64081         0.43456
v  Velocity[Z]             -20.537          15.649        -0.35402       0.0097496
v  ǁVelocityǁ            0.0026833          23.393          2.6723          3.5034
v  Pressure                 225.63       2.601e+05      1.4514e+05      1.3544e+05
v  k                     2.675e-07          3.3822        0.020405        0.015104
v  epsilon              0.00025088      5.2102e+05          350.87          15.372
v  TurbVisc             9.9804e-13         0.20074      0.00070533       0.0093305
v  CourantNb             0.0073983          4238.4          16.992          3.5907
v  FourierNb              0.022317      2.3654e+05          21.778          0.2843
v  total_pressure       5.0023e+05       7.601e+05      6.4514e+05      6.3544e+05
v  Local Time Step           0.001         0.01595       0.0010061       0.0010338


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43907      2.3881e+05           38.77           3.875


 TIME FOR THE TIME STEP              302:        0.16678E+03

===============================================================


 INSTANT    0.303000000E+01   TIME STEP NUMBER             303
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.570122199E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156436474E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16461E+02 0.37706E+01
   Friction velocity        uet   :  0.33152E-01 0.30164E+02
   Friction velocity        uk    :  0.41320E-01 0.30164E+02
   Dimensionless distance   yplus :  0.27420E-02 0.12443E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6031
   Nb of faces within the viscous sub-layer     :      20652
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.88712E+01      46   0.36782E-01   0.29931E+02 0.46308E+02 
c  Velocity[X]                                      0.73132E+01 
c  Velocity[Y]                                      0.12233E+02 
c  Velocity[Z]                                      0.10385E+02 
c  Pressure     0.11144E+00    3487   0.51932E+00   0.36322E+00 0.14423E+04 
c  k            0.99822E-01      20   0.15262E-02   0.25915E-01 0.15397E+03 
c  epsilon      0.11121E+04      18   0.38488E-02   0.29573E+08 0.86861E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0016781                            77
a  epsilon                 -72.037                           124
a  Local Time Step      4.2275e-08                        275510


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.4755          10.484         0.96947         0.18193
v  Velocity[Y]             -12.689          17.164         0.63833         0.43806
v  Velocity[Z]             -21.987          15.973        -0.36608       0.0040537
v  ǁVelocityǁ            0.0023478          24.942          2.7576          3.5549
v  Pressure                -6389.4           93537           62187           51453
v  k                    3.2475e-07          2.0704         0.01822          0.0159
v  epsilon              0.00022461      2.5182e+05           239.5          14.061
v  TurbVisc             9.8037e-13          0.2131      0.00071646       0.0096367
v  CourantNb             0.0058318          8529.6          17.026          3.6384
v  FourierNb              0.022311      2.3654e+05          21.784         0.28507
v  total_pressure       4.9361e+05      5.9354e+05      5.6219e+05      5.5145e+05
v  Local Time Step           0.001        0.017545       0.0010071       0.0010337


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49201      2.4323e+05           38.81          3.9235


 TIME FOR THE TIME STEP              303:        0.25147E+03

===============================================================


 INSTANT    0.304000000E+01   TIME STEP NUMBER             304
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.267307580E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156487414E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18833E+02 0.38083E+01
   Friction velocity        uet   :  0.18971E-01 0.33436E+02
   Friction velocity        uk    :  0.18913E-01 0.33436E+02
   Dimensionless distance   yplus :  0.32546E-02 0.12419E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6181
   Nb of faces within the viscous sub-layer     :      20442
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.79926E+01      52   0.39407E-01   0.35838E+02 0.51643E+02 
c  Velocity[X]                                      0.54277E+01 
c  Velocity[Y]                                      0.11501E+02 
c  Velocity[Z]                                      0.18910E+02 
c  Pressure     0.17373E+00    2115   0.31007E+00   0.52566E+00 0.91159E+03 
c  k            0.10416E+00      22   0.37595E-03   0.78432E-02 0.81183E+02 
c  epsilon      0.11064E+04      21   0.19808E-02   0.57841E+07 0.34011E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.1814e-06                            16
a  epsilon                 -1.7786                            32
a  Local Time Step      4.2276e-08                        275275


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.5965          11.018         0.97528         0.17746
v  Velocity[Y]             -14.339          20.292         0.60153         0.42412
v  Velocity[Z]             -23.986          16.532        -0.37753      -0.0020215
v  ǁVelocityǁ            0.0029534          27.087          2.7995          3.4783
v  Pressure                 -39051           59186           32416           22179
v  k                    8.9331e-09          2.4715        0.019757        0.016597
v  epsilon              7.1803e-05      3.2354e+05          290.32          14.843
v  TurbVisc             1.2121e-12         0.21526      0.00071363       0.0098594
v  CourantNb                0.0229          8895.3          17.398           3.683
v  FourierNb              0.022303      2.3654e+05          21.785         0.28525
v  total_pressure       4.6095e+05      5.5919e+05      5.3242e+05      5.2218e+05
v  Local Time Step           0.001        0.017893       0.0010077       0.0010328


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35965      2.3663e+05          39.183          3.9682


 TIME FOR THE TIME STEP              304:        0.16195E+03

===============================================================


 INSTANT    0.305000000E+01   TIME STEP NUMBER             305
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.789746496E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156342124E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21852E+02 0.38421E+01
   Friction velocity        uet   :  0.27038E-01 0.30098E+02
   Friction velocity        uk    :  0.27806E-01 0.30098E+02
   Dimensionless distance   yplus :  0.33988E-02 0.12181E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6190
   Nb of faces within the viscous sub-layer     :      20241
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74466E+01      49   0.44064E-01   0.26444E+02 0.44855E+02 
c  Velocity[X]                                      0.51601E+01 
c  Velocity[Y]                                      0.99017E+01 
c  Velocity[Z]                                      0.11382E+02 
c  Pressure     0.12446E+00    1710   0.12826E+00   0.35514E+00 0.18831E+03 
c  k            0.10754E+00      20   0.27301E-03   0.59447E-02 0.68454E+02 
c  epsilon      0.11180E+04      19   0.10947E-02   0.35303E+07 0.26474E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028694                             6
a  epsilon                -0.99307                             4
a  Local Time Step      4.2276e-08                        275231


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.6437          11.553         0.98286         0.17579
v  Velocity[Y]              -14.98          18.604         0.57258          0.4158
v  Velocity[Z]             -25.855           17.48        -0.37909      -0.0038529
v  ǁVelocityǁ           0.00055198          29.095          2.8389          3.4325
v  Pressure                 -34065           66120           38912           29315
v  k                    1.2205e-07          2.3758        0.020383        0.017096
v  epsilon              0.00024515      3.0643e+05          299.09          15.082
v  TurbVisc             6.5678e-13         0.21566      0.00072888        0.010098
v  CourantNb              0.017437          6560.1          17.863          3.7167
v  FourierNb              0.022297      2.3654e+05           21.79         0.28553
v  total_pressure       4.6594e+05      5.6612e+05      5.3891e+05      5.2931e+05
v  Local Time Step           0.001        0.016204       0.0010082       0.0010313


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41014      2.4255e+05          39.653          4.0022


 TIME FOR THE TIME STEP              305:        0.14586E+03

===============================================================


 INSTANT    0.306000000E+01   TIME STEP NUMBER             306
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.172239726E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156472197E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24938E+02 0.38574E+01
   Friction velocity        uet   :  0.14498E-01 0.28826E+02
   Friction velocity        uk    :  0.14497E-01 0.28826E+02
   Dimensionless distance   yplus :  0.36550E-02 0.12060E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6208
   Nb of faces within the viscous sub-layer     :      20069
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.73868E+01      51   0.46291E-01   0.19846E+02 0.38735E+02 
c  Velocity[X]                                      0.44982E+01 
c  Velocity[Y]                                      0.87261E+01 
c  Velocity[Z]                                      0.66221E+01 
c  Pressure     0.80612E-01    1351   0.10835E+00   0.21967E+00 0.25679E+03 
c  k            0.11025E+00      21   0.29944E-03   0.57919E-02 0.65714E+02 
c  epsilon      0.11269E+04      19   0.24235E-02   0.95636E+07 0.39328E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015411                             3
a  epsilon                 -3.7667                             5
a  Local Time Step      4.2276e-08                        275180


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.7361          12.788         0.99734         0.17615
v  Velocity[Y]             -16.774           22.61         0.55988         0.41562
v  Velocity[Z]             -27.438          18.184        -0.37467      -0.0027945
v  ǁVelocityǁ           0.00060769          30.831          2.8857          3.4379
v  Pressure                 -22758           79430           51309           41910
v  k                    2.7108e-07          4.2878        0.021578         0.01755
v  epsilon              0.00023983       7.215e+05          352.55          15.518
v  TurbVisc             9.0871e-13          0.2159      0.00074306         0.01035
v  CourantNb             0.0049646          5414.8          18.265          3.7484
v  FourierNb              0.022294      2.3654e+05          21.795         0.28585
v  total_pressure       4.7724e+05      5.7943e+05      5.5131e+05      5.4191e+05
v  Local Time Step           0.001        0.011743       0.0010088         0.00103


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38383      2.4067e+05          40.059          4.0342


 TIME FOR THE TIME STEP              306:        0.13858E+03

===============================================================


 INSTANT    0.307000000E+01   TIME STEP NUMBER             307
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.100587612E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156512636E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27693E+02 0.40815E+01
   Friction velocity        uet   :  0.27135E-01 0.28222E+02
   Friction velocity        uk    :  0.27116E-01 0.28222E+02
   Dimensionless distance   yplus :  0.34060E-02 0.12056E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6265
   Nb of faces within the viscous sub-layer     :      19940
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75066E+01      49   0.47515E-01   0.17432E+02 0.36005E+02 
c  Velocity[X]                                      0.36966E+01 
c  Velocity[Y]                                      0.74764E+01 
c  Velocity[Z]                                      0.62587E+01 
c  Pressure     0.75674E-01    1455   0.92492E-01   0.19815E+00 0.10554E+03 
c  k            0.11265E+00      21   0.21760E-03   0.41908E-02 0.54587E+02 
c  epsilon      0.11681E+04      17   0.11771E-02   0.43259E+07 0.26491E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.4944e-06                             3
a  epsilon               -0.022569                             2
a  Local Time Step      4.2275e-08                        275259


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -3.9056          13.192          1.0132         0.17635
v  Velocity[Y]             -20.441          21.213         0.55753         0.41831
v  Velocity[Z]             -28.634           19.16        -0.37361      -0.0014148
v  ǁVelocityǁ           0.00055308          32.094          2.9342          3.4631
v  Pressure                 -17663           86011           57037           47558
v  k                    3.9174e-08          2.9182        0.022025        0.017982
v  epsilon              0.00022687      4.0359e+05          350.83          15.869
v  TurbVisc             9.3131e-13         0.21608      0.00075884        0.010605
v  CourantNb             0.0027618          4940.5          18.622          3.7778
v  FourierNb              0.022293      2.3654e+05          21.799         0.28624
v  total_pressure       4.8234e+05      5.8601e+05      5.5704e+05      5.4756e+05
v  Local Time Step           0.001        0.012917       0.0010092       0.0010291


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43554      2.3771e+05          40.421          4.0641


 TIME FOR THE TIME STEP              307:        0.13375E+03

===============================================================


 INSTANT    0.308000000E+01   TIME STEP NUMBER             308
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.109232112E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156448025E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29746E+02 0.40638E+01
   Friction velocity        uet   :  0.13517E-01 0.29541E+02
   Friction velocity        uk    :  0.13506E-01 0.29541E+02
   Dimensionless distance   yplus :  0.37142E-02 0.12080E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6335
   Nb of faces within the viscous sub-layer     :      19778
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.75986E+01      49   0.49169E-01   0.16028E+02 0.34246E+02 
c  Velocity[X]                                      0.32643E+01 
c  Velocity[Y]                                      0.68215E+01 
c  Velocity[Z]                                      0.59425E+01 
c  Pressure     0.72534E-01    1155   0.77852E-01   0.18378E+00 0.94186E+01 
c  k            0.11465E+00      19   0.20955E-03   0.40753E-02 0.52745E+02 
c  epsilon      0.11896E+04      15   0.12987E-02   0.53795E+07 0.27882E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017285                             3
a  epsilon                 -1.6192                             4
a  Local Time Step      4.2275e-08                        275251


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.128          15.418          1.0269         0.17577
v  Velocity[Y]             -18.839          22.025         0.55728         0.41991
v  Velocity[Z]              -31.12          20.099        -0.38018     -0.00089531
v  ǁVelocityǁ            0.0012523          35.209          2.9811          3.4851
v  Pressure                 -17857           86746           57207           47664
v  k                    3.1812e-07          3.2473        0.023051        0.018394
v  epsilon              0.00021373      4.7023e+05           383.1          16.328
v  TurbVisc              1.254e-12         0.21621      0.00077429        0.010852
v  CourantNb            0.00049491          5201.9          19.023          3.8044
v  FourierNb              0.022293      2.3655e+05          21.803         0.28662
v  total_pressure       4.8214e+05      5.8675e+05      5.5721e+05      5.4766e+05
v  Local Time Step           0.001        0.014209       0.0010096       0.0010285


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36302      2.4175e+05          40.826           4.091


 TIME FOR THE TIME STEP              308:        0.10921E+03

===============================================================


 INSTANT    0.309000000E+01   TIME STEP NUMBER             309
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.127594629E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156390748E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26037E+02 0.40892E+01
   Friction velocity        uet   :  0.26132E-01 0.31084E+02
   Friction velocity        uk    :  0.26127E-01 0.31084E+02
   Dimensionless distance   yplus :  0.39663E-02 0.12090E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6437
   Nb of faces within the viscous sub-layer     :      19598
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76240E+01      49   0.50270E-01   0.15525E+02 0.33558E+02 
c  Velocity[X]                                      0.32012E+01 
c  Velocity[Y]                                      0.67364E+01 
c  Velocity[Z]                                      0.55873E+01 
c  Pressure     0.69052E-01    1249   0.69563E-01   0.17007E+00 0.19928E+02 
c  k            0.11633E+00      20   0.21175E-03   0.35711E-02 0.48558E+02 
c  epsilon      0.12199E+04      18   0.20143E-02   0.56312E+07 0.27861E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020201                             4
a  epsilon                 -6.2763                             6
a  Local Time Step      4.2275e-08                        275336


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.2822          13.352          1.0371         0.17491
v  Velocity[Y]             -20.877          22.637         0.55904         0.42031
v  Velocity[Z]             -28.739          20.441        -0.39196      -0.0012636
v  ǁVelocityǁ            0.0013427          32.032          3.0237          3.4997
v  Pressure                 -19794           86029           56082           46584
v  k                    4.1245e-07          3.2221        0.023753        0.018777
v  epsilon              0.00020079      4.6528e+05          400.67          16.715
v  TurbVisc             1.4804e-12         0.21626      0.00079089        0.011085
v  CourantNb             0.0090734          7710.9          19.429          3.8285
v  FourierNb              0.022295      2.3655e+05          21.808         0.28699
v  total_pressure       4.8021e+05      5.8603e+05      5.5608e+05      5.4658e+05
v  Local Time Step           0.001         0.01563       0.0010099       0.0010283


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32539      2.4426e+05          41.236          4.1155


 TIME FOR THE TIME STEP              309:        0.12816E+03

===============================================================


 INSTANT    0.310000000E+01   TIME STEP NUMBER             310
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.490618482E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156473949E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29893E+02 0.41103E+01
   Friction velocity        uet   :  0.18745E-01 0.34039E+02
   Friction velocity        uk    :  0.18710E-01 0.34039E+02
   Dimensionless distance   yplus :  0.41726E-02 0.12092E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6502
   Nb of faces within the viscous sub-layer     :      19452
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76224E+01      55   0.50617E-01   0.15905E+02 0.33886E+02 
c  Velocity[X]                                      0.31389E+01 
c  Velocity[Y]                                      0.70574E+01 
c  Velocity[Z]                                      0.57091E+01 
c  Pressure     0.67889E-01    1298   0.64510E-01   0.16348E+00 0.12220E+02 
c  k            0.11773E+00      18   0.19081E-03   0.36402E-02 0.48332E+02 
c  epsilon      0.12561E+04      14   0.13868E-02   0.49483E+07 0.25322E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020067                             8
a  epsilon                 -1.3737                            19
a  Local Time Step      4.2275e-08                        275502


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.4738          13.512           1.044         0.17419
v  Velocity[Y]             -19.073          21.153         0.56107         0.42022
v  Velocity[Z]             -27.268          20.849        -0.40728      -0.0016699
v  ǁVelocityǁ           0.00088141            30.8          3.0623          3.5096
v  Pressure                 -21810           85482           55292           45936
v  k                    4.1163e-07          3.2322        0.024432        0.019123
v  epsilon              3.0605e-05      4.6889e+05          417.06          17.105
v  TurbVisc             1.7059e-12         0.21628      0.00080435        0.011305
v  CourantNb              0.001761          9583.2          19.827          3.8518
v  FourierNb              0.022298      2.3655e+05           21.81         0.28732
v  total_pressure       4.7819e+05      5.8548e+05      5.5529e+05      5.4594e+05
v  Local Time Step           0.001        0.016914       0.0010101       0.0010283


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51589      2.4613e+05          41.638          4.1391


 TIME FOR THE TIME STEP              310:        0.12931E+03

===============================================================


 INSTANT    0.311000000E+01   TIME STEP NUMBER             311
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.105713752E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156447045E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26622E+02 0.43072E+01
   Friction velocity        uet   :  0.13216E-01 0.35772E+02
   Friction velocity        uk    :  0.13208E-01 0.35772E+02
   Dimensionless distance   yplus :  0.40721E-02 0.12088E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6580
   Nb of faces within the viscous sub-layer     :      19298
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76200E+01      51   0.52251E-01   0.15142E+02 0.32983E+02 
c  Velocity[X]                                      0.29379E+01 
c  Velocity[Y]                                      0.65109E+01 
c  Velocity[Z]                                      0.56928E+01 
c  Pressure     0.67264E-01     602   0.61485E-01   0.15874E+00 0.37456E+01 
c  k            0.11887E+00      19   0.17471E-03   0.33783E-02 0.45985E+02 
c  epsilon      0.12957E+04      15   0.22125E-02   0.64258E+07 0.27751E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.3653e-06                             1
a  epsilon                -0.87083                            11
a  Local Time Step      4.2274e-08                        275674


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.6336          12.849          1.0496         0.17406
v  Velocity[Y]             -20.387          22.516         0.56317          0.4198
v  Velocity[Z]             -27.756          20.952        -0.42273      -0.0020573
v  ǁVelocityǁ            0.0015422          30.814          3.0966          3.5178
v  Pressure                 -23095           85627           55248           46005
v  k                    1.9938e-07          3.5898        0.025239        0.019435
v  epsilon              2.4414e-05      9.2796e+05          451.55          17.441
v  TurbVisc             1.4749e-12         0.21629        0.000819         0.01151
v  CourantNb            0.00011887           10432          20.172          3.8723
v  FourierNb              0.022302      2.3655e+05          21.813         0.28771
v  total_pressure       4.7691e+05      5.8563e+05      5.5525e+05      5.4601e+05
v  Local Time Step           0.001        0.017139       0.0010103       0.0010286


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44418      2.4698e+05          41.986            4.16


 TIME FOR THE TIME STEP              311:        0.87578E+02

===============================================================


 INSTANT    0.312000000E+01   TIME STEP NUMBER             312
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.224445902E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156489884E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27135E+02 0.46078E+01
   Friction velocity        uet   :  0.17358E-01 0.38501E+02
   Friction velocity        uk    :  0.17348E-01 0.38501E+02
   Dimensionless distance   yplus :  0.32549E-02 0.12188E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6645
   Nb of faces within the viscous sub-layer     :      19137
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76240E+01      52   0.54704E-01   0.14895E+02 0.32681E+02 
c  Velocity[X]                                      0.29347E+01 
c  Velocity[Y]                                      0.60553E+01 
c  Velocity[Z]                                      0.59056E+01 
c  Pressure     0.66027E-01     632   0.58827E-01   0.15357E+00 0.43039E+01 
c  k            0.11983E+00      17   0.21325E-03   0.32114E-02 0.44386E+02 
c  epsilon      0.13265E+04      19   0.14236E-02   0.56219E+07 0.25339E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.8874e-06                             1
a  epsilon                 -3.7257                             8
a  Local Time Step      4.2275e-08                        275838


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.676          12.433          1.0532         0.17408
v  Velocity[Y]             -17.809          19.662          0.5646         0.41956
v  Velocity[Z]             -25.668          20.396        -0.43948      -0.0019578
v  ǁVelocityǁ            0.0011938           28.44          3.1283          3.5251
v  Pressure                 -24417           85730           55217           46102
v  k                    3.4945e-07          3.2591        0.025818        0.019719
v  epsilon              0.00016502      5.4823e+05          461.75          17.738
v  TurbVisc             1.9061e-12         0.21629      0.00083241        0.011702
v  CourantNb             0.0081889           11301          20.483          3.8906
v  FourierNb              0.022306      2.3655e+05          21.816         0.28806
v  total_pressure       4.7558e+05      5.8573e+05      5.5522e+05       5.461e+05
v  Local Time Step           0.001        0.018853       0.0010105       0.0010295


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47856      2.4785e+05          42.298          4.1786


 TIME FOR THE TIME STEP              312:        0.93749E+02

===============================================================


 INSTANT    0.313000000E+01   TIME STEP NUMBER             313
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.937198717E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156439469E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24790E+02 0.46175E+01
   Friction velocity        uet   :  0.26009E-01 0.38816E+02
   Friction velocity        uk    :  0.25977E-01 0.38816E+02
   Dimensionless distance   yplus :  0.38631E-02 0.12216E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6715
   Nb of faces within the viscous sub-layer     :      18990
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76269E+01      48   0.54458E-01   0.14437E+02 0.32081E+02 
c  Velocity[X]                                      0.27960E+01 
c  Velocity[Y]                                      0.58913E+01 
c  Velocity[Z]                                      0.57501E+01 
c  Pressure     0.65494E-01     605   0.58153E-01   0.15057E+00 0.35120E+01 
c  k            0.12064E+00      17   0.20863E-03   0.30450E-02 0.42767E+02 
c  epsilon      0.13669E+04      14   0.98128E-03   0.47408E+07 0.22656E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.9632e-05                             2
a  epsilon                -0.19455                             5
a  Local Time Step      4.2274e-08                        275989


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.7575          14.398          1.0557         0.17422
v  Velocity[Y]             -17.809          21.492         0.56542         0.41941
v  Velocity[Z]             -27.984          21.029        -0.45529      -0.0015141
v  ǁVelocityǁ           0.00099678          31.894          3.1579          3.5319
v  Pressure                 -25797           85856           55208           46169
v  k                    3.2155e-07          3.2694        0.026446        0.019979
v  epsilon              0.00015579      6.3195e+05          485.85           18.04
v  TurbVisc             1.6627e-12         0.21629       0.0008431        0.011882
v  CourantNb                     0           11573          20.755          3.9065
v  FourierNb               0.02231      2.3655e+05          21.817         0.28842
v  total_pressure        4.742e+05      5.8586e+05      5.5521e+05      5.4617e+05
v  Local Time Step           0.001        0.020738       0.0010106       0.0010308


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41762      2.4812e+05          42.571           4.195


 TIME FOR THE TIME STEP              313:        0.89430E+02

===============================================================


 INSTANT    0.314000000E+01   TIME STEP NUMBER             314
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.260882734E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156381820E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25956E+02 0.46264E+01
   Friction velocity        uet   :  0.86694E-02 0.38536E+02
   Friction velocity        uk    :  0.86647E-02 0.38536E+02
   Dimensionless distance   yplus :  0.42712E-02 0.12195E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6777
   Nb of faces within the viscous sub-layer     :      18876
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76308E+01      51   0.55674E-01   0.14493E+02 0.32084E+02 
c  Velocity[X]                                      0.29092E+01 
c  Velocity[Y]                                      0.58718E+01 
c  Velocity[Z]                                      0.57121E+01 
c  Pressure     0.66141E-01     845   0.58537E-01   0.15047E+00 0.65833E+01 
c  k            0.12133E+00      17   0.19734E-03   0.32310E-02 0.43753E+02 
c  epsilon      0.13924E+04      16   0.83530E-03   0.43052E+07 0.21135E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.0457e-05                             3
a  epsilon                 -2.8068                            13
a  Local Time Step      4.2274e-08                        276151


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.806          14.957          1.0582          0.1744
v  Velocity[Y]             -18.432          20.441         0.56528          0.4194
v  Velocity[Z]             -27.489           21.19        -0.47085      -0.0013797
v  ǁVelocityǁ             0.001589          31.644          3.1871          3.5387
v  Pressure                 -26990           86315           55532           46483
v  k                    2.9393e-07          3.3238         0.02695        0.020214
v  epsilon              0.00014827      6.1284e+05          499.87          18.301
v  TurbVisc             1.8801e-12         0.21629      0.00085391        0.012048
v  CourantNb            0.00064142           10233          20.989          3.9215
v  FourierNb              0.022315      2.3655e+05          21.818         0.28881
v  total_pressure       4.7301e+05      5.8631e+05      5.5553e+05      5.4648e+05
v  Local Time Step           0.001        0.022812       0.0010106       0.0010324


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56835      2.4678e+05          42.807          4.2103


 TIME FOR THE TIME STEP              314:        0.94045E+02

===============================================================


 INSTANT    0.315000000E+01   TIME STEP NUMBER             315
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.820744547E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156384911E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24041E+02 0.46468E+01
   Friction velocity        uet   :  0.24571E-01 0.38496E+02
   Friction velocity        uk    :  0.24558E-01 0.38496E+02
   Dimensionless distance   yplus :  0.46201E-02 0.12184E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6834
   Nb of faces within the viscous sub-layer     :      18784
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76349E+01      50   0.55268E-01   0.15106E+02 0.32703E+02 
c  Velocity[X]                                      0.31160E+01 
c  Velocity[Y]                                      0.63473E+01 
c  Velocity[Z]                                      0.56430E+01 
c  Pressure     0.67398E-01     505   0.59124E-01   0.15217E+00 0.29156E+01 
c  k            0.12192E+00      19   0.20815E-03   0.31246E-02 0.42753E+02 
c  epsilon      0.14201E+04      16   0.73752E-03   0.42572E+07 0.20591E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.1792e-05                             1
a  epsilon               -0.010692                             4
a  Local Time Step      4.2274e-08                        276286


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.8275           16.45            1.06          0.1744
v  Velocity[Y]             -20.198          21.479         0.56456         0.41933
v  Velocity[Z]             -30.615          20.009        -0.48474     -0.00099506
v  ǁVelocityǁ            0.0011154          35.143          3.2137          3.5442
v  Pressure                 -28469           86431           55531           46501
v  k                    2.7012e-07          3.2765        0.027461         0.02043
v  epsilon              0.00014287        6.21e+05          513.64          18.565
v  TurbVisc             1.7722e-12          0.2163      0.00086326        0.012203
v  CourantNb             0.0056347          8695.5           21.21          3.9361
v  FourierNb               0.02232      2.3655e+05          21.819         0.28919
v  total_pressure       4.7153e+05      5.8643e+05      5.5553e+05       5.465e+05
v  Local Time Step           0.001        0.019643       0.0010107        0.001034


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62619      2.4525e+05          43.028          4.2252


 TIME FOR THE TIME STEP              315:        0.70005E+02

===============================================================


 INSTANT    0.316000000E+01   TIME STEP NUMBER             316
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.144974007E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156380697E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23796E+02 0.46464E+01
   Friction velocity        uet   :  0.15047E-01 0.38449E+02
   Friction velocity        uk    :  0.15042E-01 0.38449E+02
   Dimensionless distance   yplus :  0.49061E-02 0.12113E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6873
   Nb of faces within the viscous sub-layer     :      18670
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76372E+01      53   0.56001E-01   0.15117E+02 0.32703E+02 
c  Velocity[X]                                      0.31597E+01 
c  Velocity[Y]                                      0.64671E+01 
c  Velocity[Z]                                      0.54902E+01 
c  Pressure     0.67148E-01     749   0.58452E-01   0.15067E+00 0.50679E+01 
c  k            0.12241E+00      19   0.19171E-03   0.30883E-02 0.42307E+02 
c  epsilon      0.14453E+04      16   0.70917E-03   0.34784E+07 0.18318E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00065977                             2
a  epsilon                 -1.4616                             3
a  Local Time Step      4.2274e-08                        276460


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9095          15.408          1.0617         0.17445
v  Velocity[Y]             -20.218          19.687         0.56354         0.41924
v  Velocity[Z]             -27.607          20.855        -0.49714     -0.00092624
v  ǁVelocityǁ            0.0010338          31.911          3.2385          3.5499
v  Pressure                 -29715           86832           55785           46720
v  k                    2.4987e-07          3.2912        0.027892        0.020622
v  epsilon              0.00013588      6.1606e+05          526.72          18.777
v  TurbVisc             1.8535e-12          0.2163        0.000873        0.012345
v  CourantNb             0.0042639          6110.2          21.402          3.9489
v  FourierNb              0.022325      2.3655e+05           21.82         0.28936
v  total_pressure       4.7028e+05      5.8683e+05      5.5578e+05      5.4672e+05
v  Local Time Step           0.001        0.021608       0.0010107       0.0010356


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62515      2.4266e+05          43.223          4.2383


 TIME FOR THE TIME STEP              316:        0.88140E+02

===============================================================


 INSTANT    0.317000000E+01   TIME STEP NUMBER             317
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.130420345E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156397912E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25356E+02 0.46454E+01
   Friction velocity        uet   :  0.21570E-01 0.36185E+02
   Friction velocity        uk    :  0.21555E-01 0.36185E+02
   Dimensionless distance   yplus :  0.46172E-02 0.12071E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6913
   Nb of faces within the viscous sub-layer     :      18551
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76403E+01      49   0.57359E-01   0.15058E+02 0.32615E+02 
c  Velocity[X]                                      0.30668E+01 
c  Velocity[Y]                                      0.66113E+01 
c  Velocity[Z]                                      0.53798E+01 
c  Pressure     0.66810E-01     678   0.57853E-01   0.14875E+00 0.30371E+01 
c  k            0.12281E+00      18   0.23037E-03   0.36998E-02 0.46150E+02 
c  epsilon      0.14734E+04      18   0.12499E-02   0.64294E+07 0.24226E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.9639e-05                             1
a  epsilon                -0.45181                             2
a  Local Time Step      4.2274e-08                        276550


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9811           16.51          1.0646         0.17422
v  Velocity[Y]             -18.505          19.913         0.56281         0.41902
v  Velocity[Z]             -30.515          21.646        -0.50789     -0.00092422
v  ǁVelocityǁ            0.0016684          35.066          3.2609          3.5545
v  Pressure                 -31163           86973           55809           46741
v  k                    2.3325e-07           3.261        0.028449        0.020791
v  epsilon               0.0001302      6.1617e+05          548.23          19.013
v  TurbVisc             1.9208e-12          0.2163      0.00088161        0.012476
v  CourantNb              0.010816          5082.1          21.586          3.9614
v  FourierNb               0.02233      2.3655e+05          21.823         0.28964
v  total_pressure       4.6884e+05      5.8697e+05      5.5581e+05      5.4674e+05
v  Local Time Step           0.001        0.020833       0.0010106       0.0010366


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54529      2.4156e+05          43.409           4.251


 TIME FOR THE TIME STEP              317:        0.89364E+02

===============================================================


 INSTANT    0.318000000E+01   TIME STEP NUMBER             318
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.887849396E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156390546E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22931E+02 0.46311E+01
   Friction velocity        uet   :  0.30453E-01 0.35298E+02
   Friction velocity        uk    :  0.30447E-01 0.35298E+02
   Dimensionless distance   yplus :  0.44353E-02 0.12068E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6935
   Nb of faces within the viscous sub-layer     :      18453
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76405E+01      50   0.56950E-01   0.14946E+02 0.32464E+02 
c  Velocity[X]                                      0.31095E+01 
c  Velocity[Y]                                      0.67184E+01 
c  Velocity[Z]                                      0.51185E+01 
c  Pressure     0.67932E-01     948   0.58291E-01   0.15037E+00 0.34978E+01 
c  k            0.12316E+00      18   0.15929E-03   0.27629E-02 0.39820E+02 
c  epsilon      0.14914E+04      15   0.77000E-03   0.29098E+07 0.16446E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.9922e-05                             2
a  epsilon                 -9.0317                             5
a  Local Time Step      4.2274e-08                        276724


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.1701          15.655          1.0677         0.17406
v  Velocity[Y]             -20.239          18.479         0.56079         0.41895
v  Velocity[Z]             -27.884          20.824        -0.51666       -0.001215
v  ǁVelocityǁ            0.0012863          32.279          3.2802          3.5589
v  Pressure                 -32403           87251           55935           46839
v  k                    2.1951e-07          3.2952        0.028492        0.020932
v  epsilon              0.00012654      6.1138e+05          541.76          19.095
v  TurbVisc             2.0176e-12          0.2163      0.00088815        0.012597
v  CourantNb              0.011895          5082.7          21.752          3.9719
v  FourierNb              0.022336      2.3655e+05          21.823         0.28972
v  total_pressure        4.676e+05      5.8725e+05      5.5594e+05      5.4684e+05
v  Local Time Step           0.001        0.022917       0.0010104       0.0010371


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62952      2.3981e+05          43.575          4.2616


 TIME FOR THE TIME STEP              318:        0.96073E+02

===============================================================


 INSTANT    0.319000000E+01   TIME STEP NUMBER             319
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.413869280E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156399009E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27101E+02 0.46208E+01
   Friction velocity        uet   :  0.24901E-01 0.32238E+02
   Friction velocity        uk    :  0.24873E-01 0.32238E+02
   Dimensionless distance   yplus :  0.41136E-02 0.12064E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6973
   Nb of faces within the viscous sub-layer     :      18344
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76422E+01      45   0.57417E-01   0.15439E+02 0.32980E+02 
c  Velocity[X]                                      0.31002E+01 
c  Velocity[Y]                                      0.73194E+01 
c  Velocity[Z]                                      0.50198E+01 
c  Pressure     0.67329E-01     782   0.56773E-01   0.14849E+00 0.28919E+01 
c  k            0.12345E+00      19   0.13850E-03   0.23635E-02 0.36754E+02 
c  epsilon      0.15046E+04      16   0.57655E-03   0.16380E+07 0.12205E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.8435e-05                             6
a  epsilon                 -7.0263                            18
a  Local Time Step      4.2274e-08                        276805


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3512          16.212          1.0723         0.17402
v  Velocity[Y]             -18.451          19.998         0.55812         0.41889
v  Velocity[Z]              -29.95          20.369        -0.52279      -0.0016216
v  ǁVelocityǁ            0.0017386          34.426          3.2963          3.5633
v  Pressure                 -33697           87399           55932           46870
v  k                    9.5474e-08          3.2728        0.028801        0.021064
v  epsilon              0.00012473      6.0712e+05          553.13           19.24
v  TurbVisc             2.0796e-12          0.2163       0.0008932        0.012707
v  CourantNb             0.0079015          4662.6          21.895          3.9814
v  FourierNb              0.022342      2.3655e+05          21.823         0.28985
v  total_pressure        4.663e+05       5.874e+05      5.5593e+05      5.4687e+05
v  Local Time Step           0.001        0.025208       0.0010103       0.0010382


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59236      2.3941e+05          43.719          4.2713


 TIME FOR THE TIME STEP              319:        0.10092E+03

===============================================================


 INSTANT    0.320000000E+01   TIME STEP NUMBER             320
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.125244497E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156437251E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23319E+02 0.46253E+01
   Friction velocity        uet   :  0.33145E-01 0.30869E+02
   Friction velocity        uk    :  0.33122E-01 0.30869E+02
   Dimensionless distance   yplus :  0.39389E-02 0.12060E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7005
   Nb of faces within the viscous sub-layer     :      18198
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76444E+01      46   0.57453E-01   0.15970E+02 0.33501E+02 
c  Velocity[X]                                      0.32110E+01 
c  Velocity[Y]                                      0.76504E+01 
c  Velocity[Z]                                      0.51081E+01 
c  Pressure     0.68759E-01     600   0.56580E-01   0.15112E+00 0.26682E+01 
c  k            0.12372E+00      19   0.18482E-03   0.25776E-02 0.38284E+02 
c  epsilon      0.15124E+04      18   0.70038E-03   0.32512E+07 0.17061E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.8651e-07                             1
a  epsilon                -0.61044                             1
a  Local Time Step      4.2274e-08                        276843


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4546          16.066          1.0765          0.1744
v  Velocity[Y]             -19.307          17.831         0.55589         0.41948
v  Velocity[Z]             -28.121          20.624        -0.52649      -0.0020586
v  ǁVelocityǁ            0.0018123          32.697          3.3101          3.5675
v  Pressure                 -34865           87552           55919           46883
v  k                    1.9999e-07           3.293        0.028977        0.021189
v  epsilon              0.00012482      6.1078e+05          557.33          19.389
v  TurbVisc             2.2005e-12          0.2163      0.00089655        0.012809
v  CourantNb               0.01036            5213          22.027          3.9899
v  FourierNb              0.022348      2.3655e+05          21.822         0.29004
v  total_pressure       4.6514e+05      5.8755e+05      5.5592e+05      5.4688e+05
v  Local Time Step           0.001        0.027729       0.0010103       0.0010388


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70097      2.3907e+05           43.85            4.28


 TIME FOR THE TIME STEP              320:        0.91474E+02

===============================================================


 INSTANT    0.321000000E+01   TIME STEP NUMBER             321
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.307962853E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156464841E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27896E+02 0.46054E+01
   Friction velocity        uet   :  0.30297E-01 0.29895E+02
   Friction velocity        uk    :  0.30271E-01 0.29895E+02
   Dimensionless distance   yplus :  0.27188E-02 0.12058E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7011
   Nb of faces within the viscous sub-layer     :      18069
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76453E+01      46   0.57078E-01   0.15859E+02 0.33352E+02 
c  Velocity[X]                                      0.31937E+01 
c  Velocity[Y]                                      0.74776E+01 
c  Velocity[Z]                                      0.51878E+01 
c  Pressure     0.71379E-01    1171   0.57105E-01   0.15654E+00 0.37893E+01 
c  k            0.12392E+00      20   0.17059E-03   0.22895E-02 0.35962E+02 
c  epsilon      0.15170E+04      14   0.61120E-03   0.20389E+07 0.13549E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00045294                             4
a  epsilon                 -3.2735                             3
a  Local Time Step      4.2274e-08                        276965


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5678          15.428          1.0824         0.17506
v  Velocity[Y]             -18.532          19.864         0.55431         0.42002
v  Velocity[Z]             -28.564          20.769          -0.527      -0.0024077
v  ǁVelocityǁ            0.0019874          32.823          3.3218          3.5712
v  Pressure                 -36051           87487           55709           46743
v  k                    1.9444e-07          3.2531        0.029112        0.021303
v  epsilon              0.00012488      6.0155e+05          559.54          19.482
v  TurbVisc             2.4901e-12          0.2163       0.0008998        0.012902
v  CourantNb              0.016897          5740.8          22.139          3.9975
v  FourierNb              0.022355      2.3655e+05          21.821         0.29011
v  total_pressure       4.6395e+05      5.8749e+05      5.5571e+05      5.4674e+05
v  Local Time Step           0.001        0.030502       0.0010101       0.0010391


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53469      2.3975e+05           43.96          4.2877


 TIME FOR THE TIME STEP              321:        0.11651E+03

===============================================================


 INSTANT    0.322000000E+01   TIME STEP NUMBER             322
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.122165616E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156491525E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24475E+02 0.46005E+01
   Friction velocity        uet   :  0.16024E-01 0.31225E+02
   Friction velocity        uk    :  0.15935E-01 0.31225E+02
   Dimensionless distance   yplus :  0.35993E-02 0.12056E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7006
   Nb of faces within the viscous sub-layer     :      17986
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76484E+01      44   0.57164E-01   0.15272E+02 0.32705E+02 
c  Velocity[X]                                      0.30084E+01 
c  Velocity[Y]                                      0.70459E+01 
c  Velocity[Z]                                      0.52177E+01 
c  Pressure     0.70916E-01    1014   0.56523E-01   0.15521E+00 0.41385E+01 
c  k            0.12411E+00      20   0.15360E-03   0.15875E-02 0.29827E+02 
c  epsilon      0.15281E+04      15   0.39124E-03   0.12544E+07 0.10607E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1855e-06                             1
a  epsilon                  -3.706                             5
a  Local Time Step      4.2274e-08                        277038


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6966          15.603          1.0865         0.17546
v  Velocity[Y]             -20.003          17.632         0.55373         0.41994
v  Velocity[Z]             -28.154          20.713        -0.52579      -0.0026401
v  ǁVelocityǁ            0.0019976          32.256          3.3323          3.5751
v  Pressure                 -36964           87377           55469           46578
v  k                    1.9166e-07          3.2968        0.029173        0.021401
v  epsilon              0.00012593      6.0317e+05          557.15          19.546
v  TurbVisc             1.0569e-12          0.2163      0.00090337        0.012987
v  CourantNb             0.0066651          5983.9           22.22          4.0043
v  FourierNb              0.022362      2.3655e+05           21.82         0.29021
v  total_pressure       4.6304e+05      5.8738e+05      5.5547e+05      5.4658e+05
v  Local Time Step           0.001         0.03224       0.0010099       0.0010393


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5851       2.397e+05           44.04          4.2945


 TIME FOR THE TIME STEP              322:        0.99538E+02

===============================================================


 INSTANT    0.323000000E+01   TIME STEP NUMBER             323
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.233583260E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156508092E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29147E+02 0.45905E+01
   Friction velocity        uet   :  0.24887E-01 0.30398E+02
   Friction velocity        uk    :  0.24659E-01 0.30398E+02
   Dimensionless distance   yplus :  0.36860E-02 0.12053E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6992
   Nb of faces within the viscous sub-layer     :      17863
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76510E+01      43   0.56884E-01   0.15149E+02 0.32540E+02 
c  Velocity[X]                                      0.30307E+01 
c  Velocity[Y]                                      0.66863E+01 
c  Velocity[Z]                                      0.54321E+01 
c  Pressure     0.70057E-01     677   0.55320E-01   0.15302E+00 0.23875E+01 
c  k            0.12429E+00      16   0.13911E-03   0.19003E-02 0.32694E+02 
c  epsilon      0.15347E+04      13   0.41554E-03   0.12141E+07 0.10414E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.3199e-06                             1
a  epsilon                 -3.0264                             1
a  Local Time Step      4.2275e-08                        277147


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.7921          15.084          1.0905         0.17565
v  Velocity[Y]             -18.659          20.058         0.55525         0.41974
v  Velocity[Z]             -30.321          20.831        -0.52341      -0.0029837
v  ǁVelocityǁ            0.0020016          33.684          3.3421          3.5791
v  Pressure                 -37435           87456           55435           46581
v  k                    1.9156e-07          3.2449        0.029414        0.021499
v  epsilon              0.00012847      5.9985e+05          560.62          19.673
v  TurbVisc             2.3982e-12          0.2163      0.00090613        0.013065
v  CourantNb              0.014373          5890.4          22.287          4.0107
v  FourierNb              0.022369      2.3655e+05           21.82         0.29033
v  total_pressure       4.6256e+05      5.8746e+05      5.5543e+05      5.4658e+05
v  Local Time Step           0.001        0.020467       0.0010098       0.0010397


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41218      2.4174e+05          44.107           4.301


 TIME FOR THE TIME STEP              323:        0.85089E+02

===============================================================


 INSTANT    0.324000000E+01   TIME STEP NUMBER             324
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.102025017E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156547354E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26403E+02 0.45683E+01
   Friction velocity        uet   :  0.25072E-01 0.29467E+02
   Friction velocity        uk    :  0.25046E-01 0.29467E+02
   Dimensionless distance   yplus :  0.37114E-02 0.12063E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7006
   Nb of faces within the viscous sub-layer     :      17766
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76555E+01      42   0.58106E-01   0.14911E+02 0.32273E+02 
c  Velocity[X]                                      0.30018E+01 
c  Velocity[Y]                                      0.61321E+01 
c  Velocity[Z]                                      0.57768E+01 
c  Pressure     0.69110E-01     851   0.54438E-01   0.15069E+00 0.55642E+01 
c  k            0.12437E+00      18   0.16233E-03   0.14611E-02 0.28652E+02 
c  epsilon      0.15263E+04      10   0.60077E-03   0.15342E+07 0.11623E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.5599e-07                             1
a  epsilon                 -3.2371                             3
a  Local Time Step      4.2275e-08                        277308


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.8737          14.796          1.0927         0.17545
v  Velocity[Y]             -20.076           18.07         0.55753         0.41953
v  Velocity[Z]             -28.736          20.872        -0.51897      -0.0026219
v  ǁVelocityǁ            0.0022646          32.513          3.3489          3.5824
v  Pressure                 -38119           87175           55057           46296
v  k                    1.9469e-07          3.2864        0.029555        0.021584
v  epsilon              0.00013225      5.9299e+05          567.14          19.721
v  TurbVisc             2.0271e-12          0.2163      0.00090959        0.013135
v  CourantNb             0.0014497          6448.6          22.342          4.0173
v  FourierNb              0.022376      2.3655e+05          21.819         0.29045
v  total_pressure       4.6188e+05      5.8717e+05      5.5506e+05       5.463e+05
v  Local Time Step           0.001        0.019237       0.0010096       0.0010402


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58399      2.4135e+05          44.161          4.3077


 TIME FOR THE TIME STEP              324:        0.10139E+03

===============================================================


 INSTANT    0.325000000E+01   TIME STEP NUMBER             325
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.538058154E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156526960E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30076E+02 0.45738E+01
   Friction velocity        uet   :  0.29296E-01 0.25722E+02
   Friction velocity        uk    :  0.29007E-01 0.25722E+02
   Dimensionless distance   yplus :  0.32822E-02 0.12136E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6989
   Nb of faces within the viscous sub-layer     :      17712
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76542E+01      39   0.58178E-01   0.15375E+02 0.32735E+02 
c  Velocity[X]                                      0.32071E+01 
c  Velocity[Y]                                      0.62339E+01 
c  Velocity[Z]                                      0.59336E+01 
c  Pressure     0.70440E-01     500   0.54509E-01   0.15330E+00 0.20262E+01 
c  k            0.12448E+00      18   0.11635E-03   0.14116E-02 0.28148E+02 
c  epsilon      0.15269E+04      15   0.36676E-03   0.81746E+06 0.84977E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00086577                             3
a  epsilon                 -4.2827                             4
a  Local Time Step      4.2275e-08                        277504


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5639          14.136          1.0944         0.17565
v  Velocity[Y]             -18.315          18.756         0.56114          0.4202
v  Velocity[Z]             -28.832          21.152        -0.51357      -0.0025043
v  ǁVelocityǁ            0.0016093          32.091          3.3546          3.5854
v  Pressure                 -38267           87224           55040           46297
v  k                    2.0173e-07          3.2684        0.029685        0.021664
v  epsilon              0.00013865      5.9798e+05          567.36           19.78
v  TurbVisc             2.1788e-12          0.2163       0.0009126          0.0132
v  CourantNb              0.011886          6482.4          22.358          4.0228
v  FourierNb              0.022384      2.3655e+05          21.818         0.29049
v  total_pressure       4.6173e+05      5.8722e+05      5.5504e+05       5.463e+05
v  Local Time Step           0.001        0.020134       0.0010094       0.0010404


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35105      2.4154e+05          44.176          4.3133


 TIME FOR THE TIME STEP              325:        0.73043E+02

===============================================================


 INSTANT    0.326000000E+01   TIME STEP NUMBER             326
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.133049139E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156505898E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30130E+02 0.45511E+01
   Friction velocity        uet   :  0.25596E-01 0.18273E+02
   Friction velocity        uk    :  0.25583E-01 0.18273E+02
   Dimensionless distance   yplus :  0.23316E-02 0.12099E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6998
   Nb of faces within the viscous sub-layer     :      17664
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76557E+01      47   0.55530E-01   0.14953E+02 0.32254E+02 
c  Velocity[X]                                      0.32713E+01 
c  Velocity[Y]                                      0.55910E+01 
c  Velocity[Z]                                      0.60909E+01 
c  Pressure     0.68132E-01     542   0.52906E-01   0.14793E+00 0.19887E+01 
c  k            0.12458E+00      22   0.12538E-03   0.14014E-02 0.28014E+02 
c  epsilon      0.15265E+04      15   0.45028E-03   0.16809E+07 0.12157E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.7931e-06                             3
a  epsilon                   -3.45                            11
a  Local Time Step      4.2275e-08                        277635


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.693          14.732          1.0958          0.1758
v  Velocity[Y]             -19.765          17.995         0.56562         0.42102
v  Velocity[Z]              -29.48          21.026        -0.50806      -0.0024746
v  ǁVelocityǁ            0.0024962          33.332          3.3593          3.5884
v  Pressure                 -38286           87216           55026           46305
v  k                    2.1362e-07          3.2416        0.029781         0.02173
v  epsilon              0.00014667      5.8833e+05          569.45          19.825
v  TurbVisc             1.9888e-12          0.2163      0.00091525        0.013258
v  CourantNb             0.0069544          6692.3          22.367          4.0276
v  FourierNb              0.022393      2.3655e+05          21.818          0.2905
v  total_pressure       4.6171e+05      5.8722e+05      5.5503e+05       5.463e+05
v  Local Time Step           0.001        0.022148       0.0010092         0.00104


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53611      2.4144e+05          44.185          4.3181


 TIME FOR THE TIME STEP              326:        0.85869E+02

===============================================================


 INSTANT    0.327000000E+01   TIME STEP NUMBER             327
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.138011714E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156530352E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30759E+02 0.45570E+01
   Friction velocity        uet   :  0.30901E-01 0.17538E+02
   Friction velocity        uk    :  0.30092E-01 0.17538E+02
   Dimensionless distance   yplus :  0.13973E-02 0.12226E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6997
   Nb of faces within the viscous sub-layer     :      17625
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76590E+01      41   0.56406E-01   0.14225E+02 0.31430E+02 
c  Velocity[X]                                      0.32252E+01 
c  Velocity[Y]                                      0.50548E+01 
c  Velocity[Z]                                      0.59450E+01 
c  Pressure     0.64657E-01     943   0.50640E-01   0.14043E+00 0.51049E+01 
c  k            0.12467E+00      19   0.10067E-03   0.12174E-02 0.26086E+02 
c  epsilon      0.15322E+04      18   0.30170E-03   0.10745E+07 0.97067E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -2.5492                             3
a  Local Time Step      4.2275e-08                        277820


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.7824          13.826          1.0968         0.17559
v  Velocity[Y]             -18.443          20.098         0.57075         0.42141
v  Velocity[Z]             -29.595          21.088        -0.50196      -0.0021481
v  ǁVelocityǁ            0.0015484          32.916          3.3626          3.5908
v  Pressure                 -38574           86871           54697           46044
v  k                    2.3122e-07          3.2579        0.029867         0.02179
v  epsilon              0.00016037      5.9248e+05          570.38          19.843
v  TurbVisc             1.9553e-12          0.2163      0.00091781        0.013311
v  CourantNb            3.1407e-05          6919.9          22.376          4.0325
v  FourierNb              0.022402      2.3655e+05          21.817         0.29053
v  total_pressure       4.6143e+05      5.8687e+05       5.547e+05      5.4604e+05
v  Local Time Step           0.001        0.024362        0.001009       0.0010401


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69089      2.4183e+05          44.193          4.3231


 TIME FOR THE TIME STEP              327:        0.98224E+02

===============================================================


 INSTANT    0.328000000E+01   TIME STEP NUMBER             328
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.338145974E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156478010E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31585E+02 0.45528E+01
   Friction velocity        uet   :  0.34068E-01 0.16388E+02
   Friction velocity        uk    :  0.33454E-01 0.16388E+02
   Dimensionless distance   yplus :  0.15561E-02 0.12207E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6985
   Nb of faces within the viscous sub-layer     :      17607
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76594E+01      41   0.57511E-01   0.14258E+02 0.31459E+02 
c  Velocity[X]                                      0.33001E+01 
c  Velocity[Y]                                      0.49657E+01 
c  Velocity[Z]                                      0.59919E+01 
c  Pressure     0.64353E-01     511   0.51191E-01   0.13969E+00 0.20704E+01 
c  k            0.12472E+00      16   0.99288E-04   0.12033E-02 0.25911E+02 
c  epsilon      0.15294E+04      15   0.52798E-03   0.14225E+07 0.11141E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.1409e-05                             6
a  epsilon                 -5.2551                             7
a  Local Time Step      4.2275e-08                        277992


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.0139          14.726          1.0964          0.1753
v  Velocity[Y]             -20.048          18.475         0.57569         0.42152
v  Velocity[Z]             -29.006          21.346        -0.49619      -0.0018687
v  ǁVelocityǁ           0.00070387          32.755          3.3649          3.5933
v  Pressure                 -38307           86866           54696           46059
v  k                    2.5496e-07          3.2567        0.029945        0.021839
v  epsilon              0.00017665      5.9186e+05          576.81          19.861
v  TurbVisc             1.9358e-12          0.2163      0.00092079        0.013358
v  CourantNb              0.014263          7434.2           22.38          4.0366
v  FourierNb              0.022412      2.3655e+05          21.817         0.29061
v  total_pressure       4.6169e+05      5.8687e+05       5.547e+05      5.4606e+05
v  Local Time Step           0.001        0.026799       0.0010088       0.0010404


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55942      2.4109e+05          44.197          4.3272


 TIME FOR THE TIME STEP              328:        0.82167E+02

===============================================================


 INSTANT    0.329000000E+01   TIME STEP NUMBER             329
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.269924880E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156440915E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30445E+02 0.45392E+01
   Friction velocity        uet   :  0.14232E-01 0.17445E+02
   Friction velocity        uk    :  0.14086E-01 0.17445E+02
   Dimensionless distance   yplus :  0.14879E-02 0.12231E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6971
   Nb of faces within the viscous sub-layer     :      17596
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76613E+01      38   0.56590E-01   0.13912E+02 0.31041E+02 
c  Velocity[X]                                      0.32120E+01 
c  Velocity[Y]                                      0.46702E+01 
c  Velocity[Z]                                      0.60301E+01 
c  Pressure     0.64258E-01     458   0.51384E-01   0.13919E+00 0.21219E+01 
c  k            0.12478E+00      19   0.10673E-03   0.14202E-02 0.28078E+02 
c  epsilon      0.15312E+04      17   0.10006E-02   0.35467E+07 0.17527E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.2663e-06                             1
a  epsilon                 -1.7822                             3
a  Local Time Step      4.2274e-08                        278172


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6628          14.464          1.0952         0.17497
v  Velocity[Y]             -19.108          17.445          0.5795         0.42136
v  Velocity[Z]             -29.601          21.345        -0.49116      -0.0017553
v  ǁVelocityǁ            0.0025797          32.884          3.3661          3.5965
v  Pressure                 -38063           86844           54693           46081
v  k                    2.8862e-07          3.2389        0.029902        0.021886
v  epsilon              0.00020135      5.8812e+05          571.84          19.857
v  TurbVisc             1.8869e-12          0.2163      0.00092442        0.013401
v  CourantNb             0.0055685          7150.7          22.374          4.0406
v  FourierNb              0.022423      2.3655e+05          21.816         0.29064
v  total_pressure       4.6194e+05      5.8684e+05      5.5469e+05      5.4608e+05
v  Local Time Step           0.001        0.025942       0.0010087       0.0010407


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44928      2.4225e+05          44.191          4.3312


 TIME FOR THE TIME STEP              329:        0.74472E+02

===============================================================


 INSTANT    0.330000000E+01   TIME STEP NUMBER             330
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.988956365E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156439003E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30268E+02 0.45321E+01
   Friction velocity        uet   :  0.21936E-01 0.16515E+02
   Friction velocity        uk    :  0.21563E-01 0.16515E+02
   Dimensionless distance   yplus :  0.11204E-02 0.12231E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6985
   Nb of faces within the viscous sub-layer     :      17607
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76656E+01      41   0.55628E-01   0.13571E+02 0.30663E+02 
c  Velocity[X]                                      0.31617E+01 
c  Velocity[Y]                                      0.45249E+01 
c  Velocity[Z]                                      0.58844E+01 
c  Pressure     0.63441E-01     662   0.50145E-01   0.13721E+00 0.20612E+01 
c  k            0.12483E+00      23   0.98752E-04   0.12148E-02 0.25906E+02 
c  epsilon      0.15261E+04      12   0.74651E-03   0.19057E+07 0.13005E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.7249e-06                             1
a  epsilon                  -4.439                             2
a  Local Time Step      4.2275e-08                        278264


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.7611          14.357          1.0942         0.17485
v  Velocity[Y]             -20.277          17.583         0.58094         0.42124
v  Velocity[Z]             -27.792          21.542        -0.48663      -0.0017002
v  ǁVelocityǁ            0.0019494          31.424          3.3666          3.5992
v  Pressure                 -37642           86854           54697           46095
v  k                    3.3552e-07          3.3228        0.029758        0.021931
v  epsilon              0.00022668      5.8727e+05          565.21          19.822
v  TurbVisc             1.9271e-12          0.2163      0.00092851         0.01344
v  CourantNb              0.010023            7593          22.356          4.0452
v  FourierNb              0.022434      2.3655e+05          21.816         0.29075
v  total_pressure       4.6236e+05      5.8685e+05       5.547e+05       5.461e+05
v  Local Time Step           0.001        0.027888       0.0010085       0.0010409


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47579      2.4157e+05          44.171           4.336


 TIME FOR THE TIME STEP              330:        0.79381E+02

===============================================================


 INSTANT    0.331000000E+01   TIME STEP NUMBER             331
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.455029804E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156422202E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28881E+02 0.45268E+01
   Friction velocity        uet   :  0.24863E-01 0.16069E+02
   Friction velocity        uk    :  0.24498E-01 0.16069E+02
   Dimensionless distance   yplus :  0.78105E-03 0.12211E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6982
   Nb of faces within the viscous sub-layer     :      17623
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76676E+01      40   0.57021E-01   0.13448E+02 0.30514E+02 
c  Velocity[X]                                      0.30510E+01 
c  Velocity[Y]                                      0.43682E+01 
c  Velocity[Z]                                      0.60283E+01 
c  Pressure     0.62630E-01     567   0.49354E-01   0.13498E+00 0.21625E+01 
c  k            0.12488E+00      19   0.11377E-03   0.17433E-02 0.31111E+02 
c  epsilon      0.15302E+04      18   0.88432E-03   0.30852E+07 0.16413E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001451                             2
a  epsilon                 -0.8903                             4
a  Local Time Step      4.2274e-08                        278359


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.9396          15.703          1.0933         0.17487
v  Velocity[Y]             -19.619          18.184         0.58075         0.42134
v  Velocity[Z]             -31.988          21.827        -0.48182       -0.001631
v  ǁVelocityǁ            0.0023189          36.202          3.3654          3.6018
v  Pressure                 -37201           86884           54698           46115
v  k                    4.0115e-07           3.288        0.029846        0.021979
v  epsilon              0.00026439      5.8577e+05          568.85          19.842
v  TurbVisc               1.91e-12          0.2163       0.0009324        0.013475
v  CourantNb             0.0017731          7698.4          22.324          4.0494
v  FourierNb              0.022445      2.3655e+05          21.816         0.29072
v  total_pressure        4.628e+05      5.8688e+05       5.547e+05      5.4612e+05
v  Local Time Step           0.001        0.026749       0.0010083        0.001041


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50212      2.4119e+05           44.14          4.3401


 TIME FOR THE TIME STEP              331:        0.81393E+02

===============================================================


 INSTANT    0.332000000E+01   TIME STEP NUMBER             332
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.510823324E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156410876E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30014E+02 0.45254E+01
   Friction velocity        uet   :  0.14491E-01 0.15751E+02
   Friction velocity        uk    :  0.14454E-01 0.15751E+02
   Dimensionless distance   yplus :  0.76260E-03 0.12219E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6968
   Nb of faces within the viscous sub-layer     :      17619
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76707E+01      38   0.56858E-01   0.13597E+02 0.30681E+02 
c  Velocity[X]                                      0.30046E+01 
c  Velocity[Y]                                      0.46101E+01 
c  Velocity[Z]                                      0.59822E+01 
c  Pressure     0.61159E-01     535   0.47849E-01   0.13154E+00 0.22301E+01 
c  k            0.12493E+00      17   0.11339E-03   0.19170E-02 0.32679E+02 
c  epsilon      0.15254E+04      14   0.61825E-03   0.22601E+07 0.14233E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00036402                             2
a  epsilon                  -8.063                             3
a  Local Time Step      4.2274e-08                        278400


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6402          13.798          1.0929         0.17496
v  Velocity[Y]             -20.719          18.003         0.57832         0.42138
v  Velocity[Z]             -26.714          21.764        -0.47853      -0.0016864
v  ǁVelocityǁ             0.001538          30.469          3.3643          3.6041
v  Pressure                 -36760           86947           54697           46144
v  k                    4.8404e-07          3.2668        0.029663        0.022024
v  epsilon              0.00030558      5.8821e+05          561.02          19.828
v  TurbVisc              1.912e-12          0.2163      0.00093605        0.013508
v  CourantNb               0.01297          8290.9           22.29          4.0529
v  FourierNb              0.022454      2.3655e+05          21.816         0.29071
v  total_pressure       4.6324e+05      5.8695e+05       5.547e+05      5.4614e+05
v  Local Time Step           0.001        0.029424       0.0010082        0.001041


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68089       2.416e+05          44.106          4.3436


 TIME FOR THE TIME STEP              332:        0.74764E+02

===============================================================


 INSTANT    0.333000000E+01   TIME STEP NUMBER             333
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.130067127E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156395010E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26519E+02 0.41065E+01
   Friction velocity        uet   :  0.25361E-01 0.16599E+02
   Friction velocity        uk    :  0.25342E-01 0.16599E+02
   Dimensionless distance   yplus :  0.20794E-02 0.12225E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6966
   Nb of faces within the viscous sub-layer     :      17622
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76735E+01      38   0.56832E-01   0.13906E+02 0.30992E+02 
c  Velocity[X]                                      0.30837E+01 
c  Velocity[Y]                                      0.47787E+01 
c  Velocity[Z]                                      0.60431E+01 
c  Pressure     0.60120E-01     941   0.47113E-01   0.12918E+00 0.31066E+01 
c  k            0.12496E+00      17   0.10755E-03   0.18070E-02 0.31660E+02 
c  epsilon      0.15150E+04      16   0.36807E-03   0.18062E+07 0.12772E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.6365e-05                             1
a  epsilon                 -95.305                             3
a  Local Time Step      4.2274e-08                        278435


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.7719          16.129          1.0928         0.17482
v  Velocity[Y]             -18.599          18.124         0.57486         0.42149
v  Velocity[Z]             -33.256          21.654        -0.47561      -0.0020049
v  ǁVelocityǁ           0.00044382          37.548          3.3639          3.6065
v  Pressure                 -36176           87110           54778           46262
v  k                    5.8745e-07          3.2987        0.029632        0.022068
v  epsilon              0.00035908      4.6421e+05          554.32           19.82
v  TurbVisc              1.923e-12          0.2163      0.00093848        0.013538
v  CourantNb              0.026116          7668.1          22.261          4.0561
v  FourierNb              0.022464      2.3655e+05          21.816          0.2908
v  total_pressure       4.6382e+05      5.8711e+05      5.5478e+05      5.4626e+05
v  Local Time Step           0.001        0.032367       0.0010082       0.0010411


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59052      2.4247e+05          44.078          4.3469


 TIME FOR THE TIME STEP              333:        0.94333E+02

===============================================================


 INSTANT    0.334000000E+01   TIME STEP NUMBER             334
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.405691679E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156424562E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28943E+02 0.41098E+01
   Friction velocity        uet   :  0.23117E-01 0.16375E+02
   Friction velocity        uk    :  0.23097E-01 0.16375E+02
   Dimensionless distance   yplus :  0.20895E-02 0.12284E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6986
   Nb of faces within the viscous sub-layer     :      17637
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76794E+01      37   0.57223E-01   0.14019E+02 0.31108E+02 
c  Velocity[X]                                      0.30639E+01 
c  Velocity[Y]                                      0.48910E+01 
c  Velocity[Z]                                      0.60640E+01 
c  Pressure     0.59512E-01     558   0.46148E-01   0.12754E+00 0.23471E+01 
c  k            0.12502E+00      16   0.10969E-03   0.16384E-02 0.30159E+02 
c  epsilon      0.15171E+04      12   0.31447E-03   0.12589E+07 0.10664E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015544                             2
a  epsilon                 -5.7759                             1
a  Local Time Step      4.2274e-08                        278492


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.0257          13.505          1.0909         0.17447
v  Velocity[Y]             -19.339          17.554          0.5713         0.42141
v  Velocity[Z]             -26.537          22.484        -0.47348      -0.0023768
v  ǁVelocityǁ           0.00049882          30.136          3.3631          3.6084
v  Pressure                 -35528           87165           54759           46298
v  k                    6.3127e-07          3.2254        0.029559        0.022111
v  epsilon              0.00040708      4.6934e+05          554.19          19.813
v  TurbVisc             1.9155e-12          0.2163      0.00094124        0.013565
v  CourantNb            0.00090665          8115.4          22.217          4.0594
v  FourierNb              0.022472      2.3655e+05          21.816         0.29088
v  total_pressure       4.6447e+05      5.8717e+05      5.5476e+05       5.463e+05
v  Local Time Step           0.001        0.035603       0.0010082       0.0010418


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56118      2.4154e+05          44.034          4.3503


 TIME FOR THE TIME STEP              334:        0.72820E+02

===============================================================


 INSTANT    0.335000000E+01   TIME STEP NUMBER             335
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.767468890E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156479715E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23743E+02 0.41031E+01
   Friction velocity        uet   :  0.17763E-01 0.16010E+02
   Friction velocity        uk    :  0.17761E-01 0.16010E+02
   Dimensionless distance   yplus :  0.19824E-02 0.12242E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7004
   Nb of faces within the viscous sub-layer     :      17645
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76827E+01      38   0.57972E-01   0.14266E+02 0.31309E+02 
c  Velocity[X]                                      0.29942E+01 
c  Velocity[Y]                                      0.50777E+01 
c  Velocity[Z]                                      0.61944E+01 
c  Pressure     0.59542E-01     593   0.46546E-01   0.12730E+00 0.24929E+01 
c  k            0.12505E+00      16   0.11564E-03   0.18909E-02 0.32332E+02 
c  epsilon      0.15229E+04      25   0.95099E-03   0.42684E+07 0.19396E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002135                             6
a  epsilon                 -81.796                             6
a  Local Time Step      4.2274e-08                        278514


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.1663          15.934          1.0894         0.17412
v  Velocity[Y]             -18.839          17.974         0.56763         0.42143
v  Velocity[Z]             -33.163          21.345        -0.47207      -0.0027982
v  ǁVelocityǁ            0.0010321          37.323          3.3646            3.61
v  Pressure                 -34737           87232           54721           46324
v  k                    8.2845e-07          3.2951         0.02958        0.022153
v  epsilon              0.00047009      4.6258e+05          555.31          19.851
v  TurbVisc             1.9399e-12          0.2163      0.00094401         0.01359
v  CourantNb             0.0041403          7521.5           22.17          4.0626
v  FourierNb              0.022478      2.3655e+05          21.816         0.29105
v  total_pressure       4.6526e+05      5.8723e+05      5.5472e+05      5.4632e+05
v  Local Time Step           0.001        0.039164       0.0010082       0.0010424


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51242      2.4148e+05          43.987          4.3536


 TIME FOR THE TIME STEP              335:        0.93557E+02

===============================================================


 INSTANT    0.336000000E+01   TIME STEP NUMBER             336
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.986010509E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156531486E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29463E+02 0.41036E+01
   Friction velocity        uet   :  0.19076E-01 0.18975E+02
   Friction velocity        uk    :  0.19069E-01 0.18975E+02
   Dimensionless distance   yplus :  0.24212E-02 0.12466E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7016
   Nb of faces within the viscous sub-layer     :      17645
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76858E+01      41   0.58390E-01   0.14978E+02 0.32146E+02 
c  Velocity[X]                                      0.31554E+01 
c  Velocity[Y]                                      0.57630E+01 
c  Velocity[Z]                                      0.60601E+01 
c  Pressure     0.60917E-01    1218   0.46919E-01   0.12980E+00 0.69266E+01 
c  k            0.12510E+00      15   0.12741E-03   0.17654E-02 0.31267E+02 
c  epsilon      0.15235E+04      19   0.68494E-03   0.22035E+07 0.14099E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -6.319e-05                             2
a  epsilon                 -5.2678                             4
a  Local Time Step      4.2274e-08                        278567


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.7099          14.504          1.0869         0.17392
v  Velocity[Y]             -20.656           17.16         0.56463         0.42126
v  Velocity[Z]             -28.909          21.481        -0.47124       -0.002378
v  ǁVelocityǁ           0.00092617          32.749          3.3665          3.6103
v  Pressure                 -34346           86790           54197           45959
v  k                     6.241e-07          3.4536        0.029587        0.022188
v  epsilon              0.00054382      4.6801e+05          552.94          19.874
v  TurbVisc             1.9375e-12          0.2163      0.00094646        0.013612
v  CourantNb             0.0087954          8131.4          22.173          4.0654
v  FourierNb              0.022484      2.3655e+05          21.817         0.29107
v  total_pressure       4.6565e+05      5.8679e+05       5.542e+05      5.4596e+05
v  Local Time Step           0.001         0.04308       0.0010082       0.0010422


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51208      2.4092e+05          43.989          4.3565


 TIME FOR THE TIME STEP              336:        0.11105E+03

===============================================================


 INSTANT    0.337000000E+01   TIME STEP NUMBER             337
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.184119607E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444805E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25271E+02 0.40903E+01
   Friction velocity        uet   :  0.20389E-01 0.17625E+02
   Friction velocity        uk    :  0.20508E-01 0.17625E+02
   Dimensionless distance   yplus :  0.22489E-02 0.12245E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7042
   Nb of faces within the viscous sub-layer     :      17667
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76829E+01      38   0.58555E-01   0.15283E+02 0.32414E+02 
c  Velocity[X]                                      0.32275E+01 
c  Velocity[Y]                                      0.62036E+01 
c  Velocity[Z]                                      0.58523E+01 
c  Pressure     0.59737E-01     680   0.45958E-01   0.12714E+00 0.25129E+01 
c  k            0.12512E+00      16   0.13183E-03   0.15773E-02 0.29508E+02 
c  epsilon      0.15298E+04      18   0.37498E-03   0.92208E+06 0.90761E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016265                             2
a  epsilon                 -3.8281                             3
a  Local Time Step      4.2274e-08                        278584


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.7581          16.346           1.085         0.17377
v  Velocity[Y]             -18.393          17.828         0.56342         0.42123
v  Velocity[Z]             -33.873          21.422        -0.47049      -0.0021135
v  ǁVelocityǁ            0.0014159          38.147          3.3706          3.6103
v  Pressure                 -33550           86862           54179           45991
v  k                    8.3437e-07          3.5363        0.029623        0.022215
v  epsilon              0.00060939      4.6353e+05          554.97          19.898
v  TurbVisc             1.9596e-12          0.2163       0.0009481        0.013632
v  CourantNb             0.0012533          7997.6          22.165          4.0671
v  FourierNb              0.022488      2.3655e+05          21.816         0.29114
v  total_pressure       4.6645e+05      5.8686e+05      5.5418e+05      5.4599e+05
v  Local Time Step           0.001        0.047088       0.0010083       0.0010428


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55012      2.4132e+05          43.981          4.3582


 TIME FOR THE TIME STEP              337:        0.86958E+02

===============================================================


 INSTANT    0.338000000E+01   TIME STEP NUMBER             338
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.359839721E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156447342E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29973E+02 0.41098E+01
   Friction velocity        uet   :  0.29344E-01 0.15196E+02
   Friction velocity        uk    :  0.28114E-01 0.15196E+02
   Dimensionless distance   yplus :  0.18763E-02 0.12528E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7062
   Nb of faces within the viscous sub-layer     :      17678
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76814E+01      42   0.58434E-01   0.15208E+02 0.32375E+02 
c  Velocity[X]                                      0.31639E+01 
c  Velocity[Y]                                      0.62698E+01 
c  Velocity[Z]                                      0.57743E+01 
c  Pressure     0.61260E-01     659   0.46758E-01   0.13029E+00 0.25038E+01 
c  k            0.12517E+00      15   0.10290E-03   0.14701E-02 0.28492E+02 
c  epsilon      0.15328E+04      11   0.28885E-03   0.10150E+07 0.95016E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.0881e-05                             1
a  epsilon                 -5.2494                             3
a  Local Time Step      4.2275e-08                        278551


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.9657          14.949          1.0821         0.17352
v  Velocity[Y]             -19.272          17.731         0.56374         0.42117
v  Velocity[Z]             -30.144          21.512        -0.47066      -0.0019395
v  ǁVelocityǁ            0.0018735           34.06          3.3766          3.6101
v  Pressure                 -32763           86935           54163           46034
v  k                     8.532e-07          3.6825         0.02966        0.022239
v  epsilon              0.00067642      4.6829e+05          555.89          19.941
v  TurbVisc             1.9767e-12          0.2163      0.00095023        0.013649
v  CourantNb             0.0065737          7975.1          22.173          4.0693
v  FourierNb              0.022491      2.3655e+05          21.817         0.29115
v  total_pressure       4.6724e+05      5.8694e+05      5.5416e+05      5.4603e+05
v  Local Time Step           0.001        0.048593       0.0010084       0.0010429


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74095       2.406e+05           43.99          4.3605


 TIME FOR THE TIME STEP              338:        0.78783E+02

===============================================================


 INSTANT    0.339000000E+01   TIME STEP NUMBER             339
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.373546021E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156438379E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26320E+02 0.40920E+01
   Friction velocity        uet   :  0.21963E-01 0.14357E+02
   Friction velocity        uk    :  0.21958E-01 0.14357E+02
   Dimensionless distance   yplus :  0.17139E-02 0.12235E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7079
   Nb of faces within the viscous sub-layer     :      17643
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76787E+01      44   0.58371E-01   0.15243E+02 0.32418E+02 
c  Velocity[X]                                      0.32077E+01 
c  Velocity[Y]                                      0.64645E+01 
c  Velocity[Z]                                      0.55713E+01 
c  Pressure     0.61130E-01     581   0.46998E-01   0.13009E+00 0.24046E+01 
c  k            0.12522E+00      15   0.12629E-03   0.16868E-02 0.30493E+02 
c  epsilon      0.15406E+04      10   0.22933E-03   0.54363E+06 0.69462E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.5576e-05                             2
a  epsilon                 -3.2434                             3
a  Local Time Step      4.2275e-08                        278566


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5882          15.716          1.0801         0.17321
v  Velocity[Y]             -18.313          18.177         0.56485         0.42124
v  Velocity[Z]             -33.033           21.99        -0.47015      -0.0018281
v  ǁVelocityǁ            0.0032678          37.069           3.384          3.6097
v  Pressure                 -32157           87005           54146           46072
v  k                    8.7044e-07          3.5207        0.029777        0.022265
v  epsilon              0.00075211      4.6301e+05          557.14          20.023
v  TurbVisc             2.0391e-12          0.2163      0.00095325        0.013664
v  CourantNb            0.00098874          8058.1          22.211          4.0722
v  FourierNb              0.022493      2.3655e+05          21.818         0.29115
v  total_pressure       4.6784e+05        5.87e+05      5.5415e+05      5.4607e+05
v  Local Time Step           0.001        0.040971       0.0010083       0.0010421


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71157      2.4097e+05          44.029          4.3633


 TIME FOR THE TIME STEP              339:        0.75277E+02

===============================================================


 INSTANT    0.340000000E+01   TIME STEP NUMBER             340
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.314755352E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156427785E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30644E+02 0.40825E+01
   Friction velocity        uet   :  0.28048E-01 0.13611E+02
   Friction velocity        uk    :  0.27929E-01 0.13611E+02
   Dimensionless distance   yplus :  0.15237E-02 0.12524E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7095
   Nb of faces within the viscous sub-layer     :      17621
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76757E+01      37   0.57539E-01   0.15252E+02 0.32435E+02 
c  Velocity[X]                                      0.30836E+01 
c  Velocity[Y]                                      0.67159E+01 
c  Velocity[Z]                                      0.54524E+01 
c  Pressure     0.63418E-01     592   0.47886E-01   0.13509E+00 0.21585E+01 
c  k            0.12527E+00      14   0.14854E-03   0.19072E-02 0.32350E+02 
c  epsilon      0.15358E+04      12   0.36702E-03   0.89377E+06 0.88913E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -3.159e-05                             2
a  epsilon                 -4.9307                             3
a  Local Time Step      4.2275e-08                        278553


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6047          14.789          1.0794         0.17307
v  Velocity[Y]             -19.666          17.782         0.56708         0.42122
v  Velocity[Z]             -30.079          21.733        -0.47063      -0.0017404
v  ǁVelocityǁ            0.0035379          33.903          3.3934          3.6094
v  Pressure                 -31579           87071           54133           46107
v  k                    8.5916e-07           3.618        0.029944        0.022286
v  epsilon              0.00078069      4.6197e+05          561.33          20.092
v  TurbVisc             2.0545e-12          0.2163      0.00095684        0.013677
v  CourantNb              0.001724          8168.9          22.255          4.0751
v  FourierNb              0.022495      2.3655e+05          21.819         0.29119
v  total_pressure       4.6842e+05      5.8707e+05      5.5413e+05      5.4611e+05
v  Local Time Step           0.001        0.032619       0.0010084       0.0010423


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63076      2.4064e+05          44.074          4.3662


 TIME FOR THE TIME STEP              340:        0.74702E+02

===============================================================


 INSTANT    0.341000000E+01   TIME STEP NUMBER             341
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.180680487E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156424767E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26428E+02 0.40814E+01
   Friction velocity        uet   :  0.24894E-01 0.14123E+02
   Friction velocity        uk    :  0.24867E-01 0.14123E+02
   Dimensionless distance   yplus :  0.15095E-02 0.12222E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7136
   Nb of faces within the viscous sub-layer     :      17567
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76729E+01      36   0.58709E-01   0.14677E+02 0.31813E+02 
c  Velocity[X]                                      0.30829E+01 
c  Velocity[Y]                                      0.63313E+01 
c  Velocity[Z]                                      0.52632E+01 
c  Pressure     0.62604E-01     640   0.47991E-01   0.13356E+00 0.20940E+01 
c  k            0.12531E+00      16   0.13864E-03   0.19715E-02 0.32905E+02 
c  epsilon      0.15393E+04      13   0.29581E-03   0.10879E+07 0.97899E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.5095e-05                             3
a  epsilon                 -4.3801                             4
a  Local Time Step      4.2275e-08                        278562


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.8069            14.7           1.079         0.17285
v  Velocity[Y]             -18.068          18.239         0.57098         0.42114
v  Velocity[Z]             -31.635          21.591        -0.47093      -0.0016892
v  ǁVelocityǁ            0.0048871          35.313          3.4027          3.6087
v  Pressure                 -31067           87129           54123           46141
v  k                    8.6995e-07          3.4595        0.030135        0.022308
v  epsilon              0.00085969      4.6384e+05          564.26          20.181
v  TurbVisc             2.0229e-12          0.2163      0.00095942        0.013688
v  CourantNb              0.018452          8171.7          22.331          4.0781
v  FourierNb              0.022496      2.3655e+05          21.819         0.29143
v  total_pressure       4.6893e+05      5.8713e+05      5.5412e+05      5.4614e+05
v  Local Time Step           0.001         0.03588       0.0010086       0.0010431


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41691      2.4028e+05           44.15          4.3695


 TIME FOR THE TIME STEP              341:        0.83028E+02

===============================================================


 INSTANT    0.342000000E+01   TIME STEP NUMBER             342
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.910236362E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156411487E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30055E+02 0.40782E+01
   Friction velocity        uet   :  0.32699E-01 0.13407E+02
   Friction velocity        uk    :  0.35815E-01 0.13407E+02
   Dimensionless distance   yplus :  0.17108E-02 0.12555E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7154
   Nb of faces within the viscous sub-layer     :      17561
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76693E+01      36   0.60394E-01   0.14349E+02 0.31466E+02 
c  Velocity[X]                                      0.30452E+01 
c  Velocity[Y]                                      0.61493E+01 
c  Velocity[Z]                                      0.51540E+01 
c  Pressure     0.63324E-01     585   0.48370E-01   0.13544E+00 0.17892E+01 
c  k            0.12537E+00      16   0.17410E-03   0.18405E-02 0.31780E+02 
c  epsilon      0.15387E+04      12   0.31309E-03   0.98572E+06 0.93404E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.0355e-05                             2
a  epsilon                 -4.9458                             4
a  Local Time Step      4.2275e-08                        278551


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3957          14.644          1.0796         0.17276
v  Velocity[Y]             -19.277          17.877          0.5735           0.421
v  Velocity[Z]              -30.37          21.617         -0.4726      -0.0017277
v  ǁVelocityǁ            0.0061409          34.102          3.4125           3.608
v  Pressure                 -30751           87189           54114           46173
v  k                    8.7387e-07          3.4515        0.030147        0.022326
v  epsilon              0.00088577      4.5693e+05          562.88          20.238
v  TurbVisc             2.0421e-12          0.2163      0.00096211        0.013699
v  CourantNb              0.041581            7990          22.393          4.0809
v  FourierNb              0.022496      2.3655e+05          21.819         0.29156
v  total_pressure       4.6925e+05      5.8719e+05      5.5411e+05      5.4617e+05
v  Local Time Step           0.001        0.039468       0.0010087       0.0010443


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62017      2.4025e+05          44.212          4.3725


 TIME FOR THE TIME STEP              342:        0.76812E+02

===============================================================


 INSTANT    0.343000000E+01   TIME STEP NUMBER             343
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.159753230E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156429945E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28963E+02 0.40804E+01
   Friction velocity        uet   :  0.23123E-01 0.14191E+02
   Friction velocity        uk    :  0.22789E-01 0.14191E+02
   Dimensionless distance   yplus :  0.17207E-02 0.12287E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7193
   Nb of faces within the viscous sub-layer     :      17508
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76652E+01      44   0.59153E-01   0.13778E+02 0.30814E+02 
c  Velocity[X]                                      0.29630E+01 
c  Velocity[Y]                                      0.58900E+01 
c  Velocity[Z]                                      0.49253E+01 
c  Pressure     0.63260E-01     492   0.48866E-01   0.13573E+00 0.16404E+01 
c  k            0.12541E+00      15   0.16153E-03   0.17863E-02 0.31253E+02 
c  epsilon      0.15449E+04      12   0.39392E-03   0.10131E+07 0.94121E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001821                             4
a  epsilon                 -4.0193                             6
a  Local Time Step      4.2275e-08                        278581


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.1962          13.981           1.081         0.17268
v  Velocity[Y]             -17.889           17.99         0.57624          0.4205
v  Velocity[Z]             -29.704           22.04        -0.47422      -0.0017197
v  ǁVelocityǁ            0.0050668           33.13          3.4212          3.6068
v  Pressure                 -30449           87203           54109           46188
v  k                    8.8203e-07          3.4155        0.030338        0.022349
v  epsilon              0.00093918      4.5952e+05          568.09          20.339
v  TurbVisc              2.065e-12          0.2163      0.00096426        0.013708
v  CourantNb             0.0081288          8047.5          22.471          4.0838
v  FourierNb              0.022497      2.3655e+05          21.819         0.29154
v  total_pressure       4.6955e+05       5.872e+05      5.5411e+05      5.4619e+05
v  Local Time Step           0.001        0.043415       0.0010087       0.0010447


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61406      2.3992e+05           44.29          4.3753


 TIME FOR THE TIME STEP              343:        0.69084E+02

===============================================================


 INSTANT    0.344000000E+01   TIME STEP NUMBER             344
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.221625549E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156407509E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30050E+02 0.40731E+01
   Friction velocity        uet   :  0.24119E-01 0.12166E+02
   Friction velocity        uk    :  0.23867E-01 0.12166E+02
   Dimensionless distance   yplus :  0.15524E-02 0.12454E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7209
   Nb of faces within the viscous sub-layer     :      17481
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76613E+01      34   0.58201E-01   0.13522E+02 0.30561E+02 
c  Velocity[X]                                      0.28091E+01 
c  Velocity[Y]                                      0.59034E+01 
c  Velocity[Z]                                      0.48094E+01 
c  Pressure     0.62667E-01     461   0.49029E-01   0.13469E+00 0.15431E+01 
c  k            0.12547E+00      16   0.14071E-03   0.13130E-02 0.26764E+02 
c  epsilon      0.15500E+04      11   0.42833E-03   0.99649E+06 0.93142E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014541                             3
a  epsilon                 -5.0787                             7
a  Local Time Step      4.2275e-08                        278610


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3998          14.283          1.0825         0.17269
v  Velocity[Y]              -19.09          17.925         0.57971         0.42011
v  Velocity[Z]             -29.763          21.766        -0.47867      -0.0017517
v  ǁVelocityǁ            0.0027356          33.391          3.4304          3.6057
v  Pressure                 -30287           87215           54108           46203
v  k                    8.7462e-07          3.4042        0.030517        0.022367
v  epsilon               0.0009922      4.6114e+05          573.14          20.411
v  TurbVisc             2.0602e-12          0.2163      0.00096652        0.013716
v  CourantNb             0.0055676            7889          22.528          4.0855
v  FourierNb              0.022497      2.3655e+05          21.819         0.29169
v  total_pressure       4.6971e+05      5.8721e+05      5.5411e+05       5.462e+05
v  Local Time Step           0.001        0.047757       0.0010089        0.001046


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59269      2.3953e+05          44.347          4.3772


 TIME FOR THE TIME STEP              344:        0.72576E+02

===============================================================


 INSTANT    0.345000000E+01   TIME STEP NUMBER             345
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.235214446E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156405782E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26953E+02 0.40545E+01
   Friction velocity        uet   :  0.21967E-01 0.11757E+02
   Friction velocity        uk    :  0.21877E-01 0.11757E+02
   Dimensionless distance   yplus :  0.14801E-02 0.12223E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7240
   Nb of faces within the viscous sub-layer     :      17431
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76569E+01      37   0.57331E-01   0.13236E+02 0.30233E+02 
c  Velocity[X]                                      0.27196E+01 
c  Velocity[Y]                                      0.58974E+01 
c  Velocity[Z]                                      0.46189E+01 
c  Pressure     0.62695E-01     365   0.49987E-01   0.13470E+00 0.15454E+01 
c  k            0.12552E+00      15   0.12702E-03   0.11724E-02 0.25265E+02 
c  epsilon      0.15569E+04      14   0.66608E-03   0.14224E+07 0.11057E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.7006e-05                             4
a  epsilon                 -4.1584                             7
a  Local Time Step      4.2275e-08                        278687


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.0053          13.849          1.0839          0.1728
v  Velocity[Y]             -17.829          18.411         0.58249          0.4198
v  Velocity[Z]             -29.146          22.697        -0.48354      -0.0019068
v  ǁVelocityǁ           0.00089064          32.432          3.4394          3.6047
v  Pressure                 -30153           87217           54102           46221
v  k                    8.5763e-07          3.4804        0.030638        0.022385
v  epsilon               0.0010459      4.5587e+05          576.96          20.485
v  TurbVisc             2.0422e-12          0.2163       0.0009682        0.013723
v  CourantNb              0.004993          8167.2          22.603          4.0874
v  FourierNb              0.022496      2.3655e+05          21.819         0.29175
v  total_pressure       4.6985e+05      5.8722e+05       5.541e+05      5.4622e+05
v  Local Time Step           0.001        0.052532        0.001009       0.0010461


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59413       2.399e+05          44.422          4.3792


 TIME FOR THE TIME STEP              345:        0.60138E+02

===============================================================


 INSTANT    0.346000000E+01   TIME STEP NUMBER             346
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.298091567E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156411328E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29532E+02 0.40675E+01
   Friction velocity        uet   :  0.24407E-01 0.94939E+01
   Friction velocity        uk    :  0.24401E-01 0.94939E+01
   Dimensionless distance   yplus :  0.12047E-02 0.12364E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7253
   Nb of faces within the viscous sub-layer     :      17395
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76529E+01      35   0.57980E-01   0.13169E+02 0.30171E+02 
c  Velocity[X]                                      0.26312E+01 
c  Velocity[Y]                                      0.57336E+01 
c  Velocity[Z]                                      0.48043E+01 
c  Pressure     0.62666E-01     492   0.50828E-01   0.13483E+00 0.15568E+01 
c  k            0.12556E+00      15   0.11648E-03   0.11105E-02 0.24556E+02 
c  epsilon      0.15605E+04      15   0.43650E-03   0.92699E+06 0.89110E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.6268e-05                             1
a  epsilon                  -5.362                             5
a  Local Time Step      4.2275e-08                        278665


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9389          14.185          1.0853         0.17303
v  Velocity[Y]             -19.033           18.82          0.5847         0.41956
v  Velocity[Z]             -29.555          21.534        -0.48931      -0.0021128
v  ǁVelocityǁ            0.0019132          33.171          3.4482          3.6038
v  Pressure                 -30144           87227           54100           46237
v  k                    8.5405e-07          3.6096        0.030793          0.0224
v  epsilon               0.0011288      4.5824e+05           581.5          20.538
v  TurbVisc             2.1166e-12          0.2163       0.0009694        0.013729
v  CourantNb            0.00044933          7911.5          22.667          4.0893
v  FourierNb              0.022496      2.3655e+05          21.818         0.29182
v  total_pressure       4.6986e+05      5.8723e+05       5.541e+05      5.4624e+05
v  Local Time Step           0.001        0.057786       0.0010091        0.001047


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51736      2.3985e+05          44.485          4.3811


 TIME FOR THE TIME STEP              346:        0.66164E+02

===============================================================


 INSTANT    0.347000000E+01   TIME STEP NUMBER             347
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.198516946E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156425634E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28196E+02 0.40939E+01
   Friction velocity        uet   :  0.28039E-01 0.12560E+02
   Friction velocity        uk    :  0.28021E-01 0.12560E+02
   Dimensionless distance   yplus :  0.16027E-02 0.12340E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7264
   Nb of faces within the viscous sub-layer     :      17377
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76497E+01      34   0.57309E-01   0.13149E+02 0.30102E+02 
c  Velocity[X]                                      0.25996E+01 
c  Velocity[Y]                                      0.58830E+01 
c  Velocity[Z]                                      0.46664E+01 
c  Pressure     0.64396E-01     397   0.52684E-01   0.13873E+00 0.15615E+01 
c  k            0.12558E+00      17   0.10563E-03   0.11287E-02 0.24709E+02 
c  epsilon      0.15710E+04      15   0.35762E-03   0.10908E+07 0.95868E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.1913e-05                             1
a  epsilon                 -4.2088                             6
a  Local Time Step      4.2275e-08                        278687


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9542          13.416          1.0856          0.1733
v  Velocity[Y]             -17.706          19.274         0.58614         0.41916
v  Velocity[Z]             -28.813          22.059        -0.49453      -0.0026452
v  ǁVelocityǁ            0.0053097          31.761          3.4557          3.6034
v  Pressure                 -30233           87198           54091           46250
v  k                    8.9768e-07          3.5958        0.030994        0.022413
v  epsilon               0.0012789       4.611e+05          589.71          20.602
v  TurbVisc             2.0905e-12          0.2163      0.00097132        0.013735
v  CourantNb             0.0028338          7770.1          22.738          4.0908
v  FourierNb              0.022494      2.3655e+05          21.819         0.29193
v  total_pressure       4.6977e+05       5.872e+05      5.5409e+05      5.4625e+05
v  Local Time Step           0.001        0.054382       0.0010091       0.0010469


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40602      2.4008e+05          44.556          4.3827


 TIME FOR THE TIME STEP              347:        0.72696E+02

===============================================================


 INSTANT    0.348000000E+01   TIME STEP NUMBER             348
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.169802899E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156467618E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28507E+02 0.40715E+01
   Friction velocity        uet   :  0.20392E-01 0.10319E+02
   Friction velocity        uk    :  0.20282E-01 0.10319E+02
   Dimensionless distance   yplus :  0.94930E-03 0.12322E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7271
   Nb of faces within the viscous sub-layer     :      17346
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76475E+01      38   0.55612E-01   0.13149E+02 0.30162E+02 
c  Velocity[X]                                      0.25587E+01 
c  Velocity[Y]                                      0.59050E+01 
c  Velocity[Z]                                      0.46850E+01 
c  Pressure     0.64040E-01     490   0.52642E-01   0.13811E+00 0.17217E+01 
c  k            0.12560E+00      15   0.10864E-03   0.11663E-02 0.25162E+02 
c  epsilon      0.15707E+04      11   0.27257E-03   0.95048E+06 0.89533E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.2247e-05                             1
a  epsilon                 -5.5091                             3
a  Local Time Step      4.2275e-08                        278667


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9392          14.087          1.0856         0.17354
v  Velocity[Y]             -19.005          19.094         0.58692         0.41892
v  Velocity[Z]             -29.797          21.851        -0.50043      -0.0033806
v  ǁVelocityǁ            0.0044871          33.106          3.4625          3.6034
v  Pressure                 -30408           87169           54074           46257
v  k                    1.0112e-06           3.729        0.030983        0.022425
v  epsilon              0.00084947      4.5985e+05           588.2          20.646
v  TurbVisc             2.1068e-12          0.2163      0.00097281         0.01374
v  CourantNb              0.025299          7626.7          22.797          4.0921
v  FourierNb              0.022491      2.3655e+05          21.818         0.29198
v  total_pressure       4.6959e+05      5.8717e+05      5.5407e+05      5.4626e+05
v  Local Time Step           0.001         0.05982       0.0010092       0.0010476


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56771      2.3989e+05          44.615          4.3841


 TIME FOR THE TIME STEP              348:        0.75254E+02

===============================================================


 INSTANT    0.349000000E+01   TIME STEP NUMBER             349
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.187969902E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156522964E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24655E+02 0.40675E+01
   Friction velocity        uet   :  0.30032E-01 0.11246E+02
   Friction velocity        uk    :  0.29452E-01 0.11246E+02
   Dimensionless distance   yplus :  0.13393E-02 0.12385E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7297
   Nb of faces within the viscous sub-layer     :      17335
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76468E+01      39   0.55979E-01   0.12749E+02 0.29700E+02 
c  Velocity[X]                                      0.24206E+01 
c  Velocity[Y]                                      0.53947E+01 
c  Velocity[Z]                                      0.49335E+01 
c  Pressure     0.63185E-01     568   0.51302E-01   0.13612E+00 0.17367E+01 
c  k            0.12559E+00      17   0.12156E-03   0.10719E-02 0.24084E+02 
c  epsilon      0.15798E+04      14   0.45268E-03   0.12792E+07 0.10324E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.9954e-05                             3
a  epsilon                 -4.0326                             9
a  Local Time Step      4.2275e-08                        278673


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9241          13.001          1.0857         0.17375
v  Velocity[Y]             -17.931          19.398         0.58774         0.41919
v  Velocity[Z]             -27.413          22.908        -0.50514      -0.0041698
v  ǁVelocityǁ             0.003649          30.179          3.4687          3.6038
v  Pressure                 -30609           87088           54040           46236
v  k                    4.2694e-07          3.4885        0.031148        0.022435
v  epsilon               0.0016328      4.5985e+05          593.97          20.674
v  TurbVisc             2.3295e-12          0.2163       0.0009745        0.013745
v  CourantNb              0.013429            7561          22.841          4.0939
v  FourierNb              0.022487      2.3655e+05          21.818         0.29205
v  total_pressure       4.6939e+05      5.8709e+05      5.5404e+05      5.4624e+05
v  Local Time Step           0.001        0.065802       0.0010092       0.0010479


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65939      2.4004e+05          44.659          4.3859


 TIME FOR THE TIME STEP              349:        0.77321E+02

===============================================================


 INSTANT    0.350000000E+01   TIME STEP NUMBER             350
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.392556662E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156587514E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27387E+02 0.40816E+01
   Friction velocity        uet   :  0.32070E-01 0.11282E+02
   Friction velocity        uk    :  0.37449E-01 0.11282E+02
   Dimensionless distance   yplus :  0.12148E-02 0.12445E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7283
   Nb of faces within the viscous sub-layer     :      17302
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76454E+01      37   0.56565E-01   0.11948E+02 0.28751E+02 
c  Velocity[X]                                      0.23916E+01 
c  Velocity[Y]                                      0.47210E+01 
c  Velocity[Z]                                      0.48358E+01 
c  Pressure     0.61753E-01     813   0.48176E-01   0.13271E+00 0.72603E+01 
c  k            0.12560E+00      18   0.10316E-03   0.10406E-02 0.23790E+02 
c  epsilon      0.15810E+04      14   0.37934E-03   0.83208E+06 0.83318E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.5621e-05                             1
a  epsilon                 -5.6619                             4
a  Local Time Step      4.2275e-08                        278620


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.8748          12.642          1.0859         0.17387
v  Velocity[Y]             -19.352          18.779         0.58801         0.41965
v  Velocity[Z]             -25.222          21.941        -0.50943      -0.0040481
v  ǁVelocityǁ            0.0055256          28.511          3.4734          3.6032
v  Pressure                 -31204           86572           53556           45839
v  k                    3.0319e-07          3.5175        0.031201        0.022445
v  epsilon                6.87e-06      4.5912e+05          596.05           20.71
v  TurbVisc             1.8664e-12          0.2163      0.00097689        0.013749
v  CourantNb              0.021083          7391.7          22.896          4.0955
v  FourierNb              0.022482      2.3655e+05          21.818         0.29214
v  total_pressure        4.688e+05      5.8657e+05      5.5356e+05      5.4584e+05
v  Local Time Step           0.001        0.072382       0.0010093       0.0010484


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65802      2.3969e+05          44.714          4.3877


 TIME FOR THE TIME STEP              350:        0.87043E+02

===============================================================


 INSTANT    0.351000000E+01   TIME STEP NUMBER             351
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.128321237E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156551872E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22840E+02 0.41048E+01
   Friction velocity        uet   :  0.24357E-01 0.12655E+02
   Friction velocity        uk    :  0.24057E-01 0.12655E+02
   Dimensionless distance   yplus :  0.16147E-02 0.12499E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7298
   Nb of faces within the viscous sub-layer     :      17274
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76387E+01      37   0.55827E-01   0.10713E+02 0.27232E+02 
c  Velocity[X]                                      0.22812E+01 
c  Velocity[Y]                                      0.39722E+01 
c  Velocity[Z]                                      0.44596E+01 
c  Pressure     0.58170E-01     469   0.44424E-01   0.12479E+00 0.15489E+01 
c  k            0.12559E+00      16   0.23301E-03   0.12283E-02 0.25868E+02 
c  epsilon      0.15835E+04      12   0.25603E-03   0.96821E+06 0.89632E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.5357e-05                             1
a  epsilon                  -4.382                             3
a  Local Time Step      4.2275e-08                        278618


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9269          12.163          1.0844         0.17409
v  Velocity[Y]              -17.88          18.809         0.58848         0.42028
v  Velocity[Z]             -26.845          21.916        -0.51187      -0.0039757
v  ǁVelocityǁ            0.0049796          29.448          3.4757          3.6028
v  Pressure                 -31282           86547           53540           45845
v  k                    8.5157e-07          3.3521        0.031301        0.022451
v  epsilon               0.0015046      4.6499e+05          598.68          20.748
v  TurbVisc             2.0197e-12          0.2163      0.00097888        0.013752
v  CourantNb             0.0070423            7118          22.946          4.0963
v  FourierNb              0.022476      2.3655e+05          21.819         0.29215
v  total_pressure       4.6872e+05      5.8655e+05      5.5354e+05      5.4585e+05
v  Local Time Step           0.001        0.079621       0.0010093       0.0010491


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50508      2.4081e+05          44.765          4.3884


 TIME FOR THE TIME STEP              351:        0.72007E+02

===============================================================


 INSTANT    0.352000000E+01   TIME STEP NUMBER             352
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.225279753E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156530252E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26389E+02 0.40864E+01
   Friction velocity        uet   :  0.31643E-01 0.11567E+02
   Friction velocity        uk    :  0.31808E-01 0.11567E+02
   Dimensionless distance   yplus :  0.14287E-02 0.12534E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7290
   Nb of faces within the viscous sub-layer     :      17252
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76370E+01      37   0.54999E-01   0.99361E+01 0.26230E+02 
c  Velocity[X]                                      0.21286E+01 
c  Velocity[Y]                                      0.33889E+01 
c  Velocity[Z]                                      0.44185E+01 
c  Pressure     0.52920E-01     449   0.39564E-01   0.11348E+00 0.13071E+01 
c  k            0.12559E+00      15   0.19446E-03   0.90181E-03 0.22113E+02 
c  epsilon      0.15828E+04      11   0.19175E-03   0.43061E+06 0.59912E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.1967e-05                             1
a  epsilon                 -5.4386                             4
a  Local Time Step      4.2275e-08                        278624


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9495          12.881          1.0837          0.1743
v  Velocity[Y]             -18.965           17.72         0.58821         0.42067
v  Velocity[Z]              -27.36          21.951        -0.51415      -0.0038411
v  ǁVelocityǁ            0.0047132          30.197          3.4764          3.6028
v  Pressure                 -31262           86542           53529           45845
v  k                    8.3746e-07          3.3868        0.031278        0.022451
v  epsilon               0.0014597      4.5775e+05          596.63          20.733
v  TurbVisc             1.9651e-12          0.2163      0.00098112        0.013755
v  CourantNb             0.0042005          7205.1          22.968          4.0966
v  FourierNb              0.022469      2.3655e+05          21.819         0.29221
v  total_pressure       4.6874e+05      5.8654e+05      5.5353e+05      5.4584e+05
v  Local Time Step           0.001        0.087583       0.0010094       0.0010496


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61237       2.402e+05          44.787          4.3888


 TIME FOR THE TIME STEP              352:        0.69028E+02

===============================================================


 INSTANT    0.353000000E+01   TIME STEP NUMBER             353
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.245447488E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156513708E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22896E+02 0.40818E+01
   Friction velocity        uet   :  0.23427E-01 0.12863E+02
   Friction velocity        uk    :  0.23087E-01 0.12863E+02
   Dimensionless distance   yplus :  0.16413E-02 0.12558E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7285
   Nb of faces within the viscous sub-layer     :      17246
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76356E+01      36   0.53518E-01   0.93034E+01 0.25374E+02 
c  Velocity[X]                                      0.19896E+01 
c  Velocity[Y]                                      0.30327E+01 
c  Velocity[Z]                                      0.42811E+01 
c  Pressure     0.51152E-01     455   0.38237E-01   0.10977E+00 0.12290E+01 
c  k            0.12559E+00      16   0.13890E-03   0.97462E-03 0.23009E+02 
c  epsilon      0.15818E+04      14   0.22506E-03   0.35471E+06 0.54337E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017001                             2
a  epsilon                 -4.4941                             4
a  Local Time Step      4.2275e-08                        278633


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9412          12.355          1.0822         0.17441
v  Velocity[Y]             -18.177          19.201         0.58773         0.42076
v  Velocity[Z]             -26.944          22.015        -0.51516      -0.0037732
v  ǁVelocityǁ            0.0017402          29.586          3.4758          3.6027
v  Pressure                 -31421           86489           53521           45833
v  k                    8.5096e-07          3.4461        0.031339        0.022454
v  epsilon               0.0014596      4.6353e+05          597.15          20.756
v  TurbVisc             1.9286e-12          0.2163      0.00098347        0.013757
v  CourantNb              0.010097          7282.6          22.975          4.0974
v  FourierNb              0.022461      2.3655e+05           21.82         0.29235
v  total_pressure       4.6858e+05      5.8649e+05      5.5352e+05      5.4583e+05
v  Local Time Step           0.001        0.096341       0.0010095       0.0010503


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56128      2.4011e+05          44.795          4.3898


 TIME FOR THE TIME STEP              353:        0.74184E+02

===============================================================


 INSTANT    0.354000000E+01   TIME STEP NUMBER             354
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.205414079E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156495141E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26774E+02 0.40742E+01
   Friction velocity        uet   :  0.29270E-01 0.14079E+02
   Friction velocity        uk    :  0.29110E-01 0.14079E+02
   Dimensionless distance   yplus :  0.17965E-02 0.12554E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7269
   Nb of faces within the viscous sub-layer     :      17226
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76347E+01      35   0.53255E-01   0.86479E+01 0.24474E+02 
c  Velocity[X]                                      0.18553E+01 
c  Velocity[Y]                                      0.27050E+01 
c  Velocity[Z]                                      0.40875E+01 
c  Pressure     0.48534E-01     475   0.35448E-01   0.10422E+00 0.10426E+01 
c  k            0.12559E+00      16   0.11208E-03   0.10218E-02 0.23513E+02 
c  epsilon      0.15796E+04      12   0.42807E-03   0.63188E+06 0.72541E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.1708e-05                             1
a  epsilon                 -5.5332                             4
a  Local Time Step      4.2275e-08                        278609


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9458          12.938          1.0816         0.17466
v  Velocity[Y]             -20.043           17.52         0.58685          0.4208
v  Velocity[Z]             -27.104          21.763        -0.51569      -0.0035906
v  ǁVelocityǁ            0.0035454          30.372          3.4754          3.6029
v  Pressure                 -32788           86480           53519           45827
v  k                    8.4754e-07          3.5378        0.031383        0.022456
v  epsilon              0.00071127      4.6376e+05          599.53          20.753
v  TurbVisc              1.973e-12          0.2163      0.00098613        0.013759
v  CourantNb              0.010539          7257.5          22.963          4.0981
v  FourierNb              0.022452      2.3655e+05          21.819         0.29239
v  total_pressure       4.6721e+05      5.8648e+05      5.5352e+05      5.4583e+05
v  Local Time Step           0.001        0.096022       0.0010096       0.0010511


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5837      2.3937e+05          44.782          4.3904


 TIME FOR THE TIME STEP              354:        0.72458E+02

===============================================================


 INSTANT    0.355000000E+01   TIME STEP NUMBER             355
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.621352059E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156473599E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22427E+02 0.40761E+01
   Friction velocity        uet   :  0.29566E-01 0.15126E+02
   Friction velocity        uk    :  0.29501E-01 0.15126E+02
   Dimensionless distance   yplus :  0.14265E-02 0.12540E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7280
   Nb of faces within the viscous sub-layer     :      17214
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76330E+01      34   0.53560E-01   0.83846E+01 0.24094E+02 
c  Velocity[X]                                      0.17229E+01 
c  Velocity[Y]                                      0.26635E+01 
c  Velocity[Z]                                      0.39982E+01 
c  Pressure     0.46663E-01     303   0.33806E-01   0.10035E+00 0.10305E+01 
c  k            0.12558E+00      23   0.10717E-03   0.91610E-03 0.22318E+02 
c  epsilon      0.15783E+04      12   0.28362E-03   0.51988E+06 0.65905E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.6797e-05                             1
a  epsilon                 -4.5562                             6
a  Local Time Step      4.2274e-08                        278655


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9208          12.103          1.0809         0.17487
v  Velocity[Y]             -17.651          18.631         0.58603          0.4208
v  Velocity[Z]             -26.862          21.667        -0.51569      -0.0033054
v  ǁVelocityǁ            0.0021855          29.461          3.4751          3.6029
v  Pressure                 -33804           86487           53520           45815
v  k                    8.4842e-07          3.5752        0.031422        0.022461
v  epsilon               0.0015541      4.5493e+05          596.66           20.76
v  TurbVisc             1.9637e-12          0.2163      0.00099002        0.013761
v  CourantNb              0.011203          8071.5           22.97          4.0986
v  FourierNb              0.022444      2.3655e+05          21.821         0.29249
v  total_pressure        4.662e+05      5.8649e+05      5.5352e+05      5.4582e+05
v  Local Time Step           0.001         0.10137       0.0010097       0.0010516


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61629      2.4044e+05          44.791           4.391


 TIME FOR THE TIME STEP              355:        0.73051E+02

===============================================================


 INSTANT    0.356000000E+01   TIME STEP NUMBER             356
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.968274657E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156432637E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27218E+02 0.40751E+01
   Friction velocity        uet   :  0.36683E-01 0.10946E+02
   Friction velocity        uk    :  0.38968E-01 0.10946E+02
   Dimensionless distance   yplus :  0.13967E-02 0.12515E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7277
   Nb of faces within the viscous sub-layer     :      17196
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76316E+01      36   0.53926E-01   0.80903E+01 0.23660E+02 
c  Velocity[X]                                      0.16542E+01 
c  Velocity[Y]                                      0.24926E+01 
c  Velocity[Z]                                      0.39435E+01 
c  Pressure     0.45521E-01     327   0.32378E-01   0.97846E-01 0.91293E+00 
c  k            0.12558E+00      15   0.93543E-04   0.86932E-03 0.21721E+02 
c  epsilon      0.15759E+04      14   0.35163E-03   0.59891E+06 0.70782E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -3.625e-05                             1
a  epsilon                 -5.3516                             3
a  Local Time Step      4.2275e-08                        278686


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9486          13.575          1.0808         0.17515
v  Velocity[Y]             -18.585          17.897         0.58524         0.42089
v  Velocity[Z]             -30.022          21.796        -0.51593      -0.0028743
v  ǁVelocityǁ            0.0028612          33.317          3.4755          3.6031
v  Pressure                 -34572           86474           53524           45813
v  k                    8.6093e-07          3.6898        0.031453        0.022466
v  epsilon               0.0015829        4.65e+05          597.02          20.769
v  TurbVisc             1.9597e-12          0.2163      0.00099467        0.013763
v  CourantNb            0.00068057          7261.9           22.96          4.0989
v  FourierNb              0.022435      2.3655e+05          21.823          0.2924
v  total_pressure       4.6543e+05      5.8647e+05      5.5352e+05      5.4581e+05
v  Local Time Step           0.001         0.11151       0.0010096       0.0010514


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38096      2.3954e+05          44.783          4.3913


 TIME FOR THE TIME STEP              356:        0.69968E+02

===============================================================


 INSTANT    0.357000000E+01   TIME STEP NUMBER             357
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.285618616E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156379119E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22642E+02 0.40902E+01
   Friction velocity        uet   :  0.24838E-01 0.10127E+02
   Friction velocity        uk    :  0.24473E-01 0.10127E+02
   Dimensionless distance   yplus :  0.11003E-02 0.12475E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7283
   Nb of faces within the viscous sub-layer     :      17175
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76302E+01      37   0.53191E-01   0.79511E+01 0.23443E+02 
c  Velocity[X]                                      0.16272E+01 
c  Velocity[Y]                                      0.24866E+01 
c  Velocity[Z]                                      0.38373E+01 
c  Pressure     0.45294E-01     383   0.32156E-01   0.97364E-01 0.91610E+00 
c  k            0.12560E+00      16   0.12704E-03   0.88366E-03 0.21823E+02 
c  epsilon      0.15863E+04      16   0.24999E-03   0.59189E+06 0.70353E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.5103e-05                             1
a  epsilon                  -4.632                             4
a  Local Time Step      4.2275e-08                        278720


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9488          11.378          1.0809         0.17537
v  Velocity[Y]             -17.707          18.335         0.58356         0.42061
v  Velocity[Z]             -27.185          21.565        -0.51618       -0.002363
v  ǁVelocityǁ            0.0026451          29.676          3.4758          3.6033
v  Pressure                 -35010           86481           53531           45822
v  k                    9.4385e-07          3.5791        0.031506         0.02247
v  epsilon               0.0015657      4.6148e+05          595.97          20.784
v  TurbVisc             1.9889e-12          0.2163      0.00099788        0.013764
v  CourantNb             0.0044818          7614.5          22.962          4.0997
v  FourierNb              0.022427      2.3655e+05          21.823         0.29236
v  total_pressure       4.6499e+05      5.8648e+05      5.5353e+05      5.4582e+05
v  Local Time Step           0.001        0.060631       0.0010092       0.0010494


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47157      2.3945e+05          44.786          4.3921


 TIME FOR THE TIME STEP              357:        0.70776E+02

===============================================================


 INSTANT    0.358000000E+01   TIME STEP NUMBER             358
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.240904077E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156333017E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27605E+02 0.40962E+01
   Friction velocity        uet   :  0.21631E-01 0.10151E+02
   Friction velocity        uk    :  0.21559E-01 0.10151E+02
   Dimensionless distance   yplus :  0.83700E-03 0.12426E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7286
   Nb of faces within the viscous sub-layer     :      17176
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76294E+01      39   0.53968E-01   0.76499E+01 0.22992E+02 
c  Velocity[X]                                      0.16210E+01 
c  Velocity[Y]                                      0.24179E+01 
c  Velocity[Z]                                      0.36109E+01 
c  Pressure     0.43883E-01     664   0.31318E-01   0.94339E-01 0.12157E+01 
c  k            0.12561E+00      19   0.11239E-03   0.79613E-03 0.20739E+02 
c  epsilon      0.15931E+04      13   0.33815E-03   0.61799E+06 0.71908E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018201                             2
a  epsilon                 -4.8237                             5
a  Local Time Step      4.2275e-08                        278711


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9497          12.413          1.0809         0.17539
v  Velocity[Y]             -19.704          17.898         0.58118         0.42021
v  Velocity[Z]             -27.887           21.59        -0.51653      -0.0018447
v  ǁVelocityǁ            0.0024758          30.859          3.4765          3.6039
v  Pressure                 -35164           86542           53579           45868
v  k                    9.0659e-07          3.6679        0.031484        0.022471
v  epsilon               0.0016573      4.6291e+05          596.68           20.77
v  TurbVisc             2.1676e-12          0.2163       0.0010008        0.013766
v  CourantNb             0.0052119          7754.3          22.964          4.1005
v  FourierNb               0.02242      2.3655e+05          21.824         0.29237
v  total_pressure       4.6484e+05      5.8654e+05      5.5358e+05      5.4587e+05
v  Local Time Step           0.001        0.066694       0.0010092       0.0010494


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54678      2.3987e+05          44.788          4.3929


 TIME FOR THE TIME STEP              358:        0.87960E+02

===============================================================


 INSTANT    0.359000000E+01   TIME STEP NUMBER             359
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.489757035E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156290206E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24080E+02 0.40917E+01
   Friction velocity        uet   :  0.26783E-01 0.11111E+02
   Friction velocity        uk    :  0.26721E-01 0.11111E+02
   Dimensionless distance   yplus :  0.48562E-03 0.12378E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7288
   Nb of faces within the viscous sub-layer     :      17160
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76297E+01      35   0.55161E-01   0.75706E+01 0.22873E+02 
c  Velocity[X]                                      0.15868E+01 
c  Velocity[Y]                                      0.24766E+01 
c  Velocity[Z]                                      0.35071E+01 
c  Pressure     0.41895E-01     691   0.29505E-01   0.90014E-01 0.68591E+01 
c  k            0.12557E+00      16   0.99831E-04   0.85993E-03 0.21594E+02 
c  epsilon      0.15866E+04      12   0.22306E-03   0.61783E+06 0.72143E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.9421                             3
a  Local Time Step      4.2275e-08                        278727


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9127          11.223          1.0814         0.17542
v  Velocity[Y]             -18.325          18.165         0.57915         0.42022
v  Velocity[Z]             -27.494          21.657         -0.5166      -0.0023283
v  ǁVelocityǁ            0.0017471          30.026          3.4774          3.6054
v  Pressure                 -34734           87034           54048           46250
v  k                    8.5773e-07          3.4972        0.031436        0.022473
v  epsilon               0.0016865      4.6351e+05           591.4          20.765
v  TurbVisc             2.0966e-12          0.2163       0.0010024        0.013768
v  CourantNb              0.017859            7465          22.968          4.1014
v  FourierNb              0.022414      2.3655e+05          21.824         0.29238
v  total_pressure       4.6527e+05      5.8703e+05      5.5405e+05      5.4625e+05
v  Local Time Step           0.001        0.068018       0.0010093       0.0010493


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68935      2.3929e+05          44.791          4.3938


 TIME FOR THE TIME STEP              359:        0.76182E+02

===============================================================


 INSTANT    0.360000000E+01   TIME STEP NUMBER             360
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.498288170E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156330994E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28017E+02 0.40796E+01
   Friction velocity        uet   :  0.17970E-01 0.11518E+02
   Friction velocity        uk    :  0.17873E-01 0.11518E+02
   Dimensionless distance   yplus :  0.12471E-02 0.12332E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7282
   Nb of faces within the viscous sub-layer     :      17166
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76352E+01      36   0.55330E-01   0.75777E+01 0.22878E+02 
c  Velocity[X]                                      0.16136E+01 
c  Velocity[Y]                                      0.24784E+01 
c  Velocity[Z]                                      0.34858E+01 
c  Pressure     0.41226E-01     462   0.28801E-01   0.88462E-01 0.89456E+00 
c  k            0.12551E+00      15   0.15515E-03   0.76491E-03 0.20390E+02 
c  epsilon      0.15694E+04      12   0.34980E-03   0.55250E+06 0.68296E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.0482e-05                             2
a  epsilon                 -5.1864                             8
a  Local Time Step      4.2275e-08                        278740


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9859          12.664          1.0825         0.17545
v  Velocity[Y]             -18.779           18.34         0.57607         0.42033
v  Velocity[Z]             -28.452          21.663        -0.51732       -0.002683
v  ǁVelocityǁ            0.0024623          31.453          3.4779           3.607
v  Pressure                 -34617           87078           54048           46257
v  k                    8.7787e-07          3.4349        0.031424        0.022473
v  epsilon               0.0016688      4.6098e+05          592.93          20.751
v  TurbVisc             1.9981e-12          0.2163       0.0010035        0.013769
v  CourantNb             0.0058749            7761          22.967          4.1031
v  FourierNb               0.02241      2.3655e+05          21.823         0.29254
v  total_pressure       4.6538e+05      5.8708e+05      5.5405e+05      5.4626e+05
v  Local Time Step           0.001        0.074819       0.0010094         0.00105


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51581      2.3903e+05          44.791          4.3956


 TIME FOR THE TIME STEP              360:        0.71975E+02

===============================================================


 INSTANT    0.361000000E+01   TIME STEP NUMBER             361
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.730601758E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156385840E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24554E+02 0.41001E+01
   Friction velocity        uet   :  0.33367E-01 0.11217E+02
   Friction velocity        uk    :  0.32851E-01 0.11217E+02
   Dimensionless distance   yplus :  0.12183E-02 0.12286E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7292
   Nb of faces within the viscous sub-layer     :      17132
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76368E+01      35   0.53772E-01   0.75275E+01 0.22800E+02 
c  Velocity[X]                                      0.15894E+01 
c  Velocity[Y]                                      0.25053E+01 
c  Velocity[Z]                                      0.34327E+01 
c  Pressure     0.40570E-01     345   0.28323E-01   0.87040E-01 0.95466E+00 
c  k            0.12550E+00      15   0.11467E-03   0.94196E-03 0.22673E+02 
c  epsilon      0.15688E+04      10   0.24962E-03   0.59382E+06 0.70888E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.9916                             3
a  Local Time Step      4.2275e-08                        278738


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9005          11.188          1.0832         0.17552
v  Velocity[Y]             -19.299          17.908         0.57331         0.42034
v  Velocity[Z]             -27.427          21.587         -0.5176      -0.0030816
v  ǁVelocityǁ            0.0018221          29.976          3.4785          3.6085
v  Pressure                 -34262           87108           54045           46257
v  k                    9.0243e-07          3.4125        0.031399        0.022478
v  epsilon               0.0011209      4.6425e+05           588.9          20.765
v  TurbVisc             2.0463e-12          0.2163       0.0010036        0.013771
v  CourantNb              0.030868          8134.1          22.965          4.1049
v  FourierNb              0.022407      2.3655e+05          21.822         0.29254
v  total_pressure       4.6574e+05      5.8711e+05      5.5404e+05      5.4626e+05
v  Local Time Step           0.001        0.082301       0.0010093       0.0010503


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69079      2.3956e+05          44.788          4.3974


 TIME FOR THE TIME STEP              361:        0.71931E+02

===============================================================


 INSTANT    0.362000000E+01   TIME STEP NUMBER             362
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.128142813E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156418993E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27839E+02 0.40736E+01
   Friction velocity        uet   :  0.15217E-01 0.14277E+02
   Friction velocity        uk    :  0.15213E-01 0.14277E+02
   Dimensionless distance   yplus :  0.18218E-02 0.12246E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7288
   Nb of faces within the viscous sub-layer     :      17139
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76393E+01      35   0.55868E-01   0.73682E+01 0.22538E+02 
c  Velocity[X]                                      0.15236E+01 
c  Velocity[Y]                                      0.23922E+01 
c  Velocity[Z]                                      0.34524E+01 
c  Pressure     0.40224E-01     359   0.28395E-01   0.86319E-01 0.90736E+00 
c  k            0.12550E+00      16   0.12443E-03   0.97262E-03 0.23024E+02 
c  epsilon      0.15661E+04      18   0.36408E-03   0.66605E+06 0.75175E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -5.4183                             3
a  Local Time Step      4.2275e-08                        278762


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9625          12.521          1.0849         0.17564
v  Velocity[Y]             -18.417          18.315          0.5701         0.42029
v  Velocity[Z]             -28.086          21.924        -0.51833       -0.003346
v  ǁVelocityǁ            0.0017648          31.039          3.4797            3.61
v  Pressure                 -33786           87127           54037           46265
v  k                    8.1992e-07          3.5123        0.031365        0.022478
v  epsilon               0.0015635      4.6141e+05          589.79          20.753
v  TurbVisc              2.074e-12          0.2163       0.0010038        0.013772
v  CourantNb             0.0081519          8123.5          22.964          4.1064
v  FourierNb              0.022406      2.3655e+05          21.822         0.29252
v  total_pressure       4.6621e+05      5.8713e+05      5.5404e+05      5.4627e+05
v  Local Time Step           0.001        0.090531       0.0010093       0.0010503


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9004      2.3949e+05          44.786          4.3989


 TIME FOR THE TIME STEP              362:        0.66438E+02

===============================================================


 INSTANT    0.363000000E+01   TIME STEP NUMBER             363
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.327380826E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156466505E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24273E+02 0.40817E+01
   Friction velocity        uet   :  0.13457E-01 0.11257E+02
   Friction velocity        uk    :  0.13454E-01 0.11257E+02
   Dimensionless distance   yplus :  0.12709E-02 0.12200E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7297
   Nb of faces within the viscous sub-layer     :      17129
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76425E+01      33   0.55264E-01   0.73343E+01 0.22486E+02 
c  Velocity[X]                                      0.15353E+01 
c  Velocity[Y]                                      0.24786E+01 
c  Velocity[Z]                                      0.33204E+01 
c  Pressure     0.40718E-01     351   0.28432E-01   0.87380E-01 0.87196E+00 
c  k            0.12550E+00      14   0.10451E-03   0.87077E-03 0.21788E+02 
c  epsilon      0.15641E+04      13   0.25427E-03   0.71473E+06 0.77929E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -5.0216                             6
a  Local Time Step      4.2275e-08                        278790


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.0342          11.194          1.0863         0.17569
v  Velocity[Y]             -20.539          17.969         0.56747         0.42023
v  Velocity[Z]             -27.259          21.561        -0.51907      -0.0036271
v  ǁVelocityǁ            0.0012559          29.831          3.4817          3.6116
v  Pressure                 -33042           87153           54029           46268
v  k                    8.8918e-07          3.6605         0.03134        0.022482
v  epsilon               0.0014931      4.6275e+05          586.93          20.749
v  TurbVisc             1.9079e-12          0.2163       0.0010033        0.013773
v  CourantNb              0.018433          8499.8          22.975           4.108
v  FourierNb              0.022406      2.3655e+05          21.821         0.29248
v  total_pressure       4.6696e+05      5.8715e+05      5.5403e+05      5.4627e+05
v  Local Time Step           0.001        0.099585       0.0010092       0.0010504


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83531      2.3932e+05          44.796          4.4005


 TIME FOR THE TIME STEP              363:        0.64994E+02

===============================================================


 INSTANT    0.364000000E+01   TIME STEP NUMBER             364
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.144773798E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156489451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27509E+02 0.40812E+01
   Friction velocity        uet   :  0.27798E-01 0.10499E+02
   Friction velocity        uk    :  0.27791E-01 0.10499E+02
   Dimensionless distance   yplus :  0.13396E-02 0.12173E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7277
   Nb of faces within the viscous sub-layer     :      17142
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76450E+01      35   0.54043E-01   0.73152E+01 0.22449E+02 
c  Velocity[X]                                      0.15363E+01 
c  Velocity[Y]                                      0.24281E+01 
c  Velocity[Z]                                      0.33508E+01 
c  Pressure     0.40276E-01     321   0.28333E-01   0.86421E-01 0.78425E+00 
c  k            0.12550E+00      14   0.86952E-04   0.72817E-03 0.19902E+02 
c  epsilon      0.15642E+04      14   0.34929E-03   0.55508E+06 0.68627E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.6508                             1
a  Local Time Step      4.2275e-08                        278790


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.0021          12.455          1.0877         0.17572
v  Velocity[Y]             -18.327          18.032         0.56511         0.42009
v  Velocity[Z]             -28.122          23.068        -0.52017      -0.0038519
v  ǁVelocityǁ            0.0017519          31.052          3.4838          3.6132
v  Pressure                 -32101           87186           54018           46273
v  k                    8.5911e-07          3.8279        0.031343        0.022485
v  epsilon               0.0014254      4.5955e+05          588.01           20.74
v  TurbVisc             2.0858e-12          0.2163       0.0010035        0.013774
v  CourantNb              0.012144            8421          22.988          4.1098
v  FourierNb              0.022408      2.3655e+05           21.82         0.29246
v  total_pressure        4.679e+05      5.8719e+05      5.5402e+05      5.4627e+05
v  Local Time Step           0.001         0.10954       0.0010092       0.0010505


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66026      2.3945e+05          44.808          4.4023


 TIME FOR THE TIME STEP              364:        0.69838E+02

===============================================================


 INSTANT    0.365000000E+01   TIME STEP NUMBER             365
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.150433758E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156541642E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24737E+02 0.40839E+01
   Friction velocity        uet   :  0.15472E-01 0.10139E+02
   Friction velocity        uk    :  0.15430E-01 0.10139E+02
   Dimensionless distance   yplus :  0.10449E-02 0.12186E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7280
   Nb of faces within the viscous sub-layer     :      17117
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76470E+01      37   0.55008E-01   0.72907E+01 0.22409E+02 
c  Velocity[X]                                      0.16198E+01 
c  Velocity[Y]                                      0.22996E+01 
c  Velocity[Z]                                      0.33713E+01 
c  Pressure     0.40024E-01     423   0.28090E-01   0.86068E-01 0.72443E+00 
c  k            0.12549E+00      13   0.76717E-04   0.62212E-03 0.18390E+02 
c  epsilon      0.15635E+04      10   0.22661E-03   0.31334E+06 0.51552E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                  -4.788                             1
a  Local Time Step      4.2275e-08                        278773


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9174          11.498          1.0886         0.17569
v  Velocity[Y]             -19.091          17.924         0.56419         0.41986
v  Velocity[Z]             -27.664          22.769         -0.5212       -0.004066
v  ǁVelocityǁ            0.0019238          30.304          3.4863           3.615
v  Pressure                 -30850           87188           54003           46270
v  k                     8.643e-07          3.7887        0.031395        0.022491
v  epsilon               0.0013766      4.5903e+05          588.29          20.755
v  TurbVisc             1.9969e-12          0.2163        0.001004        0.013776
v  CourantNb              0.014956          8652.6          23.004          4.1117
v  FourierNb              0.022411      2.3655e+05          21.821         0.29254
v  total_pressure       4.6915e+05      5.8719e+05        5.54e+05      5.4627e+05
v  Local Time Step           0.001          0.1174       0.0010092       0.0010506


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73223      2.3964e+05          44.825          4.4042


 TIME FOR THE TIME STEP              365:        0.81918E+02

===============================================================


 INSTANT    0.366000000E+01   TIME STEP NUMBER             366
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.125690025E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156562552E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28259E+02 0.40776E+01
   Friction velocity        uet   :  0.38935E-02 0.10039E+02
   Friction velocity        uk    :  0.38926E-02 0.10039E+02
   Dimensionless distance   yplus :  0.12810E-02 0.12201E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7283
   Nb of faces within the viscous sub-layer     :      17122
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76514E+01      34   0.55655E-01   0.73455E+01 0.22484E+02 
c  Velocity[X]                                      0.15537E+01 
c  Velocity[Y]                                      0.23935E+01 
c  Velocity[Z]                                      0.33983E+01 
c  Pressure     0.40059E-01     509   0.27811E-01   0.86174E-01 0.70615E+00 
c  k            0.12550E+00      14   0.85109E-04   0.68025E-03 0.19255E+02 
c  epsilon      0.15625E+04      14   0.20175E-03   0.44893E+06 0.61802E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017802                             3
a  epsilon                 -4.4348                             3
a  Local Time Step      4.2275e-08                        278746


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.981          12.956            1.09         0.17568
v  Velocity[Y]             -17.657          18.177         0.56375         0.41974
v  Velocity[Z]             -28.985           23.13        -0.52332      -0.0043316
v  ǁVelocityǁ            0.0018802          32.071          3.4899          3.6168
v  Pressure                 -30896           87192           53992           46264
v  k                    4.0398e-07          3.9347        0.031368        0.022497
v  epsilon               0.0013371      4.6027e+05          586.76          20.753
v  TurbVisc             1.9992e-12          0.2163       0.0010047        0.013777
v  CourantNb             0.0044904          8871.7           23.02          4.1138
v  FourierNb              0.022415      2.3655e+05          21.821         0.29251
v  total_pressure        4.691e+05      5.8719e+05      5.5399e+05      5.4626e+05
v  Local Time Step           0.001        0.090555       0.0010093       0.0010499


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74021      2.3956e+05          44.841          4.4063


 TIME FOR THE TIME STEP              366:        0.76108E+02

===============================================================


 INSTANT    0.367000000E+01   TIME STEP NUMBER             367
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.977711894E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156594400E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24084E+02 0.40868E+01
   Friction velocity        uet   :  0.33815E-01 0.10435E+02
   Friction velocity        uk    :  0.33724E-01 0.10435E+02
   Dimensionless distance   yplus :  0.10710E-02 0.12216E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7269
   Nb of faces within the viscous sub-layer     :      17082
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76523E+01      33   0.55176E-01   0.72291E+01 0.22295E+02 
c  Velocity[X]                                      0.15130E+01 
c  Velocity[Y]                                      0.23210E+01 
c  Velocity[Z]                                      0.33951E+01 
c  Pressure     0.39157E-01     688   0.27209E-01   0.84326E-01 0.64846E+01 
c  k            0.12550E+00      16   0.95191E-04   0.72093E-03 0.19791E+02 
c  epsilon      0.15662E+04      11   0.24405E-03   0.42012E+06 0.59556E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -5.0126                             2
a  Local Time Step      4.2274e-08                        278776


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.0428          11.175          1.0901         0.17558
v  Velocity[Y]             -19.192           18.14         0.56373         0.41954
v  Velocity[Z]             -27.434           22.23        -0.52358      -0.0037627
v  ǁVelocityǁ            0.0019176          30.007          3.4919          3.6175
v  Pressure                 -31446           86729           53550           45900
v  k                    9.0283e-07          3.6914        0.031478        0.022507
v  epsilon               0.0013023      4.6517e+05          590.46          20.784
v  TurbVisc             1.9799e-12          0.2163       0.0010058        0.013778
v  CourantNb              0.013098          8535.6          23.057          4.1162
v  FourierNb               0.02242      2.3655e+05          21.822         0.29255
v  total_pressure       4.6855e+05      5.8673e+05      5.5355e+05       5.459e+05
v  Local Time Step           0.001        0.099409       0.0010093         0.00105


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72241      2.3968e+05          44.879          4.4088


 TIME FOR THE TIME STEP              367:        0.91537E+02

===============================================================


 INSTANT    0.368000000E+01   TIME STEP NUMBER             368
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.499218202E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156522676E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27871E+02 0.40800E+01
   Friction velocity        uet   :  0.27368E-01 0.12030E+02
   Friction velocity        uk    :  0.27359E-01 0.12030E+02
   Dimensionless distance   yplus :  0.11665E-02 0.12226E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7279
   Nb of faces within the viscous sub-layer     :      17061
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76503E+01      38   0.54286E-01   0.72555E+01 0.22344E+02 
c  Velocity[X]                                      0.15596E+01 
c  Velocity[Y]                                      0.23403E+01 
c  Velocity[Z]                                      0.33556E+01 
c  Pressure     0.39249E-01     325   0.27030E-01   0.84601E-01 0.66563E+00 
c  k            0.12550E+00      17   0.78988E-04   0.79485E-03 0.20756E+02 
c  epsilon      0.15662E+04      11   0.18970E-03   0.42889E+06 0.60313E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.7251e-05                             1
a  epsilon                 -4.5441                             3
a  Local Time Step      4.2275e-08                        278736


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.132          12.786          1.0913         0.17553
v  Velocity[Y]             -17.594          18.602         0.56383         0.41937
v  Velocity[Z]             -28.498          22.088         -0.5246      -0.0031673
v  ǁVelocityǁ            0.0014496           31.56          3.4945           3.618
v  Pressure                 -31580           86721           53551           45901
v  k                    8.6353e-07          3.7196        0.031447        0.022516
v  epsilon               0.0012762      4.5915e+05           588.3          20.797
v  TurbVisc             2.1193e-12          0.2163       0.0010074        0.013779
v  CourantNb              0.012489          8506.2          23.082          4.1175
v  FourierNb              0.022426      2.3655e+05          21.822         0.29252
v  total_pressure       4.6842e+05      5.8672e+05      5.5355e+05       5.459e+05
v  Local Time Step           0.001        0.068427       0.0010092       0.0010486


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74417      2.3998e+05          44.904            4.41


 TIME FOR THE TIME STEP              368:        0.68733E+02

===============================================================


 INSTANT    0.369000000E+01   TIME STEP NUMBER             369
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.184768254E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156454411E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25146E+02 0.40897E+01
   Friction velocity        uet   :  0.29924E-01 0.12513E+02
   Friction velocity        uk    :  0.29915E-01 0.12513E+02
   Dimensionless distance   yplus :  0.13740E-02 0.12237E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7287
   Nb of faces within the viscous sub-layer     :      17026
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76504E+01      34   0.54597E-01   0.71842E+01 0.22216E+02 
c  Velocity[X]                                      0.15168E+01 
c  Velocity[Y]                                      0.23956E+01 
c  Velocity[Z]                                      0.32718E+01 
c  Pressure     0.39083E-01     331   0.27069E-01   0.84245E-01 0.68132E+00 
c  k            0.12552E+00      13   0.90904E-04   0.70354E-03 0.19490E+02 
c  epsilon      0.15708E+04      10   0.26909E-03   0.43683E+06 0.60635E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -5.1768                             3
a  Local Time Step      4.2275e-08                        278742


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3101           11.49          1.0909          0.1754
v  Velocity[Y]             -19.502          18.284         0.56469          0.4194
v  Velocity[Z]             -28.095          22.368        -0.52495      -0.0025944
v  ǁVelocityǁ            0.0017744          30.726          3.4959          3.6186
v  Pressure                 -31613           86720           53557           45906
v  k                    8.6104e-07          3.6856        0.031579        0.022526
v  epsilon               0.0012529      4.6231e+05           592.8           20.84
v  TurbVisc             2.0108e-12          0.2163       0.0010086        0.013781
v  CourantNb             0.0042279          8600.6          23.105          4.1183
v  FourierNb              0.022431      2.3655e+05          21.822         0.29249
v  total_pressure       4.6839e+05      5.8672e+05      5.5356e+05      5.4591e+05
v  Local Time Step           0.001        0.064765       0.0010092       0.0010484


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6581      2.3946e+05          44.927          4.4108


 TIME FOR THE TIME STEP              369:        0.69486E+02

===============================================================


 INSTANT    0.370000000E+01   TIME STEP NUMBER             370
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.176913912E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156394318E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29097E+02 0.40785E+01
   Friction velocity        uet   :  0.18554E-01 0.11710E+02
   Friction velocity        uk    :  0.18549E-01 0.11710E+02
   Dimensionless distance   yplus :  0.13141E-02 0.12358E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7286
   Nb of faces within the viscous sub-layer     :      17022
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76508E+01      33   0.56274E-01   0.73341E+01 0.22438E+02 
c  Velocity[X]                                      0.15516E+01 
c  Velocity[Y]                                      0.23492E+01 
c  Velocity[Z]                                      0.34333E+01 
c  Pressure     0.39573E-01     477   0.27128E-01   0.85291E-01 0.75856E+00 
c  k            0.12553E+00      16   0.11676E-03   0.76746E-03 0.20465E+02 
c  epsilon      0.15699E+04      14   0.56952E-03   0.10754E+07 0.94902E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -1.424e-05                             1
a  epsilon                 -4.4745                             5
a  Local Time Step      4.2275e-08                        278708


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.0783           12.95          1.0902         0.17517
v  Velocity[Y]             -18.314          18.468         0.56541         0.41933
v  Velocity[Z]             -28.889           21.68         -0.5245      -0.0020158
v  ǁVelocityǁ            0.0017295          31.977           3.496          3.6188
v  Pressure                 -31653           86765           53574           45915
v  k                    8.2862e-07          3.6756        0.031615        0.022536
v  epsilon               0.0012334      4.5956e+05          595.52          20.862
v  TurbVisc             1.9885e-12          0.2163       0.0010097        0.013782
v  CourantNb            0.00053625          8658.7           23.13          4.1197
v  FourierNb              0.022436      2.3655e+05          21.823         0.29255
v  total_pressure       4.6835e+05      5.8677e+05      5.5357e+05      5.4591e+05
v  Local Time Step           0.001        0.069904       0.0010093       0.0010488


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62264       2.407e+05          44.952          4.4123


 TIME FOR THE TIME STEP              370:        0.73134E+02

===============================================================


 INSTANT    0.371000000E+01   TIME STEP NUMBER             371
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.290393178E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156319492E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24858E+02 0.40901E+01
   Friction velocity        uet   :  0.19289E-01 0.12262E+02
   Friction velocity        uk    :  0.19278E-01 0.12262E+02
   Dimensionless distance   yplus :  0.15646E-02 0.12363E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7289
   Nb of faces within the viscous sub-layer     :      17029
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76485E+01      34   0.56850E-01   0.75365E+01 0.22741E+02 
c  Velocity[X]                                      0.16473E+01 
c  Velocity[Y]                                      0.24106E+01 
c  Velocity[Z]                                      0.34785E+01 
c  Pressure     0.40534E-01     685   0.27843E-01   0.87370E-01 0.54597E+01 
c  k            0.12554E+00      14   0.94220E-04   0.80565E-03 0.20785E+02 
c  epsilon      0.15725E+04      11   0.32057E-03   0.43378E+06 0.60315E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -5.1161                             4
a  Local Time Step      4.2274e-08                        278658


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.1741          11.519          1.0887         0.17498
v  Velocity[Y]              -19.57          17.681          0.5664         0.41927
v  Velocity[Z]             -27.998          21.553         -0.5236      -0.0020719
v  ǁVelocityǁ            0.0011488          30.579          3.4948          3.6192
v  Pressure                 -31277           87137           53941           46223
v  k                    8.3774e-07          3.6925        0.031616        0.022544
v  epsilon               0.0012174      4.6128e+05          594.46          20.875
v  TurbVisc             1.9147e-12          0.2163       0.0010107        0.013783
v  CourantNb              0.012656          8559.2           23.13          4.1202
v  FourierNb              0.022441      2.3655e+05          21.822         0.29264
v  total_pressure       4.6872e+05      5.8714e+05      5.5394e+05      5.4622e+05
v  Local Time Step           0.001        0.076895       0.0010094       0.0010494


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76969      2.3984e+05          44.953          4.4129


 TIME FOR THE TIME STEP              371:        0.76570E+02

===============================================================


 INSTANT    0.372000000E+01   TIME STEP NUMBER             372
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.179097151E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156353568E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28964E+02 0.40873E+01
   Friction velocity        uet   :  0.30365E-01 0.10890E+02
   Friction velocity        uk    :  0.29815E-01 0.10890E+02
   Dimensionless distance   yplus :  0.13015E-02 0.12461E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7292
   Nb of faces within the viscous sub-layer     :      17014
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76519E+01      37   0.56142E-01   0.72947E+01 0.22370E+02 
c  Velocity[X]                                      0.15702E+01 
c  Velocity[Y]                                      0.23258E+01 
c  Velocity[Z]                                      0.33987E+01 
c  Pressure     0.39972E-01     483   0.27466E-01   0.86202E-01 0.81200E+00 
c  k            0.12555E+00      16   0.12091E-03   0.10152E-02 0.23488E+02 
c  epsilon      0.15675E+04      16   0.49023E-03   0.11595E+07 0.98440E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.1224e-05                             1
a  epsilon                 -4.6841                             4
a  Local Time Step      4.2274e-08                        278575


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.2015          12.635          1.0878         0.17481
v  Velocity[Y]             -18.328          18.975         0.56742         0.41923
v  Velocity[Z]              -28.53          21.594         -0.5231      -0.0021223
v  ǁVelocityǁ            0.0020274          31.498          3.4954          3.6198
v  Pressure                 -31224           87170           53959           46229
v  k                    8.5996e-07          3.8303        0.031746        0.022553
v  epsilon               0.0011967       4.641e+05          601.05          20.913
v  TurbVisc             1.9511e-12          0.2163       0.0010115        0.013784
v  CourantNb             0.0034417          8734.5          23.121          4.1208
v  FourierNb              0.022446      2.3655e+05          21.824         0.29274
v  total_pressure       4.6878e+05      5.8717e+05      5.5396e+05      5.4623e+05
v  Local Time Step           0.001        0.083401       0.0010095       0.0010498


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71522      2.4002e+05          44.945          4.4136


 TIME FOR THE TIME STEP              372:        0.68983E+02

===============================================================


 INSTANT    0.373000000E+01   TIME STEP NUMBER             373
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.516439785E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156359282E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24699E+02 0.40983E+01
   Friction velocity        uet   :  0.17366E-01 0.10901E+02
   Friction velocity        uk    :  0.17357E-01 0.10901E+02
   Dimensionless distance   yplus :  0.11148E-02 0.12430E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7307
   Nb of faces within the viscous sub-layer     :      16999
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76514E+01      32   0.56056E-01   0.71083E+01 0.22087E+02 
c  Velocity[X]                                      0.14657E+01 
c  Velocity[Y]                                      0.22745E+01 
c  Velocity[Z]                                      0.33681E+01 
c  Pressure     0.39459E-01     349   0.27064E-01   0.84927E-01 0.76703E+00 
c  k            0.12557E+00      14   0.10269E-03   0.71625E-03 0.19632E+02 
c  epsilon      0.15690E+04      10   0.28323E-03   0.55917E+06 0.68434E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -5.0367                             3
a  Local Time Step      4.2274e-08                        278510


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.2855          11.321          1.0867         0.17456
v  Velocity[Y]             -20.007          18.249         0.56856         0.41918
v  Velocity[Z]             -27.715          21.206        -0.52166      -0.0021261
v  ǁVelocityǁ            0.0025215          30.307          3.4952          3.6201
v  Pressure                 -31161           87181           53969           46230
v  k                    8.9291e-07          3.7123        0.031685        0.022563
v  epsilon               0.0011791       4.616e+05          596.29          20.924
v  TurbVisc             1.9862e-12          0.2163       0.0010125        0.013785
v  CourantNb             0.0014292          8448.4          23.123           4.122
v  FourierNb              0.022449      2.3655e+05          21.824         0.29258
v  total_pressure       4.6884e+05      5.8718e+05      5.5397e+05      5.4623e+05
v  Local Time Step           0.001        0.091741       0.0010095       0.0010493


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58216      2.3982e+05          44.946          4.4146


 TIME FOR THE TIME STEP              373:        0.71791E+02

===============================================================


 INSTANT    0.374000000E+01   TIME STEP NUMBER             374
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.333808365E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156373734E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28352E+02 0.41028E+01
   Friction velocity        uet   :  0.30654E-01 0.10808E+02
   Friction velocity        uk    :  0.30486E-01 0.10808E+02
   Dimensionless distance   yplus :  0.10401E-02 0.12490E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7306
   Nb of faces within the viscous sub-layer     :      17025
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76513E+01      36   0.56515E-01   0.71897E+01 0.22221E+02 
c  Velocity[X]                                      0.15635E+01 
c  Velocity[Y]                                      0.22516E+01 
c  Velocity[Z]                                      0.33746E+01 
c  Pressure     0.39743E-01     502   0.27420E-01   0.85632E-01 0.99406E+00 
c  k            0.12558E+00      15   0.97893E-04   0.69001E-03 0.19328E+02 
c  epsilon      0.15664E+04      10   0.33308E-03   0.36585E+06 0.55430E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.8359e-05                             2
a  epsilon                 -4.7362                             2
a  Local Time Step      4.2274e-08                        278461


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.359          12.336          1.0851         0.17445
v  Velocity[Y]              -18.63          18.633         0.56956         0.41923
v  Velocity[Z]             -28.279          21.684        -0.52023      -0.0020476
v  ǁVelocityǁ            0.0028368          31.145          3.4945          3.6201
v  Pressure                 -31115           87222           53984           46236
v  k                    9.1657e-07          3.8113        0.031648        0.022569
v  epsilon               0.0011632      4.6527e+05          595.67          20.915
v  TurbVisc             2.0891e-12          0.2163       0.0010135        0.013787
v  CourantNb              0.005763          8760.4          23.111          4.1228
v  FourierNb              0.022452      2.3655e+05          21.824         0.29277
v  total_pressure       4.6888e+05      5.8722e+05      5.5398e+05      5.4624e+05
v  Local Time Step           0.001         0.10091       0.0010097       0.0010501


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72178      2.4111e+05          44.935          4.4156


 TIME FOR THE TIME STEP              374:        0.64460E+02

===============================================================


 INSTANT    0.375000000E+01   TIME STEP NUMBER             375
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.358416875E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156356072E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24624E+02 0.40983E+01
   Friction velocity        uet   :  0.20349E-01 0.11463E+02
   Friction velocity        uk    :  0.20327E-01 0.11463E+02
   Dimensionless distance   yplus :  0.10959E-02 0.12446E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7307
   Nb of faces within the viscous sub-layer     :      17003
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76500E+01      38   0.56105E-01   0.71469E+01 0.22149E+02 
c  Velocity[X]                                      0.15203E+01 
c  Velocity[Y]                                      0.22901E+01 
c  Velocity[Z]                                      0.33364E+01 
c  Pressure     0.39581E-01     645   0.26842E-01   0.85139E-01 0.21496E+01 
c  k            0.12558E+00      14   0.10023E-03   0.73838E-03 0.20016E+02 
c  epsilon      0.15648E+04       9   0.26949E-03   0.39636E+06 0.57712E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -5.1379                             2
a  Local Time Step      4.2275e-08                        278395


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4559          11.205          1.0843         0.17429
v  Velocity[Y]             -19.508          17.868         0.57061         0.41935
v  Velocity[Z]              -27.53          21.335        -0.51951      -0.0022013
v  ǁVelocityǁ            0.0020642          30.113          3.4943          3.6204
v  Pressure                 -30863           87360           54116           46350
v  k                    8.9022e-07          3.5617         0.03168        0.022577
v  epsilon               0.0011455      4.6341e+05          595.74          20.934
v  TurbVisc             2.1311e-12          0.2163       0.0010144        0.013788
v  CourantNb              0.018241          9147.1          23.086          4.1232
v  FourierNb              0.022454      2.3655e+05          21.824         0.29289
v  total_pressure       4.6914e+05      5.8736e+05      5.5412e+05      5.4635e+05
v  Local Time Step           0.001         0.11101       0.0010098       0.0010512


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61447       2.392e+05          44.911          4.4161


 TIME FOR THE TIME STEP              375:        0.84660E+02

===============================================================


 INSTANT    0.376000000E+01   TIME STEP NUMBER             376
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.218842749E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156375613E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27959E+02 0.40977E+01
   Friction velocity        uet   :  0.18181E-01 0.11223E+02
   Friction velocity        uk    :  0.18163E-01 0.11223E+02
   Dimensionless distance   yplus :  0.10298E-02 0.12503E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7314
   Nb of faces within the viscous sub-layer     :      17013
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76498E+01      35   0.56387E-01   0.71081E+01 0.22086E+02 
c  Velocity[X]                                      0.14649E+01 
c  Velocity[Y]                                      0.23080E+01 
c  Velocity[Z]                                      0.33352E+01 
c  Pressure     0.38790E-01     448   0.26494E-01   0.83484E-01 0.81813E+00 
c  k            0.12559E+00      15   0.82949E-04   0.66743E-03 0.19007E+02 
c  epsilon      0.15647E+04      10   0.31159E-03   0.35311E+06 0.54497E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.6915                             1
a  Local Time Step      4.2274e-08                        278335


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4944          12.131           1.083         0.17419
v  Velocity[Y]             -17.499          18.601         0.57187         0.41956
v  Velocity[Z]              -27.61          21.369        -0.51834      -0.0021658
v  ǁVelocityǁ            0.0011481          30.424          3.4941          3.6205
v  Pressure                 -30701           87405           54126           46360
v  k                    8.7035e-07          3.5371        0.031632        0.022585
v  epsilon               0.0011229      4.6474e+05          595.22           20.94
v  TurbVisc             2.0681e-12          0.2163       0.0010157        0.013789
v  CourantNb             0.0041284          9328.3          23.076          4.1238
v  FourierNb              0.022456      2.3655e+05          21.825         0.29289
v  total_pressure        4.693e+05      5.8741e+05      5.5413e+05      5.4636e+05
v  Local Time Step           0.001         0.12211         0.00101       0.0010516


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70611      2.4049e+05          44.901          4.4167


 TIME FOR THE TIME STEP              376:        0.72253E+02

===============================================================


 INSTANT    0.377000000E+01   TIME STEP NUMBER             377
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.863594027E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156368404E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24514E+02 0.40857E+01
   Friction velocity        uet   :  0.25117E-01 0.12046E+02
   Friction velocity        uk    :  0.24745E-01 0.12046E+02
   Dimensionless distance   yplus :  0.12126E-02 0.12305E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7314
   Nb of faces within the viscous sub-layer     :      16982
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76487E+01      38   0.57300E-01   0.69171E+01 0.21785E+02 
c  Velocity[X]                                      0.14377E+01 
c  Velocity[Y]                                      0.22140E+01 
c  Velocity[Z]                                      0.32653E+01 
c  Pressure     0.38941E-01     354   0.26165E-01   0.83690E-01 0.66294E+00 
c  k            0.12558E+00      17   0.79975E-04   0.74700E-03 0.20100E+02 
c  epsilon      0.15618E+04      11   0.23575E-03   0.42119E+06 0.59643E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                  -5.332                             1
a  Local Time Step      4.2274e-08                        278305


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4057           11.54          1.0831         0.17398
v  Velocity[Y]              -18.81          17.761         0.57308         0.41971
v  Velocity[Z]             -28.023          21.492        -0.51745      -0.0021665
v  ǁVelocityǁ            0.0017418          30.633          3.4951          3.6209
v  Pressure                 -30526           87411           54130           46375
v  k                    8.6473e-07          3.4503        0.031626        0.022592
v  epsilon               0.0010942      4.6335e+05           593.2          20.953
v  TurbVisc             1.9867e-12          0.2163       0.0010167         0.01379
v  CourantNb              0.014973          9176.4          23.044          4.1246
v  FourierNb              0.022457      2.3655e+05          21.826         0.29295
v  total_pressure       4.6947e+05      5.8741e+05      5.5413e+05      5.4637e+05
v  Local Time Step           0.001         0.13432       0.0010101       0.0010511


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5773      2.3988e+05           44.87          4.4175


 TIME FOR THE TIME STEP              377:        0.69822E+02

===============================================================


 INSTANT    0.378000000E+01   TIME STEP NUMBER             378
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.861843073E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156375292E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28903E+02 0.40843E+01
   Friction velocity        uet   :  0.21792E-01 0.11504E+02
   Friction velocity        uk    :  0.21770E-01 0.11504E+02
   Dimensionless distance   yplus :  0.76703E-03 0.12556E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7317
   Nb of faces within the viscous sub-layer     :      16993
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76490E+01      35   0.55637E-01   0.70224E+01 0.21946E+02 
c  Velocity[X]                                      0.14954E+01 
c  Velocity[Y]                                      0.22337E+01 
c  Velocity[Z]                                      0.32933E+01 
c  Pressure     0.39200E-01     295   0.26326E-01   0.84312E-01 0.56940E+00 
c  k            0.12559E+00      16   0.76168E-04   0.61767E-03 0.18338E+02 
c  epsilon      0.15611E+04       9   0.26086E-03   0.46773E+06 0.62957E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.7989                             1
a  Local Time Step      4.2274e-08                        278274


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4232          12.211          1.0838         0.17391
v  Velocity[Y]             -17.791          18.036         0.57429         0.41974
v  Velocity[Z]             -28.842          21.592        -0.51691      -0.0022193
v  ǁVelocityǁ           0.00081935          31.592          3.4965          3.6209
v  Pressure                 -30435           87413           54135           46383
v  k                     8.459e-07          3.4763        0.031593        0.022598
v  epsilon               0.0010649      4.5926e+05          592.46          20.951
v  TurbVisc             2.0059e-12          0.2163       0.0010181        0.013791
v  CourantNb             0.0012114          9247.8          23.039          4.1255
v  FourierNb              0.022457      2.3655e+05          21.826         0.29299
v  total_pressure       4.6957e+05      5.8741e+05      5.5413e+05      5.4638e+05
v  Local Time Step           0.001         0.14775       0.0010102       0.0010518


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65249      2.3947e+05          44.866          4.4185


 TIME FOR THE TIME STEP              378:        0.65902E+02

===============================================================


 INSTANT    0.379000000E+01   TIME STEP NUMBER             379
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.116425219E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156389950E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24304E+02 0.40735E+01
   Friction velocity        uet   :  0.19587E-01 0.12881E+02
   Friction velocity        uk    :  0.19564E-01 0.12881E+02
   Dimensionless distance   yplus :  0.11188E-02 0.12286E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7305
   Nb of faces within the viscous sub-layer     :      16987
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76482E+01      37   0.55828E-01   0.67558E+01 0.21526E+02 
c  Velocity[X]                                      0.14388E+01 
c  Velocity[Y]                                      0.21336E+01 
c  Velocity[Z]                                      0.31834E+01 
c  Pressure     0.38485E-01     480   0.25731E-01   0.82711E-01 0.69783E+00 
c  k            0.12559E+00      14   0.83095E-04   0.72773E-03 0.19831E+02 
c  epsilon      0.15574E+04      14   0.28490E-03   0.76937E+06 0.80840E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.8861                             1
a  Local Time Step      4.2275e-08                        278262


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3495           11.12          1.0842         0.17388
v  Velocity[Y]              -19.44          17.986         0.57525         0.41974
v  Velocity[Z]             -27.034          21.341        -0.51636       -0.002428
v  ǁVelocityǁ           0.00057001          29.586          3.4968          3.6213
v  Pressure                 -30329           87443           54144           46402
v  k                    8.8997e-07          3.5697        0.031569        0.022602
v  epsilon                0.001024      4.5887e+05          590.35          20.962
v  TurbVisc              1.922e-12          0.2163       0.0010197        0.013793
v  CourantNb              0.018732          9121.1          23.043          4.1261
v  FourierNb              0.022458      2.3655e+05          21.827         0.29309
v  total_pressure       4.6967e+05      5.8744e+05      5.5414e+05       5.464e+05
v  Local Time Step           0.001         0.16252       0.0010104        0.001053


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.79554      2.3897e+05           44.87          4.4191


 TIME FOR THE TIME STEP              379:        0.77183E+02

===============================================================


 INSTANT    0.380000000E+01   TIME STEP NUMBER             380
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.106038099E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156411034E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26922E+02 0.40856E+01
   Friction velocity        uet   :  0.14755E-01 0.11303E+02
   Friction velocity        uk    :  0.14746E-01 0.11303E+02
   Dimensionless distance   yplus :  0.14423E-02 0.12472E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7320
   Nb of faces within the viscous sub-layer     :      16991
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76497E+01      36   0.56356E-01   0.66957E+01 0.21415E+02 
c  Velocity[X]                                      0.14127E+01 
c  Velocity[Y]                                      0.21150E+01 
c  Velocity[Z]                                      0.31680E+01 
c  Pressure     0.38469E-01     263   0.25636E-01   0.82699E-01 0.56340E+00 
c  k            0.12558E+00      15   0.76742E-04   0.61797E-03 0.18280E+02 
c  epsilon      0.15538E+04      11   0.17029E-03   0.36303E+06 0.55719E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.7955                             1
a  Local Time Step      4.2275e-08                        278293


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3387          11.774          1.0847         0.17385
v  Velocity[Y]             -18.175          18.443         0.57572         0.41963
v  Velocity[Z]             -27.103          21.673        -0.51719      -0.0028198
v  ǁVelocityǁ            0.0012935           29.79          3.4988           3.622
v  Pressure                 -30323           87446           54144           46408
v  k                    8.5836e-07            3.59        0.031503        0.022604
v  epsilon              0.00098885      4.5947e+05          586.61           20.94
v  TurbVisc             2.0654e-12          0.2163       0.0010206        0.013793
v  CourantNb               0.01403          9622.9          23.025          4.1267
v  FourierNb              0.022458      2.3655e+05          21.828          0.2931
v  total_pressure       4.6968e+05      5.8745e+05      5.5414e+05      5.4641e+05
v  Local Time Step           0.001         0.16544       0.0010104       0.0010529


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60063      2.3917e+05          44.853          4.4198


 TIME FOR THE TIME STEP              380:        0.61485E+02

===============================================================


 INSTANT    0.381000000E+01   TIME STEP NUMBER             381
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.170431127E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156446492E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25185E+02 0.40509E+01
   Friction velocity        uet   :  0.11824E-01 0.14001E+02
   Friction velocity        uk    :  0.11812E-01 0.14001E+02
   Dimensionless distance   yplus :  0.15656E-02 0.12267E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7302
   Nb of faces within the viscous sub-layer     :      16989
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76507E+01      36   0.56984E-01   0.66581E+01 0.21358E+02 
c  Velocity[X]                                      0.14070E+01 
c  Velocity[Y]                                      0.21105E+01 
c  Velocity[Z]                                      0.31407E+01 
c  Pressure     0.37962E-01     320   0.25334E-01   0.81497E-01 0.53243E+00 
c  k            0.12558E+00      14   0.82140E-04   0.56056E-03 0.17438E+02 
c  epsilon      0.15537E+04       9   0.20985E-03   0.23279E+06 0.44618E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -5.0178                             1
a  Local Time Step      4.2275e-08                        278266


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.2949           11.63          1.0861         0.17396
v  Velocity[Y]              -19.78          17.925         0.57587         0.41965
v  Velocity[Z]             -28.301          21.481        -0.51826      -0.0032575
v  ǁVelocityǁ            0.0012584          30.963          3.5003          3.6227
v  Pressure                 -30289           87442           54140           46411
v  k                    8.6428e-07          3.5233        0.031537        0.022606
v  epsilon              0.00095532      4.5322e+05           586.6          20.951
v  TurbVisc             2.0061e-12          0.2163       0.0010215        0.013794
v  CourantNb              0.035794          9542.7          23.047          4.1284
v  FourierNb              0.022458      2.3655e+05          21.828         0.29312
v  total_pressure       4.6971e+05      5.8744e+05      5.5414e+05      5.4641e+05
v  Local Time Step           0.001         0.16545       0.0010104       0.0010532


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78654      2.4007e+05          44.875          4.4215


 TIME FOR THE TIME STEP              381:        0.64198E+02

===============================================================


 INSTANT    0.382000000E+01   TIME STEP NUMBER             382
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.677399295E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156462974E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29297E+02 0.40626E+01
   Friction velocity        uet   :  0.32480E-01 0.13518E+02
   Friction velocity        uk    :  0.32441E-01 0.13518E+02
   Dimensionless distance   yplus :  0.13702E-02 0.12297E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7306
   Nb of faces within the viscous sub-layer     :      16986
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76510E+01      38   0.56650E-01   0.66218E+01 0.21299E+02 
c  Velocity[X]                                      0.13974E+01 
c  Velocity[Y]                                      0.20319E+01 
c  Velocity[Z]                                      0.31925E+01 
c  Pressure     0.37048E-01     464   0.24852E-01   0.79671E-01 0.60675E+00 
c  k            0.12559E+00      12   0.79007E-04   0.58601E-03 0.17821E+02 
c  epsilon      0.15537E+04       9   0.26556E-03   0.38247E+06 0.57121E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.6529                             1
a  Local Time Step      4.2275e-08                        278241


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3072          12.188          1.0876         0.17417
v  Velocity[Y]             -17.737          18.045         0.57569         0.41958
v  Velocity[Z]             -28.604          21.653        -0.51985      -0.0036258
v  ǁVelocityǁ           0.00094885          31.352          3.5027          3.6232
v  Pressure                 -30306           87441           54128           46405
v  k                    8.7003e-07          3.6137         0.03157        0.022609
v  epsilon              0.00092107       4.596e+05          588.84          20.959
v  TurbVisc             2.0086e-12          0.2163       0.0010223        0.013795
v  CourantNb            0.00082065            9143           23.03          4.1298
v  FourierNb              0.022459      2.3655e+05          21.829         0.29309
v  total_pressure       4.6969e+05      5.8744e+05      5.5413e+05      5.4641e+05
v  Local Time Step           0.001         0.11381       0.0010104       0.0010522


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64203      2.3962e+05          44.859          4.4229


 TIME FOR THE TIME STEP              382:        0.68796E+02

===============================================================


 INSTANT    0.383000000E+01   TIME STEP NUMBER             383
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.141896458E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156503187E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24318E+02 0.40621E+01
   Friction velocity        uet   :  0.32990E-01 0.10555E+02
   Friction velocity        uk    :  0.32978E-01 0.10555E+02
   Dimensionless distance   yplus :  0.74432E-03 0.12242E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7315
   Nb of faces within the viscous sub-layer     :      16988
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76503E+01      37   0.56509E-01   0.67438E+01 0.21485E+02 
c  Velocity[X]                                      0.14959E+01 
c  Velocity[Y]                                      0.20285E+01 
c  Velocity[Z]                                      0.32194E+01 
c  Pressure     0.37917E-01     448   0.25359E-01   0.81391E-01 0.58777E+00 
c  k            0.12561E+00      13   0.74959E-04   0.55303E-03 0.17289E+02 
c  epsilon      0.15541E+04       9   0.24098E-03   0.41061E+06 0.59244E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00051622                             4
a  epsilon                 -5.1555                             4
a  Local Time Step      4.2275e-08                        278195


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.946          11.303          1.0881         0.17428
v  Velocity[Y]             -19.368          18.028         0.57524         0.41962
v  Velocity[Z]             -27.301          21.392        -0.52071      -0.0040345
v  ǁVelocityǁ           0.00054164          29.912          3.5038          3.6239
v  Pressure                 -30347           87390           54112           46407
v  k                    8.6279e-07           3.716        0.031546        0.022612
v  epsilon              0.00076071      4.5762e+05          586.65          20.969
v  TurbVisc             2.0135e-12          0.2163       0.0010224        0.013795
v  CourantNb             0.0096608          9436.6           23.05          4.1311
v  FourierNb              0.022459      2.3655e+05          21.829         0.29311
v  total_pressure       4.6965e+05      5.8739e+05      5.5411e+05      5.4641e+05
v  Local Time Step           0.001         0.12519       0.0010104       0.0010522


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57844      2.4029e+05          44.879          4.4242


 TIME FOR THE TIME STEP              383:        0.69889E+02

===============================================================


 INSTANT    0.384000000E+01   TIME STEP NUMBER             384
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.345121305E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156549234E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27429E+02 0.40746E+01
   Friction velocity        uet   :  0.11901E-01 0.13755E+02
   Friction velocity        uk    :  0.11897E-01 0.13755E+02
   Dimensionless distance   yplus :  0.13295E-02 0.12344E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7313
   Nb of faces within the viscous sub-layer     :      16995
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76518E+01      36   0.56267E-01   0.66809E+01 0.21391E+02 
c  Velocity[X]                                      0.15009E+01 
c  Velocity[Y]                                      0.20790E+01 
c  Velocity[Z]                                      0.31010E+01 
c  Pressure     0.37641E-01     971   0.25136E-01   0.81033E-01 0.50754E+01 
c  k            0.12561E+00      14   0.69455E-04   0.51835E-03 0.16783E+02 
c  epsilon      0.15542E+04       9   0.23000E-03   0.28564E+06 0.49428E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.7796                             1
a  Local Time Step      4.2275e-08                        278181


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.0042          11.872          1.0893         0.17439
v  Velocity[Y]             -18.073          18.322         0.57456         0.41958
v  Velocity[Z]             -27.629          21.743        -0.52226      -0.0036303
v  ǁVelocityǁ            0.0035044           30.32          3.5061          3.6238
v  Pressure                 -30734           87035           53749           46120
v  k                    8.1624e-07          3.8251        0.031558        0.022613
v  epsilon              0.00028616      4.5895e+05          587.09          20.963
v  TurbVisc             2.4508e-12          0.2163       0.0010224        0.013796
v  CourantNb               0.01478          9105.5          23.052          4.1324
v  FourierNb               0.02246      2.3655e+05          21.829         0.29316
v  total_pressure       4.6927e+05      5.8703e+05      5.5375e+05      5.4612e+05
v  Local Time Step           0.001         0.13771       0.0010105        0.001053


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73924      2.4064e+05          44.881          4.4256


 TIME FOR THE TIME STEP              384:        0.83260E+02

===============================================================


 INSTANT    0.385000000E+01   TIME STEP NUMBER             385
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.155749140E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156484176E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24782E+02 0.40602E+01
   Friction velocity        uet   :  0.36071E-01 0.12641E+02
   Friction velocity        uk    :  0.38999E-01 0.12641E+02
   Dimensionless distance   yplus :  0.11578E-02 0.12211E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7313
   Nb of faces within the viscous sub-layer     :      16988
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76474E+01      34   0.55847E-01   0.64750E+01 0.21050E+02 
c  Velocity[X]                                      0.14128E+01 
c  Velocity[Y]                                      0.20305E+01 
c  Velocity[Z]                                      0.30317E+01 
c  Pressure     0.37555E-01     357   0.24877E-01   0.80806E-01 0.63531E+00 
c  k            0.12561E+00      13   0.80382E-04   0.59178E-03 0.17897E+02 
c  epsilon      0.15562E+04      10   0.19699E-03   0.26010E+06 0.47037E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.9196                             2
a  Local Time Step      4.2275e-08                        278176


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.0578          11.441          1.0892         0.17439
v  Velocity[Y]             -19.586          18.048         0.57407         0.41944
v  Velocity[Z]             -27.782          21.653        -0.52288      -0.0033382
v  ǁVelocityǁ            0.0025549          30.428          3.5073          3.6241
v  Pressure                 -30744           87004           53746           46120
v  k                    8.3822e-07          3.5922        0.031605        0.022618
v  epsilon              0.00030251      4.5689e+05          588.78          20.982
v  TurbVisc             1.8064e-12          0.2163       0.0010228        0.013796
v  CourantNb             0.0046433            9687           23.07          4.1329
v  FourierNb               0.02246      2.3655e+05          21.829         0.29312
v  total_pressure       4.6926e+05        5.87e+05      5.5375e+05      5.4612e+05
v  Local Time Step           0.001         0.15148       0.0010106       0.0010531


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71114      2.3962e+05          44.899           4.426


 TIME FOR THE TIME STEP              385:        0.72693E+02

===============================================================


 INSTANT    0.386000000E+01   TIME STEP NUMBER             386
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.148896310E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156475483E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28314E+02 0.40707E+01
   Friction velocity        uet   :  0.36426E-01 0.15363E+02
   Friction velocity        uk    :  0.38403E-01 0.15363E+02
   Dimensionless distance   yplus :  0.16255E-02 0.12194E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7305
   Nb of faces within the viscous sub-layer     :      16983
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76472E+01      42   0.55899E-01   0.65692E+01 0.21213E+02 
c  Velocity[X]                                      0.14409E+01 
c  Velocity[Y]                                      0.20379E+01 
c  Velocity[Z]                                      0.30904E+01 
c  Pressure     0.37509E-01     301   0.24841E-01   0.80832E-01 0.51286E+00 
c  k            0.12562E+00      13   0.73110E-04   0.53425E-03 0.17007E+02 
c  epsilon      0.15571E+04       9   0.22492E-03   0.31727E+06 0.52006E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.8085                             2
a  Local Time Step      4.2275e-08                        278152


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.2549          12.199          1.0887         0.17441
v  Velocity[Y]             -17.547          18.091         0.57358         0.41917
v  Velocity[Z]             -28.396          21.644        -0.52405      -0.0030439
v  ǁVelocityǁ            0.0017793          31.167          3.5078          3.6238
v  Pressure                 -30770           86984           53746           46120
v  k                    8.2507e-07          3.6664        0.031597        0.022623
v  epsilon              0.00019932      4.5615e+05          588.58          20.983
v  TurbVisc             2.0772e-12          0.2163       0.0010229        0.013796
v  CourantNb             0.0046799          9712.4          23.076          4.1341
v  FourierNb              0.022461      2.3655e+05          21.829         0.29321
v  total_pressure       4.6923e+05      5.8698e+05      5.5375e+05      5.4612e+05
v  Local Time Step           0.001         0.16545       0.0010107        0.001054


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71652      2.3965e+05          44.905          4.4273


 TIME FOR THE TIME STEP              386:        0.68550E+02

===============================================================


 INSTANT    0.387000000E+01   TIME STEP NUMBER             387
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.200394860E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156447865E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24976E+02 0.40659E+01
   Friction velocity        uet   :  0.29527E-01 0.15104E+02
   Friction velocity        uk    :  0.31117E-01 0.15104E+02
   Dimensionless distance   yplus :  0.19273E-02 0.12177E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7308
   Nb of faces within the viscous sub-layer     :      16975
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76459E+01      34   0.56435E-01   0.64548E+01 0.21019E+02 
c  Velocity[X]                                      0.14342E+01 
c  Velocity[Y]                                      0.19185E+01 
c  Velocity[Z]                                      0.31021E+01 
c  Pressure     0.37461E-01     299   0.24815E-01   0.80671E-01 0.56058E+00 
c  k            0.12562E+00      17   0.91738E-04   0.57367E-03 0.17593E+02 
c  epsilon      0.15575E+04      13   0.28871E-03   0.69231E+06 0.76661E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.9794                             2
a  Local Time Step      4.2275e-08                        278117


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3618          11.405          1.0878         0.17449
v  Velocity[Y]             -18.953          18.176         0.57322         0.41915
v  Velocity[Z]             -27.668          21.594        -0.52491      -0.0028057
v  ǁVelocityǁ            0.0026759            30.3          3.5082           3.624
v  Pressure                 -30814           86982           53750           46117
v  k                    8.0495e-07          3.5264         0.03167        0.022625
v  epsilon              0.00060877      4.5495e+05          592.46          20.997
v  TurbVisc             1.9745e-12          0.2163       0.0010234        0.013797
v  CourantNb             0.0034098          9671.7          23.088          4.1344
v  FourierNb              0.022461      2.3655e+05           21.83         0.29329
v  total_pressure       4.6919e+05      5.8698e+05      5.5375e+05      5.4612e+05
v  Local Time Step           0.001         0.16544       0.0010107       0.0010543


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54663      2.3923e+05          44.918          4.4277


 TIME FOR THE TIME STEP              387:        0.61288E+02

===============================================================


 INSTANT    0.388000000E+01   TIME STEP NUMBER             388
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.218524435E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156413925E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28090E+02 0.40691E+01
   Friction velocity        uet   :  0.21717E-01 0.14710E+02
   Friction velocity        uk    :  0.21678E-01 0.14710E+02
   Dimensionless distance   yplus :  0.15493E-02 0.12175E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7309
   Nb of faces within the viscous sub-layer     :      16991
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76432E+01      33   0.56825E-01   0.63938E+01 0.20914E+02 
c  Velocity[X]                                      0.14077E+01 
c  Velocity[Y]                                      0.18672E+01 
c  Velocity[Z]                                      0.31189E+01 
c  Pressure     0.37285E-01     348   0.24679E-01   0.80252E-01 0.56727E+00 
c  k            0.12563E+00      14   0.81252E-04   0.57341E-03 0.17616E+02 
c  epsilon      0.15565E+04       9   0.21857E-03   0.69625E+06 0.77039E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.6761                             2
a  Local Time Step      4.2275e-08                        278086


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.363          12.013          1.0877         0.17453
v  Velocity[Y]             -18.061          18.413         0.57318         0.41911
v  Velocity[Z]             -27.661          21.648        -0.52657      -0.0025139
v  ǁVelocityǁ            0.0032183          30.415          3.5093          3.6241
v  Pressure                 -30852           86999           53760           46116
v  k                    7.8632e-07          3.5846        0.031607        0.022627
v  epsilon              0.00030064      4.5488e+05          589.11          20.988
v  TurbVisc             1.9861e-12          0.2163        0.001024        0.013798
v  CourantNb              0.010083          9646.6          23.089          4.1351
v  FourierNb               0.02246      2.3655e+05          21.829         0.29326
v  total_pressure       4.6915e+05        5.87e+05      5.5376e+05      5.4612e+05
v  Local Time Step           0.001         0.16546       0.0010108       0.0010545


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44621      2.3931e+05          44.917          4.4284


 TIME FOR THE TIME STEP              388:        0.72842E+02

===============================================================


 INSTANT    0.389000000E+01   TIME STEP NUMBER             389
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.118358537E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156380277E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24547E+02 0.40770E+01
   Friction velocity        uet   :  0.23503E-01 0.11419E+02
   Friction velocity        uk    :  0.23460E-01 0.11419E+02
   Dimensionless distance   yplus :  0.14416E-02 0.12179E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7298
   Nb of faces within the viscous sub-layer     :      16978
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76410E+01      36   0.55957E-01   0.66451E+01 0.21331E+02 
c  Velocity[X]                                      0.14936E+01 
c  Velocity[Y]                                      0.19938E+01 
c  Velocity[Z]                                      0.31576E+01 
c  Pressure     0.38375E-01     331   0.25412E-01   0.82491E-01 0.52698E+00 
c  k            0.12564E+00      17   0.86771E-04   0.64459E-03 0.18664E+02 
c  epsilon      0.15597E+04      10   0.29224E-03   0.56401E+06 0.69145E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -5.4594                             6
a  Local Time Step      4.2275e-08                        278096


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.9971          11.646          1.0868         0.17453
v  Velocity[Y]             -19.682          18.756         0.57312         0.41913
v  Velocity[Z]              -28.08          22.267        -0.52784      -0.0022963
v  ǁVelocityǁ            0.0012145          30.772          3.5097          3.6239
v  Pressure                 -30905           86989           53772           46122
v  k                    7.6236e-07          3.6101        0.031664        0.022633
v  epsilon              0.00069897      4.6052e+05          591.01          21.013
v  TurbVisc             2.0432e-12          0.2163       0.0010247        0.013798
v  CourantNb             0.0086706           10466          23.111          4.1358
v  FourierNb               0.02246      2.3655e+05          21.829         0.29336
v  total_pressure       4.6909e+05      5.8699e+05      5.5377e+05      5.4612e+05
v  Local Time Step           0.001         0.16544       0.0010109       0.0010553


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44073      2.3976e+05          44.939          4.4292


 TIME FOR THE TIME STEP              389:        0.65625E+02

===============================================================


 INSTANT    0.390000000E+01   TIME STEP NUMBER             390
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.359356768E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156347122E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28909E+02 0.40815E+01
   Friction velocity        uet   :  0.28291E-01 0.11445E+02
   Friction velocity        uk    :  0.28283E-01 0.11445E+02
   Dimensionless distance   yplus :  0.50028E-03 0.12182E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7293
   Nb of faces within the viscous sub-layer     :      16983
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76406E+01      33   0.56151E-01   0.66700E+01 0.21347E+02 
c  Velocity[X]                                      0.14803E+01 
c  Velocity[Y]                                      0.20925E+01 
c  Velocity[Z]                                      0.30972E+01 
c  Pressure     0.38409E-01     540   0.25498E-01   0.82708E-01 0.21364E+01 
c  k            0.12565E+00      17   0.75618E-04   0.59714E-03 0.17988E+02 
c  epsilon      0.15581E+04      11   0.27175E-03   0.95742E+06 0.90171E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.3328e-05                             1
a  epsilon                 -4.3769                             3
a  Local Time Step      4.2275e-08                        278064


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.0996          12.359          1.0863         0.17453
v  Velocity[Y]             -17.596          18.686         0.57336         0.41921
v  Velocity[Z]             -28.783          21.667        -0.52941      -0.0023814
v  ǁVelocityǁ             0.001572          31.587          3.5097          3.6238
v  Pressure                 -30848           87138           53920           46240
v  k                    7.3703e-07          3.6661        0.031656        0.022636
v  epsilon              0.00024206      4.5316e+05           590.2          21.009
v  TurbVisc             2.0517e-12          0.2163       0.0010257        0.013799
v  CourantNb              0.022153          9797.5          23.109           4.136
v  FourierNb              0.022458      2.3655e+05          21.829         0.29334
v  total_pressure       4.6915e+05      5.8714e+05      5.5392e+05      5.4624e+05
v  Local Time Step           0.001         0.16545        0.001011       0.0010553


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56396      2.3908e+05          44.938          4.4293


 TIME FOR THE TIME STEP              390:        0.74109E+02

===============================================================


 INSTANT    0.391000000E+01   TIME STEP NUMBER             391
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.107572932E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156350534E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24563E+02 0.40761E+01
   Friction velocity        uet   :  0.31725E-01 0.10600E+02
   Friction velocity        uk    :  0.31235E-01 0.10600E+02
   Dimensionless distance   yplus :  0.13347E-02 0.12186E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7306
   Nb of faces within the viscous sub-layer     :      16975
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76394E+01      34   0.55191E-01   0.65497E+01 0.21173E+02 
c  Velocity[X]                                      0.14393E+01 
c  Velocity[Y]                                      0.20022E+01 
c  Velocity[Z]                                      0.31082E+01 
c  Pressure     0.37322E-01     299   0.24865E-01   0.80355E-01 0.49518E+00 
c  k            0.12565E+00      14   0.82904E-04   0.68292E-03 0.19209E+02 
c  epsilon      0.15549E+04      12   0.38103E-03   0.11014E+07 0.96696E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.8714                             2
a  Local Time Step      4.2275e-08                        278090


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.1582          11.381          1.0858         0.17441
v  Velocity[Y]             -18.907          18.995         0.57315         0.41921
v  Velocity[Z]             -27.292          21.336        -0.53091      -0.0024262
v  ǁVelocityǁ            0.0021733          29.914          3.5096          3.6241
v  Pressure                 -30921           87130           53928           46247
v  k                    7.1349e-07          3.6976        0.031687        0.022642
v  epsilon              0.00041175      4.6008e+05          591.39          21.027
v  TurbVisc              2.338e-12          0.2163        0.001026        0.013799
v  CourantNb              0.027924          9707.4          23.113          4.1363
v  FourierNb              0.022457      2.3655e+05          21.829         0.29337
v  total_pressure       4.6908e+05      5.8713e+05      5.5393e+05      5.4625e+05
v  Local Time Step           0.001         0.16546        0.001011       0.0010558


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76978       2.393e+05          44.943          4.4297


 TIME FOR THE TIME STEP              391:        0.61125E+02

===============================================================


 INSTANT    0.392000000E+01   TIME STEP NUMBER             392
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.200177206E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156350139E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27355E+02 0.40642E+01
   Friction velocity        uet   :  0.30081E-01 0.91995E+01
   Friction velocity        uk    :  0.30026E-01 0.91995E+01
   Dimensionless distance   yplus :  0.95773E-03 0.12189E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7303
   Nb of faces within the viscous sub-layer     :      16971
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76394E+01      34   0.56510E-01   0.65877E+01 0.21248E+02 
c  Velocity[X]                                      0.14043E+01 
c  Velocity[Y]                                      0.19548E+01 
c  Velocity[Z]                                      0.32286E+01 
c  Pressure     0.36739E-01     465   0.24512E-01   0.79125E-01 0.69231E+00 
c  k            0.12564E+00      15   0.79168E-04   0.61232E-03 0.18204E+02 
c  epsilon      0.15535E+04      11   0.23716E-03   0.50657E+06 0.65751E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -5.1016                             1
a  Local Time Step      4.2275e-08                        278082


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3261          11.784          1.0856         0.17439
v  Velocity[Y]             -18.029          19.404          0.5739         0.41927
v  Velocity[Z]             -27.061          21.782        -0.53335      -0.0023865
v  ǁVelocityǁ            0.0022518          29.743          3.5107           3.624
v  Pressure                 -30905           87175           53948           46251
v  k                    6.9132e-07          3.4946        0.031645        0.022645
v  epsilon              0.00017547       4.571e+05          588.49          21.017
v  TurbVisc             1.9085e-12          0.2163       0.0010259          0.0138
v  CourantNb              0.022598           10038          23.103          4.1369
v  FourierNb              0.022456      2.3655e+05          21.828         0.29333
v  total_pressure        4.691e+05      5.8718e+05      5.5395e+05      5.4625e+05
v  Local Time Step           0.001         0.16546        0.001011       0.0010552


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53815      2.3898e+05          44.931          4.4302


 TIME FOR THE TIME STEP              392:        0.78153E+02

===============================================================


 INSTANT    0.393000000E+01   TIME STEP NUMBER             393
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.141928788E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156330479E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25391E+02 0.40606E+01
   Friction velocity        uet   :  0.17456E-01 0.96375E+01
   Friction velocity        uk    :  0.17227E-01 0.96375E+01
   Dimensionless distance   yplus :  0.43408E-03 0.12192E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7301
   Nb of faces within the viscous sub-layer     :      16949
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76380E+01      37   0.56222E-01   0.68861E+01 0.21717E+02 
c  Velocity[X]                                      0.14499E+01 
c  Velocity[Y]                                      0.20767E+01 
c  Velocity[Z]                                      0.33595E+01 
c  Pressure     0.37606E-01     274   0.24789E-01   0.80817E-01 0.47715E+00 
c  k            0.12564E+00      16   0.77247E-04   0.62735E-03 0.18401E+02 
c  epsilon      0.15572E+04      11   0.31038E-03   0.49889E+06 0.65124E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.3337e-05                             1
a  epsilon                 -4.9259                             2
a  Local Time Step      4.2275e-08                        278078


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4163          11.766          1.0854         0.17445
v  Velocity[Y]             -19.539          19.557         0.57525         0.41927
v  Velocity[Z]             -28.558          21.567        -0.53466      -0.0023148
v  ǁVelocityǁ            0.0018976          31.264          3.5112          3.6242
v  Pressure                 -30908           87172           53953           46257
v  k                    6.6583e-07          3.4633        0.031731        0.022648
v  epsilon              0.00018468      4.5619e+05           591.6          21.038
v  TurbVisc             2.1001e-12          0.2163       0.0010258          0.0138
v  CourantNb             0.0027645           10218          23.127           4.137
v  FourierNb              0.022454      2.3655e+05          21.827         0.29329
v  total_pressure       4.6909e+05      5.8717e+05      5.5395e+05      5.4626e+05
v  Local Time Step           0.001         0.16545       0.0010109       0.0010544


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.95219      2.3922e+05          44.954          4.4303


 TIME FOR THE TIME STEP              393:        0.62537E+02

===============================================================


 INSTANT    0.394000000E+01   TIME STEP NUMBER             394
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.392770328E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156326910E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29723E+02 0.40756E+01
   Friction velocity        uet   :  0.34342E-01 0.10038E+02
   Friction velocity        uk    :  0.34438E-01 0.10038E+02
   Dimensionless distance   yplus :  0.12809E-02 0.12193E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7318
   Nb of faces within the viscous sub-layer     :      16941
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76373E+01      32   0.55422E-01   0.66540E+01 0.21344E+02 
c  Velocity[X]                                      0.13829E+01 
c  Velocity[Y]                                      0.21144E+01 
c  Velocity[Z]                                      0.31568E+01 
c  Pressure     0.37157E-01     610   0.24507E-01   0.79898E-01 0.38507E+01 
c  k            0.12564E+00      13   0.80998E-04   0.59232E-03 0.17871E+02 
c  epsilon      0.15562E+04       9   0.26077E-03   0.52568E+06 0.66781E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.1384e-05                             1
a  epsilon                 -4.7877                             3
a  Local Time Step      4.2275e-08                        278056


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4383          12.021          1.0851         0.17453
v  Velocity[Y]             -18.123          19.226         0.57685          0.4193
v  Velocity[Z]             -27.966          21.679        -0.53573      -0.0025566
v  ǁVelocityǁ            0.0024603           30.67          3.5121          3.6249
v  Pressure                 -30656           87451           54208           46470
v  k                    6.4343e-07          3.5344        0.031718        0.022653
v  epsilon              0.00046694      4.5904e+05          591.33          21.036
v  TurbVisc             2.2666e-12          0.2163       0.0010263        0.013801
v  CourantNb             0.0027274           10210          23.133          4.1374
v  FourierNb              0.022453      2.3655e+05          21.827         0.29346
v  total_pressure       4.6934e+05      5.8745e+05      5.5421e+05      5.4647e+05
v  Local Time Step           0.001         0.16545       0.0010111       0.0010551


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61772      2.3932e+05          44.961          4.4308


 TIME FOR THE TIME STEP              394:        0.81430E+02

===============================================================


 INSTANT    0.395000000E+01   TIME STEP NUMBER             395
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.285879041E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156367176E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24263E+02 0.40841E+01
   Friction velocity        uet   :  0.35626E-01 0.13137E+02
   Friction velocity        uk    :  0.35067E-01 0.13137E+02
   Dimensionless distance   yplus :  0.87361E-03 0.12195E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7314
   Nb of faces within the viscous sub-layer     :      16946
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76405E+01      32   0.54684E-01   0.64849E+01 0.21062E+02 
c  Velocity[X]                                      0.13917E+01 
c  Velocity[Y]                                      0.20756E+01 
c  Velocity[Z]                                      0.30176E+01 
c  Pressure     0.37364E-01     352   0.24663E-01   0.80296E-01 0.53459E+00 
c  k            0.12564E+00      14   0.88131E-04   0.53640E-03 0.17043E+02 
c  epsilon      0.15563E+04      11   0.23995E-03   0.34308E+06 0.53937E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.3914e-05                             1
a  epsilon                 -5.2468                             2
a  Local Time Step      4.2275e-08                        278036


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4254          11.529          1.0846         0.17453
v  Velocity[Y]             -19.623          21.117          0.5791         0.41922
v  Velocity[Z]             -27.561          21.458        -0.53591      -0.0027618
v  ǁVelocityǁ              0.00175          30.206          3.5112          3.6252
v  Pressure                 -30638           87460           54215           46463
v  k                    6.1925e-07          3.4356        0.031766        0.022658
v  epsilon                0.000544      4.5586e+05          592.96          21.042
v  TurbVisc              1.947e-12          0.2163       0.0010273        0.013801
v  CourantNb             0.0017143          9789.7           23.14          4.1386
v  FourierNb              0.022452      2.3655e+05          21.828          0.2933
v  total_pressure       4.6936e+05      5.8746e+05      5.5421e+05      5.4646e+05
v  Local Time Step           0.001         0.11677        0.001011       0.0010537


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.8128      2.4013e+05          44.967          4.4319


 TIME FOR THE TIME STEP              395:        0.58830E+02

===============================================================


 INSTANT    0.396000000E+01   TIME STEP NUMBER             396
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.279346205E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156385358E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27824E+02 0.40825E+01
   Friction velocity        uet   :  0.23479E-01 0.15623E+02
   Friction velocity        uk    :  0.23351E-01 0.15623E+02
   Dimensionless distance   yplus :  0.17667E-02 0.12196E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7306
   Nb of faces within the viscous sub-layer     :      16950
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76409E+01      33   0.56841E-01   0.65316E+01 0.21152E+02 
c  Velocity[X]                                      0.14221E+01 
c  Velocity[Y]                                      0.20710E+01 
c  Velocity[Z]                                      0.30384E+01 
c  Pressure     0.36302E-01     375   0.23974E-01   0.77999E-01 0.62844E+00 
c  k            0.12565E+00      15   0.85202E-04   0.64751E-03 0.18672E+02 
c  epsilon      0.15543E+04      10   0.35977E-03   0.48909E+06 0.64513E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.2489e-05                             1
a  epsilon                  -4.903                             2
a  Local Time Step      4.2275e-08                        277988


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4838          11.712          1.0838         0.17448
v  Velocity[Y]             -18.058          18.689         0.58105          0.4192
v  Velocity[Z]             -26.972          21.521        -0.53618      -0.0029078
v  ǁVelocityǁ            0.0026392          29.522          3.5103          3.6253
v  Pressure                 -30672           87495           54222           46456
v  k                     5.921e-07          3.5322        0.031727        0.022664
v  epsilon              0.00052159      4.6563e+05          591.16          21.039
v  TurbVisc             2.2558e-12          0.2163       0.0010288        0.013802
v  CourantNb              0.007666           10341          23.136          4.1389
v  FourierNb              0.022452      2.3655e+05          21.829         0.29335
v  total_pressure       4.6933e+05      5.8749e+05      5.5422e+05      5.4646e+05
v  Local Time Step           0.001         0.12844       0.0010112       0.0010534


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83939      2.3882e+05          44.965          4.4323


 TIME FOR THE TIME STEP              396:        0.67819E+02

===============================================================


 INSTANT    0.397000000E+01   TIME STEP NUMBER             397
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.131022463E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156390164E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25187E+02 0.40690E+01
   Friction velocity        uet   :  0.16818E-01 0.12640E+02
   Friction velocity        uk    :  0.16728E-01 0.12640E+02
   Dimensionless distance   yplus :  0.14974E-02 0.12195E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7319
   Nb of faces within the viscous sub-layer     :      16934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76399E+01      36   0.56688E-01   0.65038E+01 0.21087E+02 
c  Velocity[X]                                      0.13223E+01 
c  Velocity[Y]                                      0.21256E+01 
c  Velocity[Z]                                      0.30559E+01 
c  Pressure     0.37029E-01     267   0.24421E-01   0.79464E-01 0.52045E+00 
c  k            0.12567E+00      16   0.69179E-04   0.51339E-03 0.16594E+02 
c  epsilon      0.15537E+04      11   0.26949E-03   0.40330E+06 0.58512E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.5423e-05                             1
a  epsilon                 -4.5503                             2
a  Local Time Step      4.2275e-08                        277972


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -5.484          11.522          1.0836         0.17441
v  Velocity[Y]             -20.018          20.734         0.58309         0.41925
v  Velocity[Z]             -27.708          21.622        -0.53567      -0.0029839
v  ǁVelocityǁ            0.0025741          30.323          3.5107          3.6257
v  Pressure                 -30642           87473           54224           46452
v  k                    5.6622e-07          3.5792         0.03177        0.022671
v  epsilon              0.00049953      4.5376e+05          592.57          21.055
v  TurbVisc             1.9128e-12          0.2163       0.0010301        0.013803
v  CourantNb              0.017043           10671          23.119          4.1392
v  FourierNb              0.022452      2.3655e+05           21.83         0.29339
v  total_pressure       4.6936e+05      5.8747e+05      5.5422e+05      5.4645e+05
v  Local Time Step           0.001         0.14129       0.0010112       0.0010542


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54155      2.3909e+05          44.949          4.4326


 TIME FOR THE TIME STEP              397:        0.61649E+02

===============================================================


 INSTANT    0.398000000E+01   TIME STEP NUMBER             398
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.379635114E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156402575E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28004E+02 0.40725E+01
   Friction velocity        uet   :  0.28337E-01 0.14712E+02
   Friction velocity        uk    :  0.28182E-01 0.14712E+02
   Dimensionless distance   yplus :  0.18772E-02 0.12193E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7325
   Nb of faces within the viscous sub-layer     :      16943
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76389E+01      33   0.55397E-01   0.66036E+01 0.21260E+02 
c  Velocity[X]                                      0.13885E+01 
c  Velocity[Y]                                      0.21012E+01 
c  Velocity[Z]                                      0.31139E+01 
c  Pressure     0.36300E-01     236   0.23845E-01   0.77950E-01 0.45612E+00 
c  k            0.12570E+00      18   0.82013E-04   0.64257E-03 0.18588E+02 
c  epsilon      0.15565E+04      20   0.60341E-03   0.11793E+07 0.99761E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.6013e-05                             1
a  epsilon                 -5.1798                             5
a  Local Time Step      4.2275e-08                        277941


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4765          11.786          1.0831         0.17436
v  Velocity[Y]             -18.792          18.693         0.58516         0.41923
v  Velocity[Z]             -26.706          21.715        -0.53547      -0.0029834
v  ǁVelocityǁ            0.0017154          29.248          3.5108          3.6257
v  Pressure                 -30656           87441           54226           46453
v  k                    5.4054e-07          3.6443        0.031791        0.022678
v  epsilon              0.00047648      4.5674e+05          594.66          21.068
v  TurbVisc              2.038e-12          0.2163       0.0010314        0.013804
v  CourantNb              0.016972           10596          23.122          4.1398
v  FourierNb              0.022453      2.3655e+05           21.83         0.29321
v  total_pressure       4.6934e+05      5.8744e+05      5.5423e+05      5.4645e+05
v  Local Time Step           0.001        0.090445       0.0010111       0.0010519


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70194      2.3927e+05          44.952           4.433


 TIME FOR THE TIME STEP              398:        0.64490E+02

===============================================================


 INSTANT    0.399000000E+01   TIME STEP NUMBER             399
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.886108842E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156404640E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25349E+02 0.40808E+01
   Friction velocity        uet   :  0.32926E-01 0.11618E+02
   Friction velocity        uk    :  0.32415E-01 0.11618E+02
   Dimensionless distance   yplus :  0.14824E-02 0.12191E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7332
   Nb of faces within the viscous sub-layer     :      16939
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76391E+01      32   0.56528E-01   0.66028E+01 0.21249E+02 
c  Velocity[X]                                      0.13251E+01 
c  Velocity[Y]                                      0.20569E+01 
c  Velocity[Z]                                      0.32208E+01 
c  Pressure     0.36957E-01     393   0.24309E-01   0.79266E-01 0.51016E+00 
c  k            0.12571E+00      17   0.69172E-04   0.52190E-03 0.16810E+02 
c  epsilon      0.15560E+04      12   0.37587E-03   0.61546E+06 0.72235E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.3621e-05                             1
a  epsilon                 -4.4362                             3
a  Local Time Step      4.2275e-08                        277901


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4495          11.619          1.0839         0.17435
v  Velocity[Y]             -20.387          20.659         0.58659         0.41923
v  Velocity[Z]              -27.95          21.552        -0.53501      -0.0029214
v  ǁVelocityǁ            0.0023927           30.57          3.5114          3.6258
v  Pressure                 -30620           87438           54229           46461
v  k                    5.1874e-07          3.7158        0.031762        0.022684
v  epsilon              0.00045869      4.5982e+05          593.14          21.071
v  TurbVisc             1.9758e-12          0.2163       0.0010321        0.013804
v  CourantNb              0.032852           10572           23.12          4.1403
v  FourierNb              0.022454      2.3655e+05          21.831         0.29324
v  total_pressure       4.6938e+05      5.8744e+05      5.5423e+05      5.4646e+05
v  Local Time Step           0.001        0.094673       0.0010112       0.0010517


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65411      2.3906e+05          44.952          4.4335


 TIME FOR THE TIME STEP              399:        0.71959E+02

===============================================================


 INSTANT    0.400000000E+01   TIME STEP NUMBER             400
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.242224524E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156396570E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28432E+02 0.40800E+01
   Friction velocity        uet   :  0.36520E-01 0.14326E+02
   Friction velocity        uk    :  0.42483E-01 0.14326E+02
   Dimensionless distance   yplus :  0.15593E-02 0.12187E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7333
   Nb of faces within the viscous sub-layer     :      16943
   Total number of wall faces                   :      41000
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        400, Physical time    0.40000E+01


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint/main
 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                            
  Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary
 End writing


 Time for restart files:    0.33005E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.76389E+01      35   0.57352E-01   0.65842E+01 0.21213E+02 
c  Velocity[X]                                      0.13974E+01 
c  Velocity[Y]                                      0.20276E+01 
c  Velocity[Z]                                      0.31591E+01 
c  Pressure     0.36888E-01     409   0.24199E-01   0.79135E-01 0.48510E+00 
c  k            0.12571E+00      17   0.88742E-04   0.57347E-03 0.17631E+02 
c  epsilon      0.15533E+04      11   0.19512E-03   0.31400E+06 0.51668E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.3967e-05                             1
a  epsilon                 -5.1858                             2
a  Local Time Step      4.2275e-08                        277852


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4089          11.561          1.0849         0.17422
v  Velocity[Y]             -18.619          18.742         0.58751         0.41921
v  Velocity[Z]             -26.233          21.422        -0.53506      -0.0029905
v  ǁVelocityǁ            0.0030393          28.632          3.5123           3.626
v  Pressure                 -30587           87428           54235           46468
v  k                    4.9793e-07          3.7085         0.03177         0.02269
v  epsilon               0.0004417       4.587e+05          592.61          21.073
v  TurbVisc             2.0579e-12          0.2163       0.0010323        0.013805
v  CourantNb             0.0020669           10571          23.125          4.1407
v  FourierNb              0.022456      2.3655e+05          21.832         0.29327
v  total_pressure       4.6941e+05      5.8743e+05      5.5424e+05      5.4647e+05
v  Local Time Step           0.001         0.10414       0.0010113       0.0010519


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75596      2.4045e+05          44.957           4.434


 TIME FOR THE TIME STEP              400:        0.74177E+02

===============================================================


 INSTANT    0.401000000E+01   TIME STEP NUMBER             401
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.157430634E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156403891E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24567E+02 0.40635E+01
   Friction velocity        uet   :  0.34201E-01 0.12565E+02
   Friction velocity        uk    :  0.33666E-01 0.12565E+02
   Dimensionless distance   yplus :  0.14252E-02 0.12183E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7338
   Nb of faces within the viscous sub-layer     :      16943
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.77131E+01      40   0.55658E-01   0.10088E+04 0.21264E+03 
c  Velocity[X]                                      0.40485E+02 
c  Velocity[Y]                                      0.82320E+02 
c  Velocity[Z]                                      0.88599E+03 
c  Pressure     0.61592E-01    1595   0.66171E+00   0.13130E+00 0.79485E+03 
c  k            0.19723E+00      22   0.19258E-02   0.23468E+00 0.28693E+03 
c  epsilon      0.15559E+04      18   0.42350E-03   0.69072E+06 0.77721E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.5789e-05                             1
a  epsilon                 -4.8752                             4
a  Local Time Step      4.2275e-08                        277850


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.8584          14.624          1.2654         0.23151
v  Velocity[Y]              -22.58          21.716         0.80959         0.54485
v  Velocity[Z]             -31.142          23.048        -0.57862       0.0030917
v  ǁVelocityǁ            0.0056535          34.477          3.9158          4.5038
v  Pressure                 570.75      4.8439e+05      2.6135e+05      2.5011e+05
v  k                    4.7268e-07           3.623        0.032355        0.025447
v  epsilon               0.0004324      4.3083e+05          601.51          21.833
v  TurbVisc             1.9916e-12          0.2163       0.0010322        0.013806
v  CourantNb              0.023369           10898          23.114          4.1414
v  FourierNb              0.022459      2.3655e+05          21.831          0.2934
v  total_pressure       5.0057e+05      9.8439e+05      7.6135e+05      7.5011e+05
v  Local Time Step           0.001         0.11455       0.0010114       0.0010529


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69278      2.3875e+05          44.946          4.4348


 TIME FOR THE TIME STEP              401:        0.13444E+03

===============================================================


 INSTANT    0.402000000E+01   TIME STEP NUMBER             402
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.111035830E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221170942E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34734E+02 0.48614E+01
   Friction velocity        uet   :  0.30758E-01 0.27275E+02
   Friction velocity        uk    :  0.35050E-01 0.27275E+02
   Dimensionless distance   yplus :  0.30801E-02 0.13793E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8811
   Nb of faces within the viscous sub-layer     :      15943
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12024E+02      82   0.54138E-01   0.36721E+03 0.11611E+03 
c  Velocity[X]                                      0.29066E+02 
c  Velocity[Y]                                      0.50935E+02 
c  Velocity[Z]                                      0.28721E+03 
c  Pressure     0.32878E+00    1727   0.19695E+00   0.65581E+00 0.36528E+03 
c  k            0.23118E+00      27   0.87422E-03   0.14771E+00 0.19120E+03 
c  epsilon      0.24015E+04      22   0.55717E-02   0.12636E+09 0.65578E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020609                             5
a  epsilon                 -3.4946                             2
a  Local Time Step      4.2274e-08                        279520


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.0734          15.064          1.3682         0.25521
v  Velocity[Y]             -17.901          23.295          0.9271         0.61211
v  Velocity[Z]             -31.299          22.371        -0.55813        0.015109
v  ǁVelocityǁ            0.0075251          34.964          4.1241          4.9954
v  Pressure                  137.6      3.4329e+05      1.9669e+05      1.8059e+05
v  k                     4.352e-07          7.6298        0.039993        0.028792
v  epsilon              0.00041599      2.4592e+06          1102.4           27.48
v  TurbVisc             2.1088e-12         0.29781       0.0010881        0.015266
v  CourantNb              0.013533          5494.4           26.75          5.2524
v  FourierNb              0.022459      2.3655e+05          21.819         0.29141
v  total_pressure       5.0014e+05      8.4329e+05      6.9669e+05      6.8059e+05
v  Local Time Step           0.001        0.013688       0.0010029       0.0010167


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47903       2.406e+05          48.569          5.5438


 TIME FOR THE TIME STEP              402:        0.16060E+03

===============================================================


 INSTANT    0.403000000E+01   TIME STEP NUMBER             403
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.418768742E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221281873E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36325E+02 0.51346E+01
   Friction velocity        uet   :  0.34810E-01 0.36716E+02
   Friction velocity        uk    :  0.34475E-01 0.36716E+02
   Dimensionless distance   yplus :  0.41498E-02 0.14570E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9314
   Nb of faces within the viscous sub-layer     :      15607
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12278E+02      80   0.51937E-01   0.56145E+02 0.44784E+02 
c  Velocity[X]                                      0.13141E+02 
c  Velocity[Y]                                      0.23129E+02 
c  Velocity[Z]                                      0.19876E+02 
c  Pressure     0.15108E+00    2181   0.34351E+00   0.28015E+00 0.91392E+03 
c  k            0.24722E+00      19   0.63437E-03   0.70848E-01 0.12110E+03 
c  epsilon      0.23761E+04      24   0.35937E-02   0.80535E+08 0.64484E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00075493                            13
a  epsilon                 -19.083                            25
a  Local Time Step      4.2274e-08                        279304


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.1485          16.441          1.4007         0.25409
v  Velocity[Y]             -21.291          23.615         0.93142         0.61641
v  Velocity[Z]             -31.089          23.175        -0.57513        0.006912
v  ǁVelocityǁ             0.002772          36.526          4.2249          5.0578
v  Pressure                 -21031      1.6058e+05       1.065e+05           88291
v  k                    4.0808e-07          3.7781        0.038039        0.031037
v  epsilon              0.00040334      7.3711e+05          868.66          27.246
v  TurbVisc             2.1576e-12         0.32193         0.00112        0.016261
v  CourantNb              0.046879           19450          27.019          5.3189
v  FourierNb              0.022457      2.3655e+05          21.824         0.29252
v  total_pressure       4.7897e+05      6.6058e+05       6.065e+05      5.8829e+05
v  Local Time Step           0.001        0.015057       0.0010032        0.001017


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38339       2.514e+05          48.844          5.6114


 TIME FOR THE TIME STEP              403:        0.18481E+03

===============================================================


 INSTANT    0.404000000E+01   TIME STEP NUMBER             404
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.108030704E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221100985E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34212E+02 0.50027E+01
   Friction velocity        uet   :  0.30927E-01 0.40055E+02
   Friction velocity        uk    :  0.36172E-01 0.40055E+02
   Dimensionless distance   yplus :  0.44003E-02 0.15145E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9460
   Nb of faces within the viscous sub-layer     :      15361
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.11314E+02      74   0.56771E-01   0.59617E+02 0.46795E+02 
c  Velocity[X]                                      0.10085E+02 
c  Velocity[Y]                                      0.20098E+02 
c  Velocity[Z]                                      0.29433E+02 
c  Pressure     0.21258E+00    1472   0.21606E+00   0.37140E+00 0.44512E+03 
c  k            0.25937E+00      19   0.32901E-03   0.39778E-01 0.85268E+02 
c  epsilon      0.24075E+04      17   0.18767E-02   0.20683E+08 0.30479E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00033059                             3
a  epsilon                 -6.6016                             5
a  Local Time Step      4.2275e-08                        279109


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.4849           15.67          1.4062         0.24892
v  Velocity[Y]             -24.012          28.035         0.88266         0.60125
v  Velocity[Z]             -35.267          25.291        -0.59758      -0.0040389
v  ǁVelocityǁ            0.0041527          39.441          4.2756          4.9773
v  Pressure                 -58438      1.2621e+05           74085           56259
v  k                    3.8379e-07          4.6222        0.039912        0.032869
v  epsilon               0.0004086      1.1432e+06          972.02           28.31
v  TurbVisc             2.0994e-12         0.32553       0.0011339        0.017058
v  CourantNb              0.010303           19639          27.282           5.373
v  FourierNb              0.022453      2.3655e+05          21.825         0.29348
v  total_pressure       4.4156e+05      6.2621e+05      5.7409e+05      5.5626e+05
v  Local Time Step           0.001        0.016563       0.0010035       0.0010176


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50457      2.3763e+05          49.106          5.6665


 TIME FOR THE TIME STEP              404:        0.15105E+03

===============================================================


 INSTANT    0.405000000E+01   TIME STEP NUMBER             405
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.757851621E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221273170E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43515E+02 0.50701E+01
   Friction velocity        uet   :  0.31395E-01 0.38114E+02
   Friction velocity        uk    :  0.40394E-01 0.38114E+02
   Dimensionless distance   yplus :  0.41706E-02 0.15470E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9451
   Nb of faces within the viscous sub-layer     :      15158
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10721E+02      71   0.62412E-01   0.46510E+02 0.41679E+02 
c  Velocity[X]                                      0.86800E+01 
c  Velocity[Y]                                      0.17211E+02 
c  Velocity[Z]                                      0.20619E+02 
c  Pressure     0.16067E+00    1548   0.10769E+00   0.26699E+00 0.97781E+02 
c  k            0.26851E+00      18   0.22924E-03   0.27070E-01 0.67262E+02 
c  epsilon      0.25031E+04      18   0.16653E-02   0.26408E+08 0.32674E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.6832e-05                             1
a  epsilon                -0.26558                             2
a  Local Time Step      4.2275e-08                        279121


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3003          18.046          1.4117         0.24708
v  Velocity[Y]             -22.953           27.24         0.83596         0.59185
v  Velocity[Z]             -37.807          23.428        -0.60441      -0.0076028
v  ǁVelocityǁ            0.0025176          43.245          4.3198          4.9281
v  Pressure                 -54787      1.3378e+05           80680           63842
v  k                    3.6187e-07          5.8012         0.04092        0.034351
v  epsilon              0.00041349       2.165e+06          1029.9          28.846
v  TurbVisc             2.1193e-12         0.32612       0.0011615        0.017824
v  CourantNb            0.00056079           17190          27.782          5.4151
v  FourierNb               0.02245      2.3654e+05          21.828         0.29448
v  total_pressure       4.4521e+05      6.3378e+05      5.8068e+05      5.6384e+05
v  Local Time Step           0.001        0.018219       0.0010038       0.0010183


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46133      2.4446e+05           49.61          5.7096


 TIME FOR THE TIME STEP              405:        0.15456E+03

===============================================================


 INSTANT    0.406000000E+01   TIME STEP NUMBER             406
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.174246307E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221267806E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47016E+02 0.53918E+01
   Friction velocity        uet   :  0.31990E-01 0.35206E+02
   Friction velocity        uk    :  0.43556E-01 0.35206E+02
   Dimensionless distance   yplus :  0.43873E-02 0.15592E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9410
   Nb of faces within the viscous sub-layer     :      15012
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10650E+02      72   0.63135E-01   0.36693E+02 0.36934E+02 
c  Velocity[X]                                      0.78461E+01 
c  Velocity[Y]                                      0.15079E+02 
c  Velocity[Z]                                      0.13768E+02 
c  Pressure     0.11717E+00    1479   0.90177E-01   0.18696E+00 0.15542E+03 
c  k            0.27540E+00      18   0.16434E-03   0.19493E-01 0.55182E+02 
c  epsilon      0.25306E+04      18   0.13861E-02   0.21371E+08 0.28939E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.9882                             2
a  Local Time Step      4.2275e-08                        279150


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.3889          15.907          1.4228         0.24785
v  Velocity[Y]             -24.642          25.528           0.808          0.5916
v  Velocity[Z]             -36.931          24.301        -0.60057      -0.0052377
v  ǁVelocityǁ            0.0016594          40.641          4.3719          4.9348
v  Pressure                 -42856       1.488e+05           94403           77951
v  k                    3.4193e-07          4.4989        0.041759         0.03566
v  epsilon              0.00040974       1.068e+06          1064.7          29.372
v  TurbVisc             2.0352e-12         0.32636       0.0011878        0.018565
v  CourantNb              0.014843           14850          28.199          5.4494
v  FourierNb               0.02245      2.3655e+05          21.831         0.29543
v  total_pressure       4.5714e+05       6.488e+05       5.944e+05      5.7795e+05
v  Local Time Step           0.001        0.020041       0.0010041        0.001019


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48434      2.4144e+05           50.03          5.7448


 TIME FOR THE TIME STEP              406:        0.14195E+03

===============================================================


 INSTANT    0.407000000E+01   TIME STEP NUMBER             407
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.397791118E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221296523E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44863E+02 0.53752E+01
   Friction velocity        uet   :  0.31959E-01 0.34558E+02
   Friction velocity        uk    :  0.37732E-01 0.34558E+02
   Dimensionless distance   yplus :  0.44024E-02 0.15641E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9466
   Nb of faces within the viscous sub-layer     :      14887
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10782E+02      64   0.65100E-01   0.34552E+02 0.35576E+02 
c  Velocity[X]                                      0.68011E+01 
c  Velocity[Y]                                      0.13737E+02 
c  Velocity[Z]                                      0.14013E+02 
c  Pressure     0.10826E+00    1559   0.77074E-01   0.16670E+00 0.72122E+02 
c  k            0.28084E+00      18   0.13858E-03   0.15192E-01 0.47443E+02 
c  epsilon      0.25824E+04      21   0.88724E-03   0.13903E+08 0.22863E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.0454e-05                             1
a  epsilon               -0.019067                             2
a  Local Time Step      4.2274e-08                        279204


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.5295           17.56          1.4369         0.24852
v  Velocity[Y]             -25.609          30.007         0.79558         0.59447
v  Velocity[Z]             -39.641          25.416        -0.60042      -0.0025147
v  ǁVelocityǁ            0.0018293          44.564          4.4291          4.9637
v  Pressure                 -37159      1.5709e+05      1.0146e+05           84850
v  k                     3.262e-07          5.0244        0.043006        0.036843
v  epsilon              0.00039514      1.2094e+06            1120          30.019
v  TurbVisc              2.132e-12         0.32648       0.0012151        0.019269
v  CourantNb             0.0082062           14193          28.636          5.4839
v  FourierNb              0.022451      2.3655e+05          21.833         0.29647
v  total_pressure       4.6284e+05      6.5709e+05      6.0146e+05      5.8485e+05
v  Local Time Step           0.001        0.020639       0.0010042         0.00102


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47498      2.3911e+05          50.469          5.7804


 TIME FOR THE TIME STEP              407:        0.14932E+03

===============================================================


 INSTANT    0.408000000E+01   TIME STEP NUMBER             408
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.401812151E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221254277E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52789E+02 0.54084E+01
   Friction velocity        uet   :  0.19693E-01 0.32029E+02
   Friction velocity        uk    :  0.19471E-01 0.32029E+02
   Dimensionless distance   yplus :  0.40327E-02 0.15751E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9536
   Nb of faces within the viscous sub-layer     :      14755
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10889E+02      67   0.67624E-01   0.32782E+02 0.34476E+02 
c  Velocity[X]                                      0.60132E+01 
c  Velocity[Y]                                      0.13319E+02 
c  Velocity[Z]                                      0.13450E+02 
c  Pressure     0.10552E+00    1290   0.67068E-01   0.15739E+00 0.11989E+02 
c  k            0.28511E+00      19   0.12495E-03   0.12391E-01 0.41921E+02 
c  epsilon      0.26484E+04      13   0.70005E-03   0.10406E+08 0.19151E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0005403                             7
a  epsilon                 -4.8694                             9
a  Local Time Step      4.2274e-08                        279241


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.6373          15.678          1.4506         0.24867
v  Velocity[Y]             -26.226          27.501         0.79152         0.59625
v  Velocity[Z]             -36.186          25.542        -0.61212      -0.0020427
v  ǁVelocityǁ            0.0029916          39.055          4.4852          4.9893
v  Pressure                 -37452      1.5898e+05      1.0243e+05           85654
v  k                    3.1221e-07          5.6705         0.04409        0.037913
v  epsilon              0.00037852      1.1493e+06          1164.9            30.7
v  TurbVisc             2.1447e-12         0.32653       0.0012391        0.019925
v  CourantNb              0.026398           14250          29.123          5.5165
v  FourierNb              0.022454      2.3655e+05          21.835         0.29737
v  total_pressure       4.6255e+05      6.5898e+05      6.0243e+05      5.8565e+05
v  Local Time Step           0.001        0.018174       0.0010043       0.0010209


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6318      2.4293e+05          50.958          5.8139


 TIME FOR THE TIME STEP              408:        0.12261E+03

===============================================================


 INSTANT    0.409000000E+01   TIME STEP NUMBER             409
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.412357591E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221310184E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46734E+02 0.54576E+01
   Friction velocity        uet   :  0.20814E-01 0.28754E+02
   Friction velocity        uk    :  0.20368E-01 0.28754E+02
   Dimensionless distance   yplus :  0.35059E-02 0.15893E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9646
   Nb of faces within the viscous sub-layer     :      14649
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10925E+02      64   0.69836E-01   0.31850E+02 0.33865E+02 
c  Velocity[X]                                      0.60538E+01 
c  Velocity[Y]                                      0.13327E+02 
c  Velocity[Z]                                      0.12470E+02 
c  Pressure     0.10077E+00    1280   0.59873E-01   0.14642E+00 0.12683E+02 
c  k            0.28846E+00      17   0.13227E-03   0.99087E-02 0.36824E+02 
c  epsilon      0.26955E+04      14   0.17047E-02   0.99659E+07 0.18441E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00040764                             2
a  epsilon                -0.51088                             2
a  Local Time Step      4.2273e-08                        279335


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.7339          17.105          1.4606         0.24809
v  Velocity[Y]             -24.934          28.379         0.79132         0.59692
v  Velocity[Z]              -40.88          26.721        -0.63211      -0.0026699
v  ǁVelocityǁ            0.0033618          45.282          4.5376          5.0054
v  Pressure                 -39703      1.5837e+05      1.0113e+05           84432
v  k                    2.9959e-07          6.4458        0.044958        0.038867
v  epsilon              0.00035857      1.1977e+06          1188.9          31.273
v  TurbVisc             2.9073e-12         0.32656        0.001265        0.020528
v  CourantNb              0.033482           13649          29.602          5.5465
v  FourierNb              0.022457      2.3656e+05          21.838         0.29822
v  total_pressure        4.603e+05      6.5837e+05      6.0113e+05      5.8443e+05
v  Local Time Step           0.001        0.018086       0.0010044        0.001022


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51806       2.462e+05          51.441          5.8447


 TIME FOR THE TIME STEP              409:        0.13334E+03

===============================================================


 INSTANT    0.410000000E+01   TIME STEP NUMBER             410
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.381668563E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221247391E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45817E+02 0.54733E+01
   Friction velocity        uet   :  0.37429E-01 0.28431E+02
   Friction velocity        uk    :  0.45947E-01 0.28431E+02
   Dimensionless distance   yplus :  0.36278E-02 0.15966E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9710
   Nb of faces within the viscous sub-layer     :      14534
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10923E+02      75   0.73235E-01   0.31819E+02 0.33734E+02 
c  Velocity[X]                                      0.59163E+01 
c  Velocity[Y]                                      0.13332E+02 
c  Velocity[Z]                                      0.12571E+02 
c  Pressure     0.99294E-01     889   0.56334E-01   0.14138E+00 0.50105E+01 
c  k            0.29111E+00      21   0.11929E-03   0.86603E-02 0.34029E+02 
c  epsilon      0.27730E+04      25   0.13967E-02   0.14982E+08 0.21915E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00032468                             2
a  epsilon        
a  Local Time Step      4.2275e-08                        279391


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5.8563          14.895          1.4675         0.24751
v  Velocity[Y]             -27.604          29.611         0.79288         0.59718
v  Velocity[Z]             -36.915          28.517        -0.65583      -0.0039705
v  ǁVelocityǁ            0.0027362          39.826          4.5875          5.0161
v  Pressure                 -41892      1.5842e+05      1.0062e+05           84091
v  k                     2.898e-07          7.0823        0.046242        0.039708
v  epsilon              0.00034144      1.1859e+06          1255.3          31.868
v  TurbVisc             2.1705e-12         0.32657       0.0012879         0.02108
v  CourantNb              0.016162           12763          30.034          5.5731
v  FourierNb               0.02246      2.3655e+05          21.839          0.2991
v  total_pressure       4.5811e+05      6.5842e+05      6.0062e+05      5.8409e+05
v  Local Time Step           0.001        0.019895       0.0010045       0.0010231


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47293      2.4617e+05          51.872          5.8722


 TIME FOR THE TIME STEP              410:        0.10771E+03

===============================================================


 INSTANT    0.411000000E+01   TIME STEP NUMBER             411
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.620357392E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221378473E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.48822E+02 0.55056E+01
   Friction velocity        uet   :  0.34830E-01 0.30835E+02
   Friction velocity        uk    :  0.45597E-01 0.30835E+02
   Dimensionless distance   yplus :  0.29037E-02 0.16001E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9802
   Nb of faces within the viscous sub-layer     :      14422
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10920E+02      63   0.73162E-01   0.30831E+02 0.33151E+02 
c  Velocity[X]                                      0.56591E+01 
c  Velocity[Y]                                      0.12770E+02 
c  Velocity[Z]                                      0.12402E+02 
c  Pressure     0.95382E-01     662   0.52660E-01   0.13343E+00 0.40450E+01 
c  k            0.29321E+00      18   0.97843E-04   0.77460E-02 0.31852E+02 
c  epsilon      0.28330E+04      19   0.85351E-03   0.15657E+08 0.22015E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0015781                             5
a  epsilon                 -13.518                             4
a  Local Time Step      4.2274e-08                        279483


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.1078          16.601          1.4735         0.24709
v  Velocity[Y]             -25.768          30.161         0.79438         0.59709
v  Velocity[Z]             -39.993          30.198        -0.67884       -0.004401
v  ǁVelocityǁ            0.0023346          44.063          4.6354          5.0255
v  Pressure                 -43584      1.5874e+05      1.0053e+05           84214
v  k                    2.8477e-07          7.3729        0.046938        0.040451
v  epsilon              0.00033079      1.2077e+06          1282.7          32.369
v  TurbVisc             2.5359e-12         0.32657       0.0013081        0.021587
v  CourantNb              0.033016           12011          30.476          5.5982
v  FourierNb              0.022462      2.3655e+05           21.84         0.29973
v  total_pressure       4.5642e+05      6.5874e+05      6.0053e+05      5.8421e+05
v  Local Time Step           0.001        0.021513       0.0010045       0.0010239


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65236      2.4781e+05          52.316          5.8979


 TIME FOR THE TIME STEP              411:        0.83394E+02

===============================================================


 INSTANT    0.412000000E+01   TIME STEP NUMBER             412
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.502649937E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221321906E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50885E+02 0.55300E+01
   Friction velocity        uet   :  0.38226E-01 0.35719E+02
   Friction velocity        uk    :  0.42507E-01 0.35719E+02
   Dimensionless distance   yplus :  0.33295E-02 0.16016E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9867
   Nb of faces within the viscous sub-layer     :      14317
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10922E+02      70   0.72498E-01   0.29259E+02 0.32231E+02 
c  Velocity[X]                                      0.53864E+01 
c  Velocity[Y]                                      0.11575E+02 
c  Velocity[Z]                                      0.12298E+02 
c  Pressure     0.93452E-01     747   0.50942E-01   0.12891E+00 0.37849E+01 
c  k            0.29492E+00      17   0.10262E-03   0.70633E-02 0.30155E+02 
c  epsilon      0.29015E+04      19   0.69278E-03   0.11719E+08 0.18678E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.5181e-05                             1
a  epsilon        
a  Local Time Step      4.2274e-08                        279603


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.1182          14.843          1.4766         0.24692
v  Velocity[Y]             -25.424          29.652         0.79439         0.59671
v  Velocity[Z]             -36.162          30.166        -0.69995      -0.0035587
v  ǁVelocityǁ            0.0021276          38.874           4.678          5.0331
v  Pressure                 -45140      1.5902e+05      1.0048e+05           84353
v  k                    4.0142e-08           7.524        0.047852        0.041116
v  epsilon              0.00032606      1.2119e+06          1325.1           32.83
v  TurbVisc             2.9419e-12         0.32658       0.0013264        0.022051
v  CourantNb              0.033437           11751          30.911          5.6207
v  FourierNb              0.022465      2.3655e+05          21.841         0.30031
v  total_pressure       4.5486e+05      6.5902e+05      6.0048e+05      5.8435e+05
v  Local Time Step           0.001        0.023665       0.0010046       0.0010248


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5668      2.4804e+05          52.751          5.9211


 TIME FOR THE TIME STEP              412:        0.95648E+02

===============================================================


 INSTANT    0.413000000E+01   TIME STEP NUMBER             413
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.224789771E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221195595E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47120E+02 0.55423E+01
   Friction velocity        uet   :  0.39328E-01 0.34617E+02
   Friction velocity        uk    :  0.39425E-01 0.34617E+02
   Dimensionless distance   yplus :  0.18310E-02 0.16023E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9918
   Nb of faces within the viscous sub-layer     :      14179
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10922E+02      61   0.73745E-01   0.29697E+02 0.32404E+02 
c  Velocity[X]                                      0.53301E+01 
c  Velocity[Y]                                      0.11697E+02 
c  Velocity[Z]                                      0.12669E+02 
c  Pressure     0.94381E-01    1411   0.49810E-01   0.12849E+00 0.84913E+01 
c  k            0.29631E+00      20   0.12133E-03   0.61639E-02 0.27988E+02 
c  epsilon      0.29698E+04      22   0.99965E-03   0.14315E+08 0.20131E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                -0.12205                             1
a  Local Time Step      4.2274e-08                        279682


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.2723          16.408          1.4778         0.24725
v  Velocity[Y]             -26.473          32.034         0.79352         0.59687
v  Velocity[Z]             -40.496          26.636        -0.71876      -0.0032816
v  ǁVelocityǁ            0.0025965          44.476          4.7191          5.0423
v  Pressure                 -45780      1.6018e+05      1.0128e+05           85132
v  k                    7.9689e-08          7.4232        0.048622        0.041712
v  epsilon              0.00032652       1.217e+06          1376.5          33.228
v  TurbVisc              2.695e-12         0.32658       0.0013431        0.022476
v  CourantNb             0.0085452           12059          31.278          5.6402
v  FourierNb              0.022467      2.3655e+05          21.843         0.30088
v  total_pressure       4.5422e+05      6.6018e+05      6.0128e+05      5.8513e+05
v  Local Time Step           0.001        0.026031       0.0010046       0.0010257


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5727      2.4861e+05          53.121          5.9411


 TIME FOR THE TIME STEP              413:        0.12291E+03

===============================================================


 INSTANT    0.414000000E+01   TIME STEP NUMBER             414
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.236639347E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221255600E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52017E+02 0.55919E+01
   Friction velocity        uet   :  0.27647E-01 0.36975E+02
   Friction velocity        uk    :  0.41454E-01 0.36975E+02
   Dimensionless distance   yplus :  0.42672E-02 0.16026E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9981
   Nb of faces within the viscous sub-layer     :      14086
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10928E+02      67   0.72490E-01   0.30342E+02 0.32726E+02 
c  Velocity[X]                                      0.57335E+01 
c  Velocity[Y]                                      0.11981E+02 
c  Velocity[Z]                                      0.12628E+02 
c  Pressure     0.96461E-01    1019   0.49700E-01   0.12990E+00 0.35642E+01 
c  k            0.29750E+00      17   0.95411E-04   0.51053E-02 0.25316E+02 
c  epsilon      0.30485E+04      16   0.73206E-03   0.14135E+08 0.19677E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon        
a  Local Time Step      4.2272e-08                        279755


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.2025           15.02          1.4802         0.24759
v  Velocity[Y]             -28.402          29.726         0.79265          0.5974
v  Velocity[Z]             -35.968          27.031        -0.73632      -0.0033581
v  ǁVelocityǁ            0.0041209          39.004          4.7543          5.0498
v  Pressure                 -46884      1.6073e+05      1.0157e+05           85372
v  k                    2.9727e-07           6.961        0.049195        0.042257
v  epsilon              0.00033114      1.5777e+06          1418.9          33.594
v  TurbVisc             2.6575e-12         0.32658       0.0013581        0.022865
v  CourantNb              0.014257           14527          31.665          5.6605
v  FourierNb              0.022469      2.3656e+05          21.843         0.30152
v  total_pressure       4.5312e+05      6.6073e+05      6.0157e+05      5.8537e+05
v  Local Time Step           0.001        0.028634       0.0010045       0.0010263


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64929      2.5109e+05          53.509           5.962


 TIME FOR THE TIME STEP              414:        0.99644E+02

===============================================================


 INSTANT    0.415000000E+01   TIME STEP NUMBER             415
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.400803342E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221184739E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46712E+02 0.56154E+01
   Friction velocity        uet   :  0.29567E-01 0.38706E+02
   Friction velocity        uk    :  0.28532E-01 0.38706E+02
   Dimensionless distance   yplus :  0.47476E-02 0.16027E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10031
   Nb of faces within the viscous sub-layer     :      13957
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10929E+02      68   0.72307E-01   0.30763E+02 0.32912E+02 
c  Velocity[X]                                      0.58270E+01 
c  Velocity[Y]                                      0.11870E+02 
c  Velocity[Z]                                      0.13066E+02 
c  Pressure     0.92324E-01     614   0.46888E-01   0.12341E+00 0.21814E+01 
c  k            0.29850E+00      21   0.94108E-04   0.53417E-02 0.25704E+02 
c  epsilon      0.31139E+04      18   0.93587E-03   0.24287E+08 0.25091E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0024267                             5
a  epsilon                 -35.172                             4
a  Local Time Step      4.2272e-08                        279782


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.3516           16.19          1.4829         0.24783
v  Velocity[Y]             -27.009          30.618         0.79212         0.59738
v  Velocity[Z]             -40.441          26.003        -0.75043      -0.0033532
v  ǁVelocityǁ            0.0020829          44.365          4.7867          5.0565
v  Pressure                 -48144      1.6091e+05      1.0158e+05           85373
v  k                    3.1374e-07          6.7106        0.050027        0.042753
v  epsilon              0.00034059      1.6513e+06          1461.1          33.985
v  TurbVisc             3.1938e-12         0.32658       0.0013731        0.023221
v  CourantNb             0.0058369           14672          31.967          5.6762
v  FourierNb              0.022471      2.3656e+05          21.845           0.302
v  total_pressure       4.5186e+05      6.6091e+05      6.0158e+05      5.8537e+05
v  Local Time Step           0.001        0.031498       0.0010045       0.0010268


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48853      2.5124e+05          53.812          5.9782


 TIME FOR THE TIME STEP              415:        0.10211E+03

===============================================================


 INSTANT    0.416000000E+01   TIME STEP NUMBER             416
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.401736668E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221141066E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52093E+02 0.56834E+01
   Friction velocity        uet   :  0.25977E-01 0.42337E+02
   Friction velocity        uk    :  0.27778E-01 0.42337E+02
   Dimensionless distance   yplus :  0.54023E-02 0.16027E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10095
   Nb of faces within the viscous sub-layer     :      13870
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10927E+02      54   0.74853E-01   0.31286E+02 0.33173E+02 
c  Velocity[X]                                      0.62209E+01 
c  Velocity[Y]                                      0.12291E+02 
c  Velocity[Z]                                      0.12774E+02 
c  Pressure     0.93678E-01     522   0.46968E-01   0.12463E+00 0.20711E+01 
c  k            0.29940E+00      20   0.81417E-04   0.45146E-02 0.23476E+02 
c  epsilon      0.31410E+04      15   0.61514E-03   0.14317E+08 0.19360E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019119                             2
a  epsilon              -0.0023435                             1
a  Local Time Step      4.2272e-08                        279862


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.3411           15.25           1.488         0.24769
v  Velocity[Y]             -25.252          25.817         0.79134         0.59682
v  Velocity[Z]             -37.363          26.279        -0.75994      -0.0028683
v  ǁVelocityǁ            0.0042162           41.16          4.8141          5.0625
v  Pressure                 -49410      1.6104e+05      1.0161e+05           85389
v  k                    3.3556e-07           6.526        0.050389        0.043214
v  epsilon              0.00035316      1.3009e+06          1469.2          34.297
v  TurbVisc             2.9661e-12         0.32658       0.0013885        0.023545
v  CourantNb              0.002883           12286          32.262          5.6917
v  FourierNb              0.022473      2.3657e+05          21.847         0.30246
v  total_pressure       4.5059e+05      6.6104e+05      6.0161e+05      5.8539e+05
v  Local Time Step           0.001        0.034648       0.0010044       0.0010274


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58594      2.4885e+05          54.109          5.9941


 TIME FOR THE TIME STEP              416:        0.75597E+02

===============================================================


 INSTANT    0.417000000E+01   TIME STEP NUMBER             417
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.276213129E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221073487E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40961E+02 0.55727E+01
   Friction velocity        uet   :  0.30457E-01 0.46461E+02
   Friction velocity        uk    :  0.48277E-01 0.46461E+02
   Dimensionless distance   yplus :  0.47998E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10121
   Nb of faces within the viscous sub-layer     :      13732
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10924E+02      60   0.73427E-01   0.31703E+02 0.33353E+02 
c  Velocity[X]                                      0.61917E+01 
c  Velocity[Y]                                      0.13136E+02 
c  Velocity[Z]                                      0.12375E+02 
c  Pressure     0.95106E-01     789   0.47195E-01   0.12614E+00 0.36215E+01 
c  k            0.30015E+00      18   0.11191E-03   0.51219E-02 0.24974E+02 
c  epsilon      0.31463E+04      17   0.97372E-03   0.12932E+08 0.18195E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0636e-05                             1
a  epsilon                 -10.258                             4
a  Local Time Step      4.2272e-08                        279966


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.4271          16.159          1.4926         0.24741
v  Velocity[Y]             -24.219          33.737         0.79063         0.59632
v  Velocity[Z]             -40.387          26.406        -0.76646      -0.0024117
v  ǁVelocityǁ            0.0040093          44.343          4.8371          5.0684
v  Pressure                 -50305      1.6155e+05      1.0199e+05           85685
v  k                    3.6254e-07           6.632        0.051269        0.043639
v  epsilon              0.00037278      1.2112e+06          1490.9          34.678
v  TurbVisc             3.4917e-12         0.32658       0.0014045         0.02384
v  CourantNb              0.039176           13275          32.516          5.7052
v  FourierNb              0.022477      2.3657e+05          21.848         0.30288
v  total_pressure        4.497e+05      6.6155e+05      6.0199e+05      5.8569e+05
v  Local Time Step           0.001        0.038112       0.0010043       0.0010277


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69739      2.4751e+05          54.364           6.008


 TIME FOR THE TIME STEP              417:        0.95364E+02

===============================================================


 INSTANT    0.418000000E+01   TIME STEP NUMBER             418
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.411034136E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221029348E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51329E+02 0.55836E+01
   Friction velocity        uet   :  0.30765E-01 0.49061E+02
   Friction velocity        uk    :  0.37953E-01 0.49061E+02
   Dimensionless distance   yplus :  0.40378E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10173
   Nb of faces within the viscous sub-layer     :      13625
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10926E+02      53   0.72624E-01   0.31643E+02 0.33316E+02 
c  Velocity[X]                                      0.60912E+01 
c  Velocity[Y]                                      0.13672E+02 
c  Velocity[Z]                                      0.11880E+02 
c  Pressure     0.95885E-01     766   0.48183E-01   0.12691E+00 0.45754E+01 
c  k            0.30078E+00      17   0.94675E-04   0.46081E-02 0.23701E+02 
c  epsilon      0.31710E+04      16   0.71543E-03   0.11115E+08 0.16752E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.3761e-06                             2
a  epsilon                 -2.0397                             1
a  Local Time Step      4.2272e-08                        280078


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7764          15.559          1.4982          0.2469
v  Velocity[Y]             -27.637          26.984         0.79052         0.59605
v  Velocity[Z]             -39.427          27.179        -0.76821      -0.0025321
v  ǁVelocityǁ            0.0046629          43.252          4.8525          5.0744
v  Pressure                 -51026      1.6222e+05      1.0255e+05           86112
v  k                    3.9423e-07          6.7393        0.051726        0.044025
v  epsilon              0.00039453      1.2392e+06            1506          34.975
v  TurbVisc              3.948e-13         0.32658       0.0014207        0.024109
v  CourantNb              0.011279           13200          32.729          5.7174
v  FourierNb              0.022482      2.3657e+05           21.85         0.30333
v  total_pressure       4.4897e+05      6.6222e+05      6.0255e+05      5.8611e+05
v  Local Time Step           0.001        0.041924       0.0010043       0.0010285


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62751      2.4596e+05          54.579          6.0208


 TIME FOR THE TIME STEP              418:        0.91004E+02

===============================================================


 INSTANT    0.419000000E+01   TIME STEP NUMBER             419
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.140827592E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221068061E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41938E+02 0.55820E+01
   Friction velocity        uet   :  0.22984E-01 0.48454E+02
   Friction velocity        uk    :  0.36531E-01 0.48454E+02
   Dimensionless distance   yplus :  0.19182E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10197
   Nb of faces within the viscous sub-layer     :      13528
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10933E+02      59   0.74431E-01   0.31776E+02 0.33317E+02 
c  Velocity[X]                                      0.60297E+01 
c  Velocity[Y]                                      0.14026E+02 
c  Velocity[Z]                                      0.11720E+02 
c  Pressure     0.96991E-01     463   0.48330E-01   0.12807E+00 0.18699E+01 
c  k            0.30127E+00      19   0.85199E-04   0.46031E-02 0.23627E+02 
c  epsilon      0.31963E+04      18   0.58398E-03   0.92677E+07 0.15199E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.4933e-05                             2
a  epsilon                 -6.4083                             5
a  Local Time Step      4.2272e-08                        280151


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8594          16.297          1.5024         0.24654
v  Velocity[Y]             -26.656          36.025         0.79094         0.59584
v  Velocity[Z]             -40.857          28.062        -0.76548       -0.002297
v  ǁVelocityǁ            0.0046816           45.28          4.8621          5.0796
v  Pressure                 -52120      1.6231e+05      1.0258e+05           86102
v  k                    1.1935e-07           6.844        0.052315        0.044369
v  epsilon              0.00042541      1.2379e+06          1524.6          35.221
v  TurbVisc             2.3197e-12         0.32658       0.0014374        0.024352
v  CourantNb              0.033071           14051          32.861           5.728
v  FourierNb              0.022489      2.3657e+05          21.851          0.3037
v  total_pressure       4.4788e+05      6.6231e+05      6.0258e+05       5.861e+05
v  Local Time Step           0.001        0.046116       0.0010042       0.0010286


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70992      2.4614e+05          54.712          6.0317


 TIME FOR THE TIME STEP              419:        0.88198E+02

===============================================================


 INSTANT    0.420000000E+01   TIME STEP NUMBER             420
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.153516291E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221063008E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55894E+02 0.55328E+01
   Friction velocity        uet   :  0.33023E-01 0.46637E+02
   Friction velocity        uk    :  0.32835E-01 0.46637E+02
   Dimensionless distance   yplus :  0.39020E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10239
   Nb of faces within the viscous sub-layer     :      13437
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10934E+02      54   0.75541E-01   0.32195E+02 0.33545E+02 
c  Velocity[X]                                      0.59419E+01 
c  Velocity[Y]                                      0.14631E+02 
c  Velocity[Z]                                      0.11623E+02 
c  Pressure     0.10142E+00     946   0.50537E-01   0.13361E+00 0.34205E+01 
c  k            0.30168E+00      18   0.69475E-04   0.37076E-02 0.21143E+02 
c  epsilon      0.32047E+04      15   0.57458E-03   0.59102E+07 0.12119E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.5059e-06                             1
a  epsilon                 -6.8023                             3
a  Local Time Step      4.2271e-08                        280216


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9624          14.964          1.5044         0.24643
v  Velocity[Y]              -26.47          33.298         0.79274         0.59543
v  Velocity[Z]             -39.284          27.453        -0.76352      -0.0025727
v  ǁVelocityǁ            0.0045721          42.869           4.868          5.0851
v  Pressure                 -52658      1.6268e+05      1.0297e+05           86395
v  k                    4.9366e-07           6.848        0.052657        0.044675
v  epsilon              0.00046395       1.199e+06          1534.2          35.411
v  TurbVisc             8.9075e-14         0.32658        0.001455        0.024571
v  CourantNb               0.03118           15013          32.917           5.736
v  FourierNb              0.022498      2.3657e+05          21.852         0.30406
v  total_pressure       4.4734e+05      6.6268e+05      6.0297e+05       5.864e+05
v  Local Time Step           0.001        0.050728       0.0010042       0.0010292


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52771      2.4563e+05           54.77            6.04


 TIME FOR THE TIME STEP              420:        0.96876E+02

===============================================================


 INSTANT    0.421000000E+01   TIME STEP NUMBER             421
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.408261086E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221131256E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49384E+02 0.55469E+01
   Friction velocity        uet   :  0.37641E-01 0.43167E+02
   Friction velocity        uk    :  0.45095E-01 0.43167E+02
   Dimensionless distance   yplus :  0.29457E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10271
   Nb of faces within the viscous sub-layer     :      13357
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10940E+02      53   0.75924E-01   0.31247E+02 0.33013E+02 
c  Velocity[X]                                      0.58770E+01 
c  Velocity[Y]                                      0.14042E+02 
c  Velocity[Z]                                      0.11328E+02 
c  Pressure     0.10218E+00     470   0.51101E-01   0.13436E+00 0.18779E+01 
c  k            0.30198E+00      19   0.74103E-04   0.35623E-02 0.20693E+02 
c  epsilon      0.32220E+04      13   0.44912E-03   0.51766E+07 0.11283E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00037143                             2
a  epsilon                 -5.5002                             5
a  Local Time Step      4.2271e-08                        280323


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9954          16.136          1.5056         0.24632
v  Velocity[Y]             -24.894          32.961         0.79582         0.59484
v  Velocity[Z]             -41.469          27.419        -0.75773      -0.0023801
v  ǁVelocityǁ            0.0030908          45.879          4.8699          5.0899
v  Pressure                 -53477       1.627e+05      1.0298e+05           86391
v  k                    5.6295e-07          6.9701        0.052973        0.044943
v  epsilon              0.00050799      1.2243e+06            1541          35.572
v  TurbVisc             3.4648e-12         0.32658       0.0014721        0.024768
v  CourantNb              0.025861           15421          32.943          5.7436
v  FourierNb               0.02251      2.3657e+05          21.856         0.30434
v  total_pressure       4.4652e+05       6.627e+05      6.0298e+05      5.8639e+05
v  Local Time Step           0.001          0.0558       0.0010042       0.0010295


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64319      2.4769e+05          54.798          6.0479


 TIME FOR THE TIME STEP              421:        0.70167E+02

===============================================================


 INSTANT    0.422000000E+01   TIME STEP NUMBER             422
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.105381145E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221138874E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57198E+02 0.55270E+01
   Friction velocity        uet   :  0.18719E-01 0.37469E+02
   Friction velocity        uk    :  0.18592E-01 0.37469E+02
   Dimensionless distance   yplus :  0.34649E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10327
   Nb of faces within the viscous sub-layer     :      13308
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10944E+02      59   0.75218E-01   0.31493E+02 0.33123E+02 
c  Velocity[X]                                      0.59128E+01 
c  Velocity[Y]                                      0.14163E+02 
c  Velocity[Z]                                      0.11418E+02 
c  Pressure     0.10369E+00     491   0.51514E-01   0.13599E+00 0.19143E+01 
c  k            0.30224E+00      18   0.72558E-04   0.34489E-02 0.20308E+02 
c  epsilon      0.32233E+04      14   0.34189E-03   0.32043E+07 0.88970E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003153                             1
a  epsilon                 -5.1562                             3
a  Local Time Step      4.2272e-08                        280387


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0943          14.286          1.5057         0.24622
v  Velocity[Y]             -25.756          31.352         0.80257          0.5946
v  Velocity[Z]             -38.156           27.45        -0.75142      -0.0021323
v  ǁVelocityǁ            0.0034464          41.548          4.8717          5.0939
v  Pressure                 -54067      1.6269e+05      1.0299e+05           86406
v  k                    6.4994e-07          7.1167        0.053153        0.045179
v  epsilon               0.0005751       1.198e+06            1542          35.669
v  TurbVisc             3.0606e-12         0.32658       0.0014879        0.024944
v  CourantNb              0.014758           16014           32.88          5.7503
v  FourierNb              0.022524      2.3656e+05          21.857         0.30458
v  total_pressure       4.4593e+05      6.6269e+05      6.0299e+05      5.8641e+05
v  Local Time Step           0.001         0.06138       0.0010041       0.0010295


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45429      2.4929e+05          54.737          6.0549


 TIME FOR THE TIME STEP              422:        0.75377E+02

===============================================================


 INSTANT    0.423000000E+01   TIME STEP NUMBER             423
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.317665687E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221139007E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46774E+02 0.55872E+01
   Friction velocity        uet   :  0.15283E-01 0.33696E+02
   Friction velocity        uk    :  0.15537E-01 0.33696E+02
   Dimensionless distance   yplus :  0.42996E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10368
   Nb of faces within the viscous sub-layer     :      13241
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10948E+02      58   0.75756E-01   0.31297E+02 0.33001E+02 
c  Velocity[X]                                      0.58721E+01 
c  Velocity[Y]                                      0.14041E+02 
c  Velocity[Z]                                      0.11383E+02 
c  Pressure     0.99624E-01     601   0.49502E-01   0.13056E+00 0.18591E+01 
c  k            0.30246E+00      15   0.90257E-04   0.41560E-02 0.22033E+02 
c  epsilon      0.32418E+04      17   0.44833E-03   0.64834E+07 0.12524E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -3.2316                             4
a  Local Time Step      4.2271e-08                        280457


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0436          15.757           1.505         0.24614
v  Velocity[Y]             -26.481          28.079          0.8116         0.59482
v  Velocity[Z]             -41.404          27.449        -0.74519      -0.0021566
v  ǁVelocityǁ             0.003948          45.501          4.8767          5.0977
v  Pressure                 -54563      1.6269e+05      1.0299e+05           86431
v  k                    7.5006e-07          7.1489        0.053457        0.045389
v  epsilon               0.0006731      1.2518e+06            1557          35.782
v  TurbVisc             3.2133e-12         0.32658       0.0014996        0.025102
v  CourantNb              0.024527           16998          32.834          5.7556
v  FourierNb              0.022539      2.3657e+05          21.858         0.30492
v  total_pressure       4.4544e+05      6.6269e+05      6.0299e+05      5.8643e+05
v  Local Time Step           0.001        0.067518       0.0010041       0.0010302


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65921      2.4949e+05          54.692          6.0605


 TIME FOR THE TIME STEP              423:        0.87057E+02

===============================================================


 INSTANT    0.424000000E+01   TIME STEP NUMBER             424
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.271072367E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221143819E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56930E+02 0.55738E+01
   Friction velocity        uet   :  0.29843E-01 0.31008E+02
   Friction velocity        uk    :  0.29749E-01 0.31008E+02
   Dimensionless distance   yplus :  0.39567E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10380
   Nb of faces within the viscous sub-layer     :      13233
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10952E+02      48   0.75939E-01   0.31564E+02 0.33109E+02 
c  Velocity[X]                                      0.58660E+01 
c  Velocity[Y]                                      0.14520E+02 
c  Velocity[Z]                                      0.11178E+02 
c  Pressure     0.98677E-01     511   0.48645E-01   0.12897E+00 0.19120E+01 
c  k            0.30270E+00      18   0.76848E-04   0.34029E-02 0.20149E+02 
c  epsilon      0.32371E+04      11   0.35497E-03   0.44325E+07 0.10410E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00048458                             3
a  epsilon                 -4.7328                             6
a  Local Time Step      4.2272e-08                        280527


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1524          14.207          1.5036         0.24597
v  Velocity[Y]             -29.917          29.018         0.81966         0.59476
v  Velocity[Z]             -38.209          27.204        -0.73897      -0.0025295
v  ǁVelocityǁ            0.0046684          41.584          4.8856          5.1013
v  Pressure                 -54940      1.6277e+05      1.0298e+05           86485
v  k                    8.7717e-07          7.1832         0.05345        0.045575
v  epsilon              0.00075499      1.2197e+06          1547.9          35.858
v  TurbVisc             3.0923e-12         0.32658        0.001508        0.025243
v  CourantNb             0.0082541           18018          32.834          5.7612
v  FourierNb              0.022553      2.3656e+05          21.857         0.30509
v  total_pressure       4.4506e+05      6.6277e+05      6.0298e+05      5.8649e+05
v  Local Time Step           0.001         0.07427       0.0010041       0.0010303


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49593      2.4803e+05          54.691          6.0663


 TIME FOR THE TIME STEP              424:        0.86416E+02

===============================================================


 INSTANT    0.425000000E+01   TIME STEP NUMBER             425
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.461258568E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221173830E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43539E+02 0.55761E+01
   Friction velocity        uet   :  0.29984E-01 0.29732E+02
   Friction velocity        uk    :  0.29875E-01 0.29732E+02
   Dimensionless distance   yplus :  0.37938E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10402
   Nb of faces within the viscous sub-layer     :      13187
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10957E+02      50   0.76722E-01   0.32364E+02 0.33510E+02 
c  Velocity[X]                                      0.60491E+01 
c  Velocity[Y]                                      0.14655E+02 
c  Velocity[Z]                                      0.11660E+02 
c  Pressure     0.96847E-01     519   0.48109E-01   0.12654E+00 0.19411E+01 
c  k            0.30283E+00      18   0.69741E-04   0.30742E-02 0.19159E+02 
c  epsilon      0.32478E+04      15   0.69531E-03   0.11086E+08 0.16267E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021938                             2
a  epsilon                 -3.3807                             4
a  Local Time Step      4.2272e-08                        280560


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1508          15.224          1.5024         0.24586
v  Velocity[Y]             -24.951          28.473          0.8251         0.59452
v  Velocity[Z]             -41.134          27.731        -0.73378      -0.0030714
v  ǁVelocityǁ            0.0054142          44.914          4.8961          5.1049
v  Pressure                 -55160      1.6289e+05      1.0294e+05           86549
v  k                    1.0269e-06          7.2212        0.053701        0.045737
v  epsilon              0.00089781      1.2368e+06            1566          35.903
v  TurbVisc             3.1882e-12         0.32658       0.0015176        0.025369
v  CourantNb             0.0021479           19169          32.878          5.7669
v  FourierNb              0.022566      2.3656e+05          21.857         0.30532
v  total_pressure       4.4484e+05      6.6289e+05      6.0294e+05      5.8655e+05
v  Local Time Step           0.001         0.06859        0.001004       0.0010298


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64771      2.4628e+05          54.735          6.0722


 TIME FOR THE TIME STEP              425:        0.75284E+02

===============================================================


 INSTANT    0.426000000E+01   TIME STEP NUMBER             426
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.339947483E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221232614E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46412E+02 0.55533E+01
   Friction velocity        uet   :  0.18566E-01 0.28439E+02
   Friction velocity        uk    :  0.35617E-01 0.28439E+02
   Dimensionless distance   yplus :  0.36289E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10426
   Nb of faces within the viscous sub-layer     :      13150
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10963E+02      54   0.75647E-01   0.33316E+02 0.33892E+02 
c  Velocity[X]                                      0.62847E+01 
c  Velocity[Y]                                      0.14285E+02 
c  Velocity[Z]                                      0.12747E+02 
c  Pressure     0.99781E-01    1001   0.49870E-01   0.13025E+00 0.19517E+01 
c  k            0.30289E+00      16   0.72630E-04   0.38387E-02 0.21117E+02 
c  epsilon      0.32655E+04      15   0.85697E-03   0.13000E+08 0.17567E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00030364                             2
a  epsilon                 -4.8507                             7
a  Local Time Step      4.2272e-08                        280597


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1414           15.35          1.5034         0.24591
v  Velocity[Y]             -24.266          29.444         0.82554         0.59478
v  Velocity[Z]             -42.597          28.864        -0.73218      -0.0032576
v  ǁVelocityǁ            0.0048158          45.462          4.9065          5.1088
v  Pressure                 -55369      1.6299e+05       1.028e+05           86554
v  k                    1.2216e-06          7.3061        0.053729        0.045883
v  epsilon               0.0010742      1.2117e+06          1566.3          35.944
v  TurbVisc             3.0818e-12         0.32658       0.0015253        0.025481
v  CourantNb              0.022618           19756          32.915          5.7727
v  FourierNb              0.022578      2.3656e+05          21.859         0.30538
v  total_pressure       4.4463e+05      6.6299e+05       6.028e+05      5.8655e+05
v  Local Time Step           0.001        0.066199       0.0010039       0.0010297


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58351       2.445e+05          54.775          6.0781


 TIME FOR THE TIME STEP              426:        0.10473E+03

===============================================================


 INSTANT    0.427000000E+01   TIME STEP NUMBER             427
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.347941678E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245452E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62661E+02 0.55620E+01
   Friction velocity        uet   :  0.34612E-01 0.26830E+02
   Friction velocity        uk    :  0.39494E-01 0.26830E+02
   Dimensionless distance   yplus :  0.34235E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10462
   Nb of faces within the viscous sub-layer     :      13104
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10969E+02      53   0.75926E-01   0.32691E+02 0.33593E+02 
c  Velocity[X]                                      0.61451E+01 
c  Velocity[Y]                                      0.14188E+02 
c  Velocity[Z]                                      0.12358E+02 
c  Pressure     0.10177E+00    1188   0.50092E-01   0.13284E+00 0.19754E+01 
c  k            0.30298E+00      19   0.61291E-04   0.27483E-02 0.18078E+02 
c  epsilon      0.32703E+04      13   0.42413E-03   0.55435E+07 0.11556E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021922                             3
a  epsilon                 -3.9134                             6
a  Local Time Step      4.2272e-08                        280628


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2405          14.207          1.5036         0.24615
v  Velocity[Y]             -26.141          26.387         0.82512          0.5953
v  Velocity[Z]             -38.403          27.594         -0.7339      -0.0032209
v  ǁVelocityǁ            0.0040872          41.889          4.9165          5.1127
v  Pressure                 -55630        1.63e+05      1.0258e+05           86491
v  k                    2.2692e-08          7.1637        0.053808        0.046011
v  epsilon               0.0013062      1.2302e+06          1562.3          35.992
v  TurbVisc             3.1195e-12         0.32658       0.0015321         0.02558
v  CourantNb              0.012633           20223          32.931          5.7789
v  FourierNb              0.022587      2.3656e+05          21.858         0.30558
v  total_pressure       4.4437e+05        6.63e+05      6.0258e+05      5.8649e+05
v  Local Time Step           0.001        0.047573       0.0010037       0.0010285


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59339       2.423e+05           54.79          6.0845


 TIME FOR THE TIME STEP              427:        0.12580E+03

===============================================================


 INSTANT    0.428000000E+01   TIME STEP NUMBER             428
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.611171247E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221252948E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46142E+02 0.55398E+01
   Friction velocity        uet   :  0.35696E-01 0.25602E+02
   Friction velocity        uk    :  0.34625E-01 0.25602E+02
   Dimensionless distance   yplus :  0.23790E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10472
   Nb of faces within the viscous sub-layer     :      13052
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10973E+02      51   0.75217E-01   0.30126E+02 0.32199E+02 
c  Velocity[X]                                      0.56699E+01 
c  Velocity[Y]                                      0.13004E+02 
c  Velocity[Z]                                      0.11453E+02 
c  Pressure     0.10691E+00     944   0.51536E-01   0.13910E+00 0.18432E+01 
c  k            0.30306E+00      20   0.66350E-04   0.31398E-02 0.19276E+02 
c  epsilon      0.32666E+04      11   0.27607E-03   0.33707E+07 0.90114E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023459                             2
a  epsilon                 -2.2381                             5
a  Local Time Step      4.2273e-08                        280634


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0477          14.236          1.5043         0.24676
v  Velocity[Y]             -30.682           26.19         0.82459          0.5959
v  Velocity[Z]             -39.494          31.976         -0.7355      -0.0035565
v  ǁVelocityǁ            0.0034634          42.069          4.9272           5.117
v  Pressure                 -55720       1.631e+05      1.0242e+05           86479
v  k                    5.7445e-07          7.0924        0.053925        0.046125
v  epsilon               0.0015852      1.2042e+06          1564.2          36.065
v  TurbVisc             9.5501e-16         0.32658       0.0015361        0.025668
v  CourantNb             0.0062979           20368          32.965          5.7851
v  FourierNb              0.022594      2.3656e+05          21.858         0.30555
v  total_pressure       4.4428e+05       6.631e+05      6.0242e+05      5.8648e+05
v  Local Time Step           0.001        0.030764       0.0010037       0.0010278


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56872      2.4213e+05          54.823          6.0906


 TIME FOR THE TIME STEP              428:        0.10229E+03

===============================================================


 INSTANT    0.429000000E+01   TIME STEP NUMBER             429
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.293204344E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221301364E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55846E+02 0.55592E+01
   Friction velocity        uet   :  0.31844E-01 0.26215E+02
   Friction velocity        uk    :  0.31221E-01 0.26215E+02
   Dimensionless distance   yplus :  0.32938E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10522
   Nb of faces within the viscous sub-layer     :      12976
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10979E+02      56   0.76173E-01   0.29747E+02 0.31998E+02 
c  Velocity[X]                                      0.52733E+01 
c  Velocity[Y]                                      0.13037E+02 
c  Velocity[Z]                                      0.11437E+02 
c  Pressure     0.10919E+00     859   0.50967E-01   0.14150E+00 0.22207E+01 
c  k            0.30312E+00      18   0.79953E-04   0.41964E-02 0.22347E+02 
c  epsilon      0.32785E+04      11   0.48735E-03   0.58345E+07 0.11771E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021632                             3
a  epsilon                 -2.4924                             4
a  Local Time Step      4.2273e-08                        280670


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1891          14.744          1.5057         0.24733
v  Velocity[Y]             -26.223          26.678         0.82437         0.59668
v  Velocity[Z]             -39.819          28.173        -0.73712      -0.0043476
v  ǁVelocityǁ            0.0031697          43.388           4.939          5.1209
v  Pressure                 -55835      1.6306e+05      1.0212e+05           86337
v  k                     1.588e-06          7.1921        0.054186        0.046229
v  epsilon              0.00024264      1.2317e+06          1580.8          36.181
v  TurbVisc             3.0999e-12         0.32658       0.0015395        0.025745
v  CourantNb              0.062796           20257          33.011          5.7918
v  FourierNb                0.0226      2.3656e+05          21.858         0.30574
v  total_pressure       4.4416e+05      6.6306e+05      6.0212e+05      5.8634e+05
v  Local Time Step           0.001        0.033841       0.0010037        0.001028


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77088      2.4257e+05          54.868          6.0976


 TIME FOR THE TIME STEP              429:        0.10262E+03

===============================================================


 INSTANT    0.430000000E+01   TIME STEP NUMBER             430
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.410802670E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221363430E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42743E+02 0.55192E+01
   Friction velocity        uet   :  0.33359E-01 0.23085E+02
   Friction velocity        uk    :  0.32355E-01 0.23085E+02
   Dimensionless distance   yplus :  0.29222E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10535
   Nb of faces within the viscous sub-layer     :      12974
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10982E+02      50   0.75923E-01   0.29104E+02 0.31652E+02 
c  Velocity[X]                                      0.51827E+01 
c  Velocity[Y]                                      0.11657E+02 
c  Velocity[Z]                                      0.12264E+02 
c  Pressure     0.10281E+00    1265   0.47576E-01   0.13259E+00 0.49020E+01 
c  k            0.30323E+00      17   0.61756E-04   0.35298E-02 0.20410E+02 
c  epsilon      0.32788E+04      11   0.38157E-03   0.29293E+07 0.83575E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010655                             2
a  epsilon                 -1.0417                             5
a  Local Time Step      4.2273e-08                        280669


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0602           13.87          1.5082          0.2473
v  Velocity[Y]             -27.248          25.053         0.82272         0.59723
v  Velocity[Z]             -39.759          30.896        -0.73572      -0.0044218
v  ǁVelocityǁ            0.0043584          42.406          4.9494          5.1233
v  Pressure                 -56128      1.6247e+05       1.014e+05           85859
v  k                    1.6022e-06          7.2037        0.054192        0.046319
v  epsilon               0.0025434       1.193e+06          1577.9          36.223
v  TurbVisc             2.9929e-12         0.32658       0.0015444        0.025813
v  CourantNb              0.015024           20508          33.068          5.7988
v  FourierNb              0.022603      2.3656e+05          21.858         0.30586
v  total_pressure       4.4387e+05      6.6247e+05       6.014e+05      5.8586e+05
v  Local Time Step           0.001         0.02908       0.0010037       0.0010278


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64602      2.4179e+05          54.925          6.1047


 TIME FOR THE TIME STEP              430:        0.13238E+03

===============================================================


 INSTANT    0.431000000E+01   TIME STEP NUMBER             431
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.566470927E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221226580E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49160E+02 0.55186E+01
   Friction velocity        uet   :  0.33169E-01 0.23398E+02
   Friction velocity        uk    :  0.35046E-01 0.23398E+02
   Dimensionless distance   yplus :  0.29857E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10561
   Nb of faces within the viscous sub-layer     :      12948
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10977E+02      52   0.75555E-01   0.28180E+02 0.31107E+02 
c  Velocity[X]                                      0.50310E+01 
c  Velocity[Y]                                      0.11000E+02 
c  Velocity[Z]                                      0.12149E+02 
c  Pressure     0.96268E-01     808   0.43796E-01   0.12381E+00 0.16662E+01 
c  k            0.30332E+00      17   0.65701E-04   0.27992E-02 0.18242E+02 
c  epsilon      0.32769E+04      13   0.26612E-03   0.27031E+07 0.80315E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001134                             2
a  epsilon                 -1.8795                             7
a  Local Time Step      4.2273e-08                        280667


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0237          13.975          1.5092         0.24679
v  Velocity[Y]             -25.698          25.817         0.82432         0.59776
v  Velocity[Z]             -39.746          27.848        -0.73408      -0.0048421
v  ǁVelocityǁ            0.0050357          42.769          4.9609           5.126
v  Pressure                 -55897      1.6246e+05      1.0125e+05           85894
v  k                    1.6362e-06          7.3957        0.054384        0.046391
v  epsilon               0.0033309      1.2109e+06          1579.7          36.305
v  TurbVisc             3.0848e-12         0.32658       0.0015508        0.025872
v  CourantNb              0.015083           20415          33.136          5.8036
v  FourierNb              0.022606      2.3656e+05          21.858         0.30587
v  total_pressure        4.441e+05      6.6246e+05      6.0125e+05      5.8589e+05
v  Local Time Step           0.001        0.026134       0.0010036       0.0010268


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63542      2.4104e+05          54.993          6.1095


 TIME FOR THE TIME STEP              431:        0.10065E+03

===============================================================


 INSTANT    0.432000000E+01   TIME STEP NUMBER             432
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.245431921E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221312638E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51268E+02 0.54779E+01
   Friction velocity        uet   :  0.24135E-01 0.22685E+02
   Friction velocity        uk    :  0.23508E-01 0.22685E+02
   Dimensionless distance   yplus :  0.26694E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10579
   Nb of faces within the viscous sub-layer     :      12941
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10979E+02      57   0.74971E-01   0.27187E+02 0.30528E+02 
c  Velocity[X]                                      0.50022E+01 
c  Velocity[Y]                                      0.10958E+02 
c  Velocity[Z]                                      0.11227E+02 
c  Pressure     0.89992E-01     721   0.41467E-01   0.11535E+00 0.15448E+01 
c  k            0.30333E+00      15   0.71851E-04   0.30775E-02 0.18968E+02 
c  epsilon      0.32673E+04      13   0.38504E-03   0.32692E+07 0.88501E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.9546e-05                             2
a  epsilon                 -1.7741                             6
a  Local Time Step      4.2274e-08                        280666


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9992          13.435          1.5108         0.24624
v  Velocity[Y]             -26.059          25.834         0.82833         0.59807
v  Velocity[Z]             -37.587          28.263        -0.73233      -0.0054365
v  ǁVelocityǁ            0.0084153          40.122          4.9727          5.1289
v  Pressure                 -55701      1.6242e+05      1.0106e+05           85842
v  k                    1.6458e-06          7.5303        0.054448        0.046449
v  epsilon               0.0029661      1.1726e+06          1577.9           36.36
v  TurbVisc             3.0987e-12         0.32658       0.0015576        0.025922
v  CourantNb             0.0029958           19850          33.223          5.8101
v  FourierNb              0.022608      2.3655e+05          21.858         0.30601
v  total_pressure        4.443e+05      6.6242e+05      6.0106e+05      5.8584e+05
v  Local Time Step           0.001        0.028659       0.0010036       0.0010265


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66738       2.404e+05          55.081          6.1161


 TIME FOR THE TIME STEP              432:        0.88840E+02

===============================================================


 INSTANT    0.433000000E+01   TIME STEP NUMBER             433
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.954038680E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221344442E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51414E+02 0.55283E+01
   Friction velocity        uet   :  0.28517E-01 0.22544E+02
   Friction velocity        uk    :  0.27706E-01 0.22544E+02
   Dimensionless distance   yplus :  0.27278E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10621
   Nb of faces within the viscous sub-layer     :      12931
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10982E+02      47   0.77488E-01   0.26983E+02 0.30411E+02 
c  Velocity[X]                                      0.51873E+01 
c  Velocity[Y]                                      0.10690E+02 
c  Velocity[Z]                                      0.11105E+02 
c  Pressure     0.87113E-01     673   0.40652E-01   0.11168E+00 0.15319E+01 
c  k            0.30337E+00      17   0.70331E-04   0.28939E-02 0.18422E+02 
c  epsilon      0.32739E+04      10   0.24569E-03   0.34214E+07 0.90355E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.4842e-05                             1
a  epsilon                 -2.3288                             8
a  Local Time Step      4.2274e-08                        280653


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0589          14.228          1.5107         0.24605
v  Velocity[Y]             -24.625          27.965         0.83172          0.5981
v  Velocity[Z]             -38.829          28.247        -0.73071      -0.0060414
v  ǁVelocityǁ            0.0094274           42.31          4.9839          5.1317
v  Pressure                 -55412      1.6249e+05      1.0096e+05           85886
v  k                    1.6819e-06           7.668        0.054573          0.0465
v  epsilon              0.00026646      1.2211e+06          1580.9          36.434
v  TurbVisc             3.1567e-12         0.32658       0.0015638        0.025965
v  CourantNb              0.032604           20256          33.317          5.8157
v  FourierNb              0.022609      2.3655e+05          21.859         0.30607
v  total_pressure       4.4459e+05      6.6249e+05      6.0096e+05      5.8589e+05
v  Local Time Step           0.001        0.031525       0.0010036       0.0010259


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6531      2.4018e+05          55.177          6.1217


 TIME FOR THE TIME STEP              433:        0.83521E+02

===============================================================


 INSTANT    0.434000000E+01   TIME STEP NUMBER             434
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.118743588E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221405303E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46950E+02 0.55098E+01
   Friction velocity        uet   :  0.16167E-01 0.22424E+02
   Friction velocity        uk    :  0.15922E-01 0.22424E+02
   Dimensionless distance   yplus :  0.22043E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10674
   Nb of faces within the viscous sub-layer     :      12953
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10985E+02      48   0.75326E-01   0.28382E+02 0.31167E+02 
c  Velocity[X]                                      0.52621E+01 
c  Velocity[Y]                                      0.11032E+02 
c  Velocity[Z]                                      0.12088E+02 
c  Pressure     0.87859E-01     943   0.41238E-01   0.11253E+00 0.27134E+01 
c  k            0.30337E+00      17   0.62221E-04   0.27983E-02 0.17936E+02 
c  epsilon      0.32663E+04      11   0.33364E-03   0.38757E+07 0.96418E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -7.9377                             8
a  Local Time Step      4.2274e-08                        280613


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9998          13.261          1.5115         0.24609
v  Velocity[Y]             -27.217          25.633         0.83607         0.59772
v  Velocity[Z]             -39.053          30.269        -0.73008      -0.0058958
v  ǁVelocityǁ             0.010915          41.529          4.9949          5.1343
v  Pressure                 -55403      1.6225e+05      1.0056e+05           85640
v  k                    1.6915e-06          7.5708         0.05458        0.046543
v  epsilon              0.00084124      1.1896e+06          1577.8          36.457
v  TurbVisc             3.1969e-12         0.32658       0.0015701        0.026002
v  CourantNb             0.0027248           19505          33.383          5.8213
v  FourierNb               0.02261      2.3655e+05          21.859         0.30606
v  total_pressure        4.446e+05      6.6225e+05      6.0056e+05      5.8564e+05
v  Local Time Step           0.001          0.0271       0.0010035       0.0010256


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61331      2.3881e+05          55.241          6.1274


 TIME FOR THE TIME STEP              434:        0.11228E+03

===============================================================


 INSTANT    0.435000000E+01   TIME STEP NUMBER             435
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.251852214E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221380076E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47602E+02 0.54950E+01
   Friction velocity        uet   :  0.34400E-01 0.20916E+02
   Friction velocity        uk    :  0.33355E-01 0.20916E+02
   Dimensionless distance   yplus :  0.23460E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10712
   Nb of faces within the viscous sub-layer     :      12955
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10984E+02      47   0.75655E-01   0.29058E+02 0.31547E+02 
c  Velocity[X]                                      0.53874E+01 
c  Velocity[Y]                                      0.11912E+02 
c  Velocity[Z]                                      0.11759E+02 
c  Pressure     0.87820E-01     785   0.42270E-01   0.11280E+00 0.25027E+01 
c  k            0.30343E+00      16   0.72584E-04   0.27913E-02 0.17926E+02 
c  epsilon      0.32688E+04      10   0.33837E-03   0.28080E+07 0.81811E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023281                             1
a  epsilon                 -2.3948                             4
a  Local Time Step      4.2274e-08                        280610


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8152          13.667          1.5106          0.2459
v  Velocity[Y]             -25.243          24.795         0.84104         0.59718
v  Velocity[Z]              -38.14          28.224        -0.73031      -0.0055566
v  ǁVelocityǁ             0.010189          41.479          5.0037          5.1345
v  Pressure                 -55374      1.6201e+05      1.0021e+05           85422
v  k                    1.7167e-06          7.6962        0.054704        0.046594
v  epsilon               0.0020524      1.1937e+06            1582          36.568
v  TurbVisc             3.2465e-12         0.32658       0.0015757        0.026034
v  CourantNb              0.001816           21038          33.453          5.8272
v  FourierNb              0.022612      2.3655e+05          21.859         0.30619
v  total_pressure       4.4463e+05      6.6201e+05      6.0021e+05      5.8542e+05
v  Local Time Step           0.001         0.02981       0.0010035       0.0010252


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51189      2.4057e+05          55.312          6.1334


 TIME FOR THE TIME STEP              435:        0.81326E+02

===============================================================


 INSTANT    0.436000000E+01   TIME STEP NUMBER             436
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.212969992E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221357089E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41471E+02 0.54839E+01
   Friction velocity        uet   :  0.34943E-01 0.19986E+02
   Friction velocity        uk    :  0.35049E-01 0.19986E+02
   Dimensionless distance   yplus :  0.20176E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10731
   Nb of faces within the viscous sub-layer     :      12920
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10978E+02      45   0.73966E-01   0.29219E+02 0.31614E+02 
c  Velocity[X]                                      0.56436E+01 
c  Velocity[Y]                                      0.12453E+02 
c  Velocity[Z]                                      0.11122E+02 
c  Pressure     0.88777E-01     663   0.42864E-01   0.11420E+00 0.13874E+01 
c  k            0.30352E+00      17   0.10586E-03   0.33649E-02 0.19062E+02 
c  epsilon      0.32811E+04      13   0.33266E-03   0.61914E+07 0.12061E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -7.4917                             6
a  Local Time Step      4.2274e-08                        280628


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7619          13.141          1.5115         0.24605
v  Velocity[Y]             -26.097          27.176         0.84313         0.59669
v  Velocity[Z]             -37.049          31.693         -0.7315      -0.0052514
v  ǁVelocityǁ            0.0081511          39.547          5.0089          5.1345
v  Pressure                 -54847      1.6211e+05      1.0017e+05           85437
v  k                    1.6898e-06          7.9321        0.055107        0.046646
v  epsilon               0.0014377      1.1837e+06            1603          36.685
v  TurbVisc             3.2377e-12         0.32658       0.0015827        0.026062
v  CourantNb                     0           21415          33.502          5.8306
v  FourierNb              0.022612      2.3655e+05          21.859         0.30627
v  total_pressure       4.4515e+05      6.6211e+05      6.0017e+05      5.8544e+05
v  Local Time Step           0.001        0.032791       0.0010034        0.001025


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58907      2.4042e+05          55.361          6.1368


 TIME FOR THE TIME STEP              436:        0.83135E+02

===============================================================


 INSTANT    0.437000000E+01   TIME STEP NUMBER             437
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.401103225E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221305201E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50103E+02 0.55089E+01
   Friction velocity        uet   :  0.33942E-01 0.21304E+02
   Friction velocity        uk    :  0.32908E-01 0.21304E+02
   Dimensionless distance   yplus :  0.21990E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10750
   Nb of faces within the viscous sub-layer     :      12931
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10978E+02      48   0.74933E-01   0.28567E+02 0.31282E+02 
c  Velocity[X]                                      0.57307E+01 
c  Velocity[Y]                                      0.12335E+02 
c  Velocity[Z]                                      0.10501E+02 
c  Pressure     0.90608E-01    1132   0.44706E-01   0.11687E+00 0.14821E+01 
c  k            0.30364E+00      16   0.12476E-03   0.35160E-02 0.19498E+02 
c  epsilon      0.32845E+04      12   0.38642E-03   0.57296E+07 0.11617E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -3.0489                             4
a  Local Time Step      4.2274e-08                        280606


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8194          13.814          1.5094         0.24606
v  Velocity[Y]             -24.337          25.257         0.84567          0.5964
v  Velocity[Z]             -37.989          28.665        -0.73164      -0.0045419
v  ǁVelocityǁ            0.0095231          41.269          5.0115          5.1345
v  Pressure                 -54447      1.6206e+05      1.0004e+05           85396
v  k                    1.7214e-06          7.9195        0.055162        0.046703
v  epsilon               0.0011793      1.2006e+06          1605.8          36.748
v  TurbVisc             3.1925e-12         0.32658       0.0015908        0.026088
v  CourantNb             0.0045547           21172          33.516          5.8326
v  FourierNb              0.022612      2.3655e+05          21.859         0.30637
v  total_pressure       4.4555e+05      6.6206e+05      6.0004e+05       5.854e+05
v  Local Time Step           0.001        0.031055       0.0010034       0.0010251


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54885      2.3895e+05          55.374           6.139


 TIME FOR THE TIME STEP              437:        0.10320E+03

===============================================================


 INSTANT    0.438000000E+01   TIME STEP NUMBER             438
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.686730313E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221254245E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39868E+02 0.55060E+01
   Friction velocity        uet   :  0.34327E-01 0.22249E+02
   Friction velocity        uk    :  0.33276E-01 0.22249E+02
   Dimensionless distance   yplus :  0.16679E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10750
   Nb of faces within the viscous sub-layer     :      12900
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10978E+02      46   0.76911E-01   0.29969E+02 0.32039E+02 
c  Velocity[X]                                      0.56571E+01 
c  Velocity[Y]                                      0.13120E+02 
c  Velocity[Z]                                      0.11192E+02 
c  Pressure     0.92551E-01     490   0.45465E-01   0.11945E+00 0.14599E+01 
c  k            0.30385E+00      17   0.20750E-03   0.56803E-02 0.23210E+02 
c  epsilon      0.32942E+04      11   0.36148E-03   0.50997E+07 0.10932E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00031353                             9
a  epsilon                 -84.368                            16
a  Local Time Step      4.2274e-08                        280595


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7924          13.268          1.5077         0.24581
v  Velocity[Y]             -27.041          27.531         0.84667         0.59595
v  Velocity[Z]             -39.627          28.154        -0.73294      -0.0041221
v  ǁVelocityǁ            0.0084416          42.037          5.0146          5.1338
v  Pressure                 -53934      1.6213e+05      1.0003e+05           85413
v  k                    1.7352e-06          7.9945        0.055249        0.046769
v  epsilon               0.0032825      1.1942e+06          1605.5          36.834
v  TurbVisc             3.2666e-12         0.32658        0.001599        0.026111
v  CourantNb             0.0069238           20919          33.515          5.8345
v  FourierNb              0.022612      2.3655e+05           21.86         0.30644
v  total_pressure       4.4607e+05      6.6213e+05      6.0003e+05      5.8541e+05
v  Local Time Step           0.001        0.028737       0.0010034       0.0010249


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81546      2.4032e+05          55.376          6.1409


 TIME FOR THE TIME STEP              438:        0.76811E+02

===============================================================


 INSTANT    0.439000000E+01   TIME STEP NUMBER             439
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.200754329E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221243524E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.48834E+02 0.54956E+01
   Friction velocity        uet   :  0.28535E-01 0.22023E+02
   Friction velocity        uk    :  0.38961E-01 0.22023E+02
   Dimensionless distance   yplus :  0.18450E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10750
   Nb of faces within the viscous sub-layer     :      12867
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10974E+02      52   0.76517E-01   0.30440E+02 0.32264E+02 
c  Velocity[X]                                      0.58033E+01 
c  Velocity[Y]                                      0.12941E+02 
c  Velocity[Z]                                      0.11695E+02 
c  Pressure     0.94534E-01     390   0.47349E-01   0.12227E+00 0.14948E+01 
c  k            0.30429E+00      17   0.18048E-03   0.53206E-02 0.23819E+02 
c  epsilon      0.33074E+04      13   0.27390E-03   0.26074E+07 0.77877E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                -0.59414                             2
a  Local Time Step      4.2274e-08                        280584


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7933           13.51           1.508         0.24555
v  Velocity[Y]             -24.629          26.272          0.8485         0.59555
v  Velocity[Z]             -38.894          28.329        -0.73464      -0.0040106
v  ǁVelocityǁ            0.0078471          41.765          5.0171          5.1327
v  Pressure                 -53381      1.6216e+05      1.0003e+05           85441
v  k                    1.7499e-06           8.143        0.055557        0.046846
v  epsilon               0.0061244      1.1923e+06          1617.1          36.978
v  TurbVisc             3.2795e-12         0.32658       0.0016077        0.026133
v  CourantNb              0.015755           22091          33.534          5.8356
v  FourierNb              0.022611      2.3655e+05          21.861         0.30654
v  total_pressure       4.4662e+05      6.6216e+05      6.0003e+05      5.8544e+05
v  Local Time Step           0.001        0.031611       0.0010033       0.0010236


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76897      2.4137e+05          55.395          6.1422


 TIME FOR THE TIME STEP              439:        0.73785E+02

===============================================================


 INSTANT    0.440000000E+01   TIME STEP NUMBER             440
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.367228051E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221216030E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49628E+02 0.54800E+01
   Friction velocity        uet   :  0.35613E-01 0.20413E+02
   Friction velocity        uk    :  0.40911E-01 0.20413E+02
   Dimensionless distance   yplus :  0.17617E-02 0.16145E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10742
   Nb of faces within the viscous sub-layer     :      12855
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10975E+02      43   0.75329E-01   0.30211E+02 0.32138E+02 
c  Velocity[X]                                      0.56980E+01 
c  Velocity[Y]                                      0.13219E+02 
c  Velocity[Z]                                      0.11294E+02 
c  Pressure     0.97568E-01     419   0.48960E-01   0.12611E+00 0.15302E+01 
c  k            0.30479E+00      17   0.36299E-03   0.92447E-02 0.28815E+02 
c  epsilon      0.33086E+04      11   0.26085E-03   0.26208E+07 0.77950E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.6823e-05                             1
a  epsilon                 -81.614                             7
a  Local Time Step      4.2274e-08                        280553


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7391          13.446          1.5084         0.24538
v  Velocity[Y]             -26.198          26.279         0.84996         0.59436
v  Velocity[Z]             -37.836          28.429        -0.73677      -0.0040314
v  ǁVelocityǁ            0.0085023           40.58          5.0216          5.1333
v  Pressure                 -52805      1.6217e+05      1.0002e+05           85475
v  k                    1.7627e-06          8.0536        0.055618        0.046927
v  epsilon               0.0075379      1.1811e+06          1619.1          37.043
v  TurbVisc             3.2737e-12         0.32658       0.0016163        0.026154
v  CourantNb              0.038223           21436          33.553          5.8351
v  FourierNb              0.022611      2.3655e+05          21.862         0.30667
v  total_pressure        4.472e+05      6.6217e+05      6.0002e+05      5.8548e+05
v  Local Time Step           0.001        0.034772       0.0010033        0.001024


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46089      2.4217e+05          55.415          6.1418


 TIME FOR THE TIME STEP              440:        0.75489E+02

===============================================================


 INSTANT    0.441000000E+01   TIME STEP NUMBER             441
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.533850010E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221234914E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46134E+02 0.54990E+01
   Friction velocity        uet   :  0.23736E-01 0.17007E+02
   Friction velocity        uk    :  0.37142E-01 0.17007E+02
   Dimensionless distance   yplus :  0.17210E-02 0.18674E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10710
   Nb of faces within the viscous sub-layer     :      12877
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10977E+02      47   0.75822E-01   0.30182E+02 0.32127E+02 
c  Velocity[X]                                      0.57942E+01 
c  Velocity[Y]                                      0.13095E+02 
c  Velocity[Z]                                      0.11293E+02 
c  Pressure     0.10013E+00     370   0.50070E-01   0.12950E+00 0.15318E+01 
c  k            0.30547E+00      20   0.16291E-03   0.78342E-02 0.29614E+02 
c  epsilon      0.33125E+04      12   0.27553E-03   0.22992E+07 0.72979E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -26.611                             5
a  Local Time Step      4.2274e-08                        280501


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7397          13.661          1.5098         0.24529
v  Velocity[Y]             -24.426          24.894         0.85283         0.59326
v  Velocity[Z]             -37.434          28.489        -0.74022      -0.0043537
v  ǁVelocityǁ            0.0066353          40.739          5.0276          5.1335
v  Pressure                 -52325      1.6216e+05      1.0001e+05           85495
v  k                    1.7851e-06          8.0453        0.055721        0.047023
v  epsilon               0.0075483      1.1962e+06          1619.4          37.166
v  TurbVisc             3.3605e-12         0.32658       0.0016239        0.026174
v  CourantNb             0.0030729           21780          33.592           5.837
v  FourierNb              0.022612      2.3655e+05          21.863         0.30675
v  total_pressure       4.4768e+05      6.6216e+05      6.0001e+05       5.855e+05
v  Local Time Step           0.001        0.038249       0.0010033       0.0010237


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43674      2.4072e+05          55.455          6.1438


 TIME FOR THE TIME STEP              441:        0.71660E+02

===============================================================


 INSTANT    0.442000000E+01   TIME STEP NUMBER             442
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.718618099E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221242057E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36385E+02 0.54910E+01
   Friction velocity        uet   :  0.28211E-01 0.18359E+02
   Friction velocity        uk    :  0.36538E-01 0.18359E+02
   Dimensionless distance   yplus :  0.15698E-02 0.18594E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10712
   Nb of faces within the viscous sub-layer     :      12871
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10978E+02      46   0.76672E-01   0.29758E+02 0.31898E+02 
c  Velocity[X]                                      0.56299E+01 
c  Velocity[Y]                                      0.12957E+02 
c  Velocity[Z]                                      0.11171E+02 
c  Pressure     0.99172E-01     443   0.48302E-01   0.12829E+00 0.15660E+01 
c  k            0.30631E+00      19   0.27156E-03   0.11900E-01 0.36618E+02 
c  epsilon      0.33217E+04      14   0.30308E-03   0.21885E+07 0.70922E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.1746e-08                             1
a  epsilon                 -5.8702                             3
a  Local Time Step      4.2274e-08                        280484


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6423          13.338          1.5093         0.24544
v  Velocity[Y]             -27.674          27.137          0.8568         0.59296
v  Velocity[Z]             -34.752          28.088        -0.74576       -0.004693
v  ǁVelocityǁ            0.0069275          37.399           5.034          5.1338
v  Pressure                 -51938      1.6216e+05      1.0002e+05           85497
v  k                    5.1746e-08          8.0578        0.055928        0.047124
v  epsilon               0.0059774      1.1885e+06          1632.2          37.305
v  TurbVisc              3.313e-12         0.32658       0.0016313        0.026193
v  CourantNb              0.005744           20697          33.647           5.839
v  FourierNb              0.022614      2.3655e+05          21.862          0.3069
v  total_pressure       4.4806e+05      6.6216e+05      6.0002e+05       5.855e+05
v  Local Time Step           0.001        0.042074       0.0010034       0.0010238


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67946      2.4074e+05          55.509          6.1459


 TIME FOR THE TIME STEP              442:        0.71837E+02

===============================================================


 INSTANT    0.443000000E+01   TIME STEP NUMBER             443
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.281230654E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221289320E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44671E+02 0.54495E+01
   Friction velocity        uet   :  0.36765E-01 0.19220E+02
   Friction velocity        uk    :  0.46387E-01 0.19220E+02
   Dimensionless distance   yplus :  0.17310E-02 0.18092E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10732
   Nb of faces within the viscous sub-layer     :      12903
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10975E+02      46   0.76377E-01   0.27837E+02 0.30851E+02 
c  Velocity[X]                                      0.51439E+01 
c  Velocity[Y]                                      0.11357E+02 
c  Velocity[Z]                                      0.11336E+02 
c  Pressure     0.98236E-01     442   0.47413E-01   0.12689E+00 0.16205E+01 
c  k            0.30683E+00      17   0.26525E-03   0.96854E-02 0.32564E+02 
c  epsilon      0.33256E+04      13   0.27795E-03   0.22846E+07 0.72382E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -1.1683                             3
a  Local Time Step      4.2274e-08                        280489


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.6831          14.025          1.5099          0.2455
v  Velocity[Y]             -24.702          27.109         0.86126         0.59338
v  Velocity[Z]             -40.471          28.199        -0.75163      -0.0048435
v  ǁVelocityǁ            0.0064948          43.731          5.0419          5.1335
v  Pressure                 -51789      1.6215e+05      1.0001e+05           85478
v  k                    1.7623e-06          8.0811        0.055951        0.047208
v  epsilon               0.0074772       1.161e+06          1624.9          37.407
v  TurbVisc              3.273e-12         0.32658       0.0016387        0.026212
v  CourantNb              0.035571           21315          33.719          5.8424
v  FourierNb              0.022618      2.3655e+05          21.863         0.30697
v  total_pressure       4.4821e+05      6.6215e+05      6.0001e+05      5.8548e+05
v  Local Time Step           0.001        0.046281       0.0010034       0.0010236


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44067      2.4207e+05          55.582          6.1493


 TIME FOR THE TIME STEP              443:        0.67223E+02

===============================================================


 INSTANT    0.444000000E+01   TIME STEP NUMBER             444
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.822777260E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221311262E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44000E+02 0.55041E+01
   Friction velocity        uet   :  0.35891E-01 0.17362E+02
   Friction velocity        uk    :  0.48549E-01 0.17362E+02
   Dimensionless distance   yplus :  0.18422E-02 0.17445E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10743
   Nb of faces within the viscous sub-layer     :      12877
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10974E+02      45   0.76914E-01   0.25910E+02 0.29735E+02 
c  Velocity[X]                                      0.48440E+01 
c  Velocity[Y]                                      0.90951E+01 
c  Velocity[Z]                                      0.11971E+02 
c  Pressure     0.93206E-01     430   0.44086E-01   0.12023E+00 0.15543E+01 
c  k            0.30702E+00      23   0.26486E-03   0.10863E-01 0.34738E+02 
c  epsilon      0.33338E+04      13   0.39687E-03   0.31464E+07 0.84530E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -1.2917                             3
a  Local Time Step      4.2274e-08                        280513


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -6.804          13.358          1.5096         0.24553
v  Velocity[Y]             -27.758          28.857         0.86438         0.59408
v  Velocity[Z]              -37.14          29.142        -0.75749      -0.0047748
v  ǁVelocityǁ            0.0060065          39.766          5.0492          5.1338
v  Pressure                 -53034      1.6216e+05      1.0002e+05           85460
v  k                    1.7521e-06          7.9464        0.056238        0.047268
v  epsilon               0.0045152      1.2095e+06          1636.8          37.562
v  TurbVisc             3.2827e-12         0.32658       0.0016471         0.02623
v  CourantNb             0.0064212           21746           33.78          5.8452
v  FourierNb              0.022625      2.3655e+05          21.862         0.30702
v  total_pressure       4.4697e+05      6.6216e+05      6.0002e+05      5.8546e+05
v  Local Time Step           0.001        0.050909       0.0010034       0.0010238


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.33625      2.4139e+05          55.642          6.1522


 TIME FOR THE TIME STEP              444:        0.77418E+02

===============================================================


 INSTANT    0.445000000E+01   TIME STEP NUMBER             445
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.159062605E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221313119E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42706E+02 0.54717E+01
   Friction velocity        uet   :  0.34757E-01 0.19217E+02
   Friction velocity        uk    :  0.52262E-01 0.19217E+02
   Dimensionless distance   yplus :  0.24521E-02 0.16334E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10741
   Nb of faces within the viscous sub-layer     :      12846
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10969E+02      45   0.75274E-01   0.24983E+02 0.29220E+02 
c  Velocity[X]                                      0.46052E+01 
c  Velocity[Y]                                      0.84171E+01 
c  Velocity[Z]                                      0.11961E+02 
c  Pressure     0.90471E-01     488   0.42670E-01   0.11657E+00 0.14948E+01 
c  k            0.30720E+00      19   0.14326E-03   0.77608E-02 0.29291E+02 
c  epsilon      0.33383E+04      11   0.43158E-03   0.27679E+07 0.79154E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.3667e-05                             1
a  epsilon                -0.67738                             3
a  Local Time Step      4.2274e-08                        280517


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8403          14.178           1.511         0.24567
v  Velocity[Y]              -24.98           25.76         0.86778          0.5948
v  Velocity[Z]             -38.877          30.705        -0.76256      -0.0045323
v  ǁVelocityǁ            0.0064979          42.299          5.0579          5.1335
v  Pressure                 -56311      1.6216e+05      1.0002e+05           85427
v  k                    1.8364e-06           7.624        0.056453        0.047319
v  epsilon               0.0066956      1.1717e+06          1646.5          37.645
v  TurbVisc              3.284e-12         0.32658       0.0016569        0.026243
v  CourantNb              0.011505           22518          33.856          5.8476
v  FourierNb              0.022636      2.3655e+05          21.863         0.30713
v  total_pressure       4.4369e+05      6.6216e+05      6.0002e+05      5.8543e+05
v  Local Time Step           0.001           0.056       0.0010034       0.0010235


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54803      2.4142e+05          55.719          6.1547


 TIME FOR THE TIME STEP              445:        0.65476E+02

===============================================================


 INSTANT    0.446000000E+01   TIME STEP NUMBER             446
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.253527995E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221273368E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38380E+02 0.54894E+01
   Friction velocity        uet   :  0.26226E-01 0.16620E+02
   Friction velocity        uk    :  0.47270E-01 0.16620E+02
   Dimensionless distance   yplus :  0.18440E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10770
   Nb of faces within the viscous sub-layer     :      12836
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10966E+02      48   0.76567E-01   0.23421E+02 0.28286E+02 
c  Velocity[X]                                      0.43823E+01 
c  Velocity[Y]                                      0.80646E+01 
c  Velocity[Z]                                      0.10974E+02 
c  Pressure     0.83752E-01     427   0.38738E-01   0.10770E+00 0.14040E+01 
c  k            0.30713E+00      18   0.16321E-03   0.49356E-02 0.23580E+02 
c  epsilon      0.33541E+04      13   0.25254E-03   0.41670E+07 0.96593E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -1.2349                             2
a  Local Time Step      4.2274e-08                        280504


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8012          13.231          1.5106         0.24591
v  Velocity[Y]             -27.136           28.94         0.86937         0.59525
v  Velocity[Z]             -34.519            32.5        -0.76703      -0.0039203
v  ǁVelocityǁ            0.0080008          36.843          5.0656          5.1338
v  Pressure                 -58759      1.6218e+05      1.0004e+05           85401
v  k                    1.8196e-06          7.5756        0.056755        0.047369
v  epsilon               0.0074541      1.1982e+06          1658.1          37.775
v  TurbVisc             3.4624e-12         0.32658       0.0016681        0.026256
v  CourantNb              0.028559           22051          33.938          5.8501
v  FourierNb              0.022649      2.3655e+05          21.864         0.30728
v  total_pressure       4.4124e+05      6.6218e+05      6.0004e+05       5.854e+05
v  Local Time Step           0.001        0.045898       0.0010034       0.0010231


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.3345      2.4202e+05          55.802          6.1574


 TIME FOR THE TIME STEP              446:        0.77872E+02

===============================================================


 INSTANT    0.447000000E+01   TIME STEP NUMBER             447
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.136233150E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221229535E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41124E+02 0.54635E+01
   Friction velocity        uet   :  0.35318E-01 0.18749E+02
   Friction velocity        uk    :  0.40445E-01 0.18749E+02
   Dimensionless distance   yplus :  0.20462E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10799
   Nb of faces within the viscous sub-layer     :      12820
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10961E+02      47   0.76877E-01   0.24055E+02 0.28671E+02 
c  Velocity[X]                                      0.40723E+01 
c  Velocity[Y]                                      0.84916E+01 
c  Velocity[Z]                                      0.11491E+02 
c  Pressure     0.83493E-01     400   0.37642E-01   0.10743E+00 0.13505E+01 
c  k            0.30694E+00      20   0.18257E-03   0.45083E-02 0.22565E+02 
c  epsilon      0.33670E+04      11   0.24661E-03   0.19237E+07 0.65526E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.8884                             6
a  Local Time Step      4.2274e-08                        280502


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7455          14.439          1.5099         0.24598
v  Velocity[Y]             -25.892           26.09         0.86946         0.59554
v  Velocity[Z]             -42.064          32.292        -0.77033       -0.002967
v  ǁVelocityǁ             0.010084          45.389          5.0693          5.1334
v  Pressure                 -59875      1.6219e+05      1.0006e+05           85368
v  k                    1.8462e-06          7.7444        0.056912        0.047421
v  epsilon               0.0075512      1.1705e+06          1661.9          37.871
v  TurbVisc             3.3876e-12         0.32658       0.0016794        0.026267
v  CourantNb              0.033677           22328          34.008          5.8527
v  FourierNb              0.022668      2.3655e+05          21.866         0.30733
v  total_pressure       4.4013e+05      6.6219e+05      6.0006e+05      5.8537e+05
v  Local Time Step           0.001        0.050488       0.0010034       0.0010231


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.16994      2.3893e+05          55.874          6.1601


 TIME FOR THE TIME STEP              447:        0.74208E+02

===============================================================


 INSTANT    0.448000000E+01   TIME STEP NUMBER             448
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.778772666E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221105220E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47151E+02 0.54710E+01
   Friction velocity        uet   :  0.35250E-01 0.16849E+02
   Friction velocity        uk    :  0.51368E-01 0.16849E+02
   Dimensionless distance   yplus :  0.18504E-02 0.16027E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10818
   Nb of faces within the viscous sub-layer     :      12784
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10958E+02      47   0.74428E-01   0.23983E+02 0.28637E+02 
c  Velocity[X]                                      0.38783E+01 
c  Velocity[Y]                                      0.83093E+01 
c  Velocity[Z]                                      0.11795E+02 
c  Pressure     0.80162E-01     473   0.35574E-01   0.10306E+00 0.11853E+01 
c  k            0.30678E+00      17   0.26234E-03   0.85062E-02 0.29953E+02 
c  epsilon      0.33817E+04      12   0.86653E-03   0.90890E+07 0.14008E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -1.4848                             5
a  Local Time Step      4.2274e-08                        280511


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8218          13.249          1.5093         0.24596
v  Velocity[Y]             -26.778          29.076         0.86704         0.59579
v  Velocity[Z]              -38.05          28.651        -0.77136      -0.0016523
v  ǁVelocityǁ            0.0049741          40.808          5.0721          5.1327
v  Pressure                 -59721      1.6219e+05      1.0011e+05           85361
v  k                    1.8678e-06          7.8159        0.057243        0.047468
v  epsilon              0.00032595      1.1841e+06          1683.4           37.99
v  TurbVisc             3.4708e-12         0.32658       0.0016903        0.026278
v  CourantNb              0.043567           22561          34.037          5.8537
v  FourierNb               0.02269      2.3655e+05          21.867          0.3074
v  total_pressure       4.4028e+05      6.6219e+05      6.0011e+05      5.8536e+05
v  Local Time Step           0.001         0.04609       0.0010034       0.0010232


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.26258      2.4002e+05          55.903          6.1611


 TIME FOR THE TIME STEP              448:        0.76291E+02

===============================================================


 INSTANT    0.449000000E+01   TIME STEP NUMBER             449
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.886417223E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.220977509E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41229E+02 0.54692E+01
   Friction velocity        uet   :  0.28116E-01 0.17856E+02
   Friction velocity        uk    :  0.28082E-01 0.17856E+02
   Dimensionless distance   yplus :  0.17861E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10835
   Nb of faces within the viscous sub-layer     :      12777
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10952E+02      61   0.74899E-01   0.23906E+02 0.28594E+02 
c  Velocity[X]                                      0.40230E+01 
c  Velocity[Y]                                      0.84472E+01 
c  Velocity[Z]                                      0.11436E+02 
c  Pressure     0.79196E-01     726   0.34998E-01   0.10175E+00 0.58696E+01 
c  k            0.30662E+00      22   0.30275E-03   0.14941E-01 0.40927E+02 
c  epsilon      0.33656E+04      12   0.56255E-03   0.56522E+07 0.11253E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -5.9245                             5
a  Local Time Step      4.2274e-08                        280545


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7728          14.356          1.5094         0.24595
v  Velocity[Y]             -25.322          26.334         0.86427         0.59608
v  Velocity[Z]               -39.9          28.437         -0.7706      -0.0017869
v  ǁVelocityǁ            0.0084659          43.392          5.0748          5.1338
v  Pressure                 -58023      1.6297e+05       1.009e+05           85962
v  k                    1.8932e-06          7.6832        0.057164        0.047505
v  epsilon               0.0012369      1.1792e+06          1665.3          37.975
v  TurbVisc             3.4732e-12         0.32658       0.0017003        0.026289
v  CourantNb              0.017202           22841          34.073          5.8546
v  FourierNb              0.022717      2.3655e+05          21.867         0.30753
v  total_pressure       4.4198e+05      6.6297e+05       6.009e+05      5.8596e+05
v  Local Time Step           0.001        0.038397       0.0010033       0.0010233


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.30447      2.3964e+05          55.941          6.1622


 TIME FOR THE TIME STEP              449:        0.86177E+02

===============================================================


 INSTANT    0.450000000E+01   TIME STEP NUMBER             450
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.622356477E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.220991633E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41635E+02 0.54643E+01
   Friction velocity        uet   :  0.27536E-01 0.15916E+02
   Friction velocity        uk    :  0.47726E-01 0.15916E+02
   Dimensionless distance   yplus :  0.17942E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10851
   Nb of faces within the viscous sub-layer     :      12755
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10956E+02      47   0.77137E-01   0.23660E+02 0.28440E+02 
c  Velocity[X]                                      0.40498E+01 
c  Velocity[Y]                                      0.87633E+01 
c  Velocity[Z]                                      0.10847E+02 
c  Pressure     0.78315E-01     804   0.34657E-01   0.10071E+00 0.42628E+01 
c  k            0.30662E+00      20   0.43263E-03   0.19209E-01 0.46463E+02 
c  epsilon      0.33654E+04      13   0.44148E-03   0.52908E+07 0.10841E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.3526e-05                             1
a  epsilon                 -1.6618                             5
a  Local Time Step      4.2274e-08                        280604


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.7817          12.983          1.5095         0.24606
v  Velocity[Y]             -28.064          27.727         0.86158         0.59622
v  Velocity[Z]             -33.281          27.826        -0.76719      -0.0024473
v  ǁVelocityǁ            0.0094763          35.592          5.0753          5.1359
v  Pressure                 -56937      1.6351e+05      1.0146e+05           86375
v  k                    1.8873e-06          7.5777        0.057545        0.047542
v  epsilon               0.0071951      1.1793e+06          1683.8          38.056
v  TurbVisc              3.543e-12         0.32658       0.0017094        0.026298
v  CourantNb                     0           23223          34.088          5.8573
v  FourierNb              0.022746      2.3655e+05          21.868         0.30759
v  total_pressure       4.4306e+05      6.6351e+05      6.0146e+05      5.8637e+05
v  Local Time Step           0.001        0.035464       0.0010033       0.0010232


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70653      2.3886e+05          55.956          6.1649


 TIME FOR THE TIME STEP              450:        0.88312E+02

===============================================================


 INSTANT    0.451000000E+01   TIME STEP NUMBER             451
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.436318968E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221046380E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39818E+02 0.54883E+01
   Friction velocity        uet   :  0.34352E-01 0.17507E+02
   Friction velocity        uk    :  0.47572E-01 0.17507E+02
   Dimensionless distance   yplus :  0.20408E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10882
   Nb of faces within the viscous sub-layer     :      12728
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10961E+02      51   0.77086E-01   0.24326E+02 0.28809E+02 
c  Velocity[X]                                      0.42958E+01 
c  Velocity[Y]                                      0.91048E+01 
c  Velocity[Z]                                      0.10926E+02 
c  Pressure     0.78119E-01     372   0.35175E-01   0.10036E+00 0.12025E+01 
c  k            0.30648E+00      19   0.25649E-03   0.11025E-01 0.35106E+02 
c  epsilon      0.33759E+04      14   0.30224E-03   0.36374E+07 0.89711E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001924                             4
a  epsilon                 -6.4813                            10
a  Local Time Step      4.1834e-08                        280629


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9053            14.7          1.5101         0.24598
v  Velocity[Y]             -24.324          25.896         0.86065         0.59602
v  Velocity[Z]             -42.357          27.703        -0.76484      -0.0027513
v  ǁVelocityǁ            0.0080979          45.732          5.0767          5.1374
v  Pressure                 -55634      1.6352e+05      1.0148e+05           86358
v  k                    4.3675e-07          7.5707        0.057611        0.047584
v  epsilon               0.0010059      1.1927e+06          1685.1          38.107
v  TurbVisc             3.5078e-12         0.32658       0.0017189        0.026306
v  CourantNb                     0           23904          34.086          5.8602
v  FourierNb              0.022773      2.3655e+05           21.87         0.30759
v  total_pressure       4.4437e+05      6.6352e+05      6.0148e+05      5.8636e+05
v  Local Time Step           0.001        0.033292       0.0010032        0.001023


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75336      2.3846e+05          55.956          6.1678


 TIME FOR THE TIME STEP              451:        0.74515E+02

===============================================================


 INSTANT    0.452000000E+01   TIME STEP NUMBER             452
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.226624169E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221091304E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47682E+02 0.54891E+01
   Friction velocity        uet   :  0.36488E-01 0.16383E+02
   Friction velocity        uk    :  0.38765E-01 0.16383E+02
   Dimensionless distance   yplus :  0.20905E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10923
   Nb of faces within the viscous sub-layer     :      12714
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10964E+02      45   0.77186E-01   0.24014E+02 0.28644E+02 
c  Velocity[X]                                      0.43058E+01 
c  Velocity[Y]                                      0.84248E+01 
c  Velocity[Z]                                      0.11284E+02 
c  Pressure     0.79424E-01     560   0.35418E-01   0.10197E+00 0.12292E+01 
c  k            0.30620E+00      18   0.22252E-03   0.81585E-02 0.29986E+02 
c  epsilon      0.33782E+04      13   0.23446E-03   0.14147E+07 0.55872E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.5371e-05                             2
a  epsilon                 -2.2865                             5
a  Local Time Step      4.2115e-08                        280617


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8123          13.101          1.5106         0.24605
v  Velocity[Y]             -25.373          26.676         0.86049         0.59592
v  Velocity[Z]             -37.563           27.79        -0.76266      -0.0029317
v  ǁVelocityǁ            0.0091045          40.211          5.0766          5.1389
v  Pressure                 -53544      1.6353e+05      1.0153e+05           86370
v  k                    3.7049e-07          7.5586        0.057726        0.047619
v  epsilon               0.0068502      1.1921e+06            1687          38.157
v  TurbVisc             3.5454e-12         0.32658       0.0017272        0.026313
v  CourantNb            0.00045393           23744          34.098          5.8621
v  FourierNb              0.022798      2.3655e+05          21.874         0.30777
v  total_pressure       4.4646e+05      6.6353e+05      6.0153e+05      5.8637e+05
v  Local Time Step           0.001        0.036621       0.0010032       0.0010232


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78293      2.3837e+05          55.971          6.1699


 TIME FOR THE TIME STEP              452:        0.84931E+02

===============================================================


 INSTANT    0.453000000E+01   TIME STEP NUMBER             453
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.204266634E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221086085E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39811E+02 0.54562E+01
   Friction velocity        uet   :  0.36384E-01 0.17361E+02
   Friction velocity        uk    :  0.39344E-01 0.17361E+02
   Dimensionless distance   yplus :  0.22153E-02 0.16249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10940
   Nb of faces within the viscous sub-layer     :      12719
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10964E+02      43   0.78040E-01   0.23230E+02 0.28170E+02 
c  Velocity[X]                                      0.42050E+01 
c  Velocity[Y]                                      0.80834E+01 
c  Velocity[Z]                                      0.10941E+02 
c  Pressure     0.76633E-01     940   0.33934E-01   0.98273E-01 0.22445E+01 
c  k            0.30596E+00      17   0.27803E-03   0.99456E-02 0.33435E+02 
c  epsilon      0.33715E+04      13   0.27972E-03   0.14772E+07 0.57268E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.4368e-05                             1
a  epsilon                 -5.2861                             9
a  Local Time Step       4.117e-08                        280630


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.8874          14.711          1.5103         0.24607
v  Velocity[Y]             -25.748          26.708         0.86255         0.59609
v  Velocity[Z]             -40.375          27.819         -0.7625      -0.0036936
v  ǁVelocityǁ             0.010566          43.973          5.0774          5.1407
v  Pressure                 -51126      1.6375e+05      1.0175e+05           86580
v  k                    2.8444e-07          7.3886        0.057691        0.047641
v  epsilon               0.0017745      1.1676e+06          1685.9          38.132
v  TurbVisc             3.4472e-12         0.32658       0.0017315         0.02632
v  CourantNb              0.013378           24289          34.089          5.8634
v  FourierNb               0.02282      2.3655e+05          21.874         0.30778
v  total_pressure       4.4887e+05      6.6375e+05      6.0175e+05      5.8658e+05
v  Local Time Step           0.001        0.032848       0.0010032       0.0010229


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61175      2.3703e+05          55.963          6.1711


 TIME FOR THE TIME STEP              453:        0.10477E+03

===============================================================


 INSTANT    0.454000000E+01   TIME STEP NUMBER             454
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.700141561E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221243029E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43859E+02 0.54638E+01
   Friction velocity        uet   :  0.36690E-01 0.15579E+02
   Friction velocity        uk    :  0.41320E-01 0.15579E+02
   Dimensionless distance   yplus :  0.18882E-02 0.16499E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10952
   Nb of faces within the viscous sub-layer     :      12691
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10971E+02      50   0.77540E-01   0.22715E+02 0.27833E+02 
c  Velocity[X]                                      0.39405E+01 
c  Velocity[Y]                                      0.83533E+01 
c  Velocity[Z]                                      0.10421E+02 
c  Pressure     0.75220E-01     491   0.33291E-01   0.96639E-01 0.11873E+01 
c  k            0.30571E+00      20   0.23614E-03   0.81525E-02 0.30273E+02 
c  epsilon      0.33628E+04      11   0.25175E-03   0.19149E+07 0.65392E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.8411e-05                             1
a  epsilon                 -3.8227                             6
a  Local Time Step      4.2274e-08                        280644


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0047           13.22          1.5113         0.24621
v  Velocity[Y]             -28.834          25.857         0.86613         0.59634
v  Velocity[Z]             -34.096           27.54        -0.76317      -0.0045158
v  ǁVelocityǁ             0.011723          36.476          5.0806          5.1429
v  Pressure                 -51166      1.6377e+05      1.0173e+05           86605
v  k                    3.5868e-08          7.3493        0.057641        0.047646
v  epsilon               0.0043122      1.1812e+06          1682.9          38.096
v  TurbVisc             3.4284e-12         0.32658       0.0017309        0.026326
v  CourantNb              0.019208           23456          34.088          5.8652
v  FourierNb              0.022837      2.3655e+05          21.871         0.30776
v  total_pressure       4.4883e+05      6.6377e+05      6.0173e+05       5.866e+05
v  Local Time Step           0.001        0.031071       0.0010032       0.0010232


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7194      2.3702e+05           55.96           6.173


 TIME FOR THE TIME STEP              454:        0.84043E+02

===============================================================


 INSTANT    0.455000000E+01   TIME STEP NUMBER             455
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.228618287E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221237882E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40306E+02 0.54665E+01
   Friction velocity        uet   :  0.35939E-01 0.16613E+02
   Friction velocity        uk    :  0.47686E-01 0.16613E+02
   Dimensionless distance   yplus :  0.11233E-02 0.17006E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10978
   Nb of faces within the viscous sub-layer     :      12694
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10975E+02      45   0.78150E-01   0.21837E+02 0.27288E+02 
c  Velocity[X]                                      0.38055E+01 
c  Velocity[Y]                                      0.81140E+01 
c  Velocity[Z]                                      0.99174E+01 
c  Pressure     0.74307E-01     549   0.32378E-01   0.95521E-01 0.11542E+01 
c  k            0.30576E+00      22   0.13882E-03   0.74580E-02 0.28648E+02 
c  epsilon      0.33560E+04      11   0.25812E-03   0.15885E+07 0.59473E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00053759                             5
a  epsilon                 -6.4528                             7
a  Local Time Step      4.1777e-08                        280661


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0166          14.999          1.5113         0.24615
v  Velocity[Y]              -26.07          25.432         0.87255         0.59679
v  Velocity[Z]             -43.617          27.959        -0.76463      -0.0054216
v  ǁVelocityǁ             0.010608          47.097          5.0838           5.145
v  Pressure                 -51286      1.6372e+05       1.017e+05           86624
v  k                    1.3672e-08          7.4059        0.057579        0.047647
v  epsilon               0.0035489      1.1728e+06          1684.2          38.067
v  TurbVisc             3.4751e-12         0.32658       0.0017269         0.02633
v  CourantNb              0.011713           23937           34.13          5.8681
v  FourierNb              0.022851      2.3655e+05          21.869         0.30778
v  total_pressure       4.4871e+05      6.6372e+05       6.017e+05      5.8662e+05
v  Local Time Step           0.001        0.025634       0.0010032       0.0010232


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77004      2.3663e+05          55.999          6.1759


 TIME FOR THE TIME STEP              455:        0.89381E+02

===============================================================


 INSTANT    0.456000000E+01   TIME STEP NUMBER             456
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.188587483E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221343163E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49707E+02 0.54955E+01
   Friction velocity        uet   :  0.23745E-01 0.16212E+02
   Friction velocity        uk    :  0.23588E-01 0.16212E+02
   Dimensionless distance   yplus :  0.17485E-02 0.17369E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10990
   Nb of faces within the viscous sub-layer     :      12669
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10983E+02      46   0.79803E-01   0.21868E+02 0.27316E+02 
c  Velocity[X]                                      0.37214E+01 
c  Velocity[Y]                                      0.78022E+01 
c  Velocity[Z]                                      0.10344E+02 
c  Pressure     0.72873E-01     900   0.31762E-01   0.93652E-01 0.40928E+01 
c  k            0.30605E+00      18   0.13686E-03   0.57768E-02 0.25480E+02 
c  epsilon      0.33499E+04      11   0.20821E-03   0.10459E+07 0.48465E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.8994e-05                             1
a  epsilon                 -4.0567                             7
a  Local Time Step      4.0615e-08                        280662


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0142          13.393          1.5101         0.24594
v  Velocity[Y]             -26.701          26.733         0.87836         0.59688
v  Velocity[Z]             -34.717          28.087        -0.76332      -0.0054577
v  ǁVelocityǁ             0.012365          37.107          5.0847          5.1459
v  Pressure                 -51740      1.6315e+05      1.0115e+05           86226
v  k                    4.2003e-08          7.3589         0.05746        0.047653
v  epsilon               0.0030451      1.2009e+06          1677.2          38.063
v  TurbVisc             3.3951e-12         0.32658       0.0017222        0.026333
v  CourantNb              0.017504           24621          34.153          5.8703
v  FourierNb               0.02286      2.3655e+05          21.869         0.30779
v  total_pressure       4.4826e+05      6.6315e+05      6.0115e+05      5.8623e+05
v  Local Time Step           0.001        0.028198       0.0010032       0.0010239


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72113      2.3733e+05          56.021           6.178


 TIME FOR THE TIME STEP              456:        0.95276E+02

===============================================================


 INSTANT    0.457000000E+01   TIME STEP NUMBER             457
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.447103878E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221359624E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41986E+02 0.54431E+01
   Friction velocity        uet   :  0.29570E-01 0.15916E+02
   Friction velocity        uk    :  0.29490E-01 0.15916E+02
   Dimensionless distance   yplus :  0.14199E-02 0.17881E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11006
   Nb of faces within the viscous sub-layer     :      12650
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10983E+02      45   0.81194E-01   0.21163E+02 0.26877E+02 
c  Velocity[X]                                      0.36855E+01 
c  Velocity[Y]                                      0.77777E+01 
c  Velocity[Z]                                      0.96998E+01 
c  Pressure     0.71588E-01     567   0.30932E-01   0.91992E-01 0.13448E+01 
c  k            0.30649E+00      20   0.18737E-03   0.49361E-02 0.23470E+02 
c  epsilon      0.33380E+04      11   0.22667E-03   0.14308E+07 0.56769E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.9542e-05                             2
a  epsilon                 -3.6421                             8
a  Local Time Step      3.9634e-08                        280634


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0484          14.683          1.5115         0.24599
v  Velocity[Y]             -24.934          25.499         0.88433         0.59717
v  Velocity[Z]             -39.559          27.735        -0.76148      -0.0059084
v  ǁVelocityǁ             0.012045          43.156          5.0876           5.147
v  Pressure                 -51791      1.6308e+05       1.011e+05           86237
v  k                    9.3893e-07          7.4525        0.057475        0.047664
v  epsilon              0.00087791      1.1546e+06          1678.8          38.074
v  TurbVisc             3.3843e-12         0.32658         0.00172        0.026335
v  CourantNb              0.016392           25231          34.147          5.8719
v  FourierNb              0.022866      2.3655e+05          21.868         0.30786
v  total_pressure       4.4821e+05      6.6308e+05       6.011e+05      5.8624e+05
v  Local Time Step           0.001        0.024565       0.0010033       0.0010242


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58517      2.3678e+05          56.016          6.1797


 TIME FOR THE TIME STEP              457:        0.99064E+02

===============================================================


 INSTANT    0.458000000E+01   TIME STEP NUMBER             458
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.101011999E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221435283E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39574E+02 0.54931E+01
   Friction velocity        uet   :  0.37142E-01 0.19804E+02
   Friction velocity        uk    :  0.40457E-01 0.19804E+02
   Dimensionless distance   yplus :  0.25270E-02 0.18550E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10991
   Nb of faces within the viscous sub-layer     :      12642
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10987E+02      47   0.77368E-01   0.20762E+02 0.26617E+02 
c  Velocity[X]                                      0.36552E+01 
c  Velocity[Y]                                      0.76877E+01 
c  Velocity[Z]                                      0.94194E+01 
c  Pressure     0.70468E-01    1055   0.30925E-01   0.90850E-01 0.58161E+01 
c  k            0.30667E+00      17   0.16882E-03   0.44922E-02 0.22124E+02 
c  epsilon      0.33420E+04      11   0.29213E-03   0.45834E+07 0.10133E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.1408e-05                             3
a  epsilon                 -3.9066                             5
a  Local Time Step      4.0073e-08                        280626


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0007          13.413          1.5122         0.24602
v  Velocity[Y]             -26.529          25.828         0.89047         0.59688
v  Velocity[Z]             -34.221          28.166         -0.7583      -0.0053321
v  ǁVelocityǁ              0.01212          36.821          5.0913          5.1466
v  Pressure                 -52207       1.623e+05      1.0036e+05           85656
v  k                    1.8414e-06          7.5909        0.057362        0.047673
v  epsilon               0.0062505      1.2037e+06          1675.5           38.08
v  TurbVisc             3.4649e-12         0.32658       0.0017181        0.026337
v  CourantNb              0.016162           24955          34.169          5.8731
v  FourierNb              0.022869      2.3655e+05          21.869         0.30791
v  total_pressure       4.4779e+05       6.623e+05      6.0036e+05      5.8566e+05
v  Local Time Step           0.001        0.027021       0.0010033       0.0010243


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67649      2.3729e+05          56.038           6.181


 TIME FOR THE TIME STEP              458:        0.97730E+02

===============================================================


 INSTANT    0.459000000E+01   TIME STEP NUMBER             459
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.302363004E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221210598E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43510E+02 0.54856E+01
   Friction velocity        uet   :  0.34348E-01 0.17873E+02
   Friction velocity        uk    :  0.38915E-01 0.17873E+02
   Dimensionless distance   yplus :  0.20019E-02 0.17635E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10997
   Nb of faces within the viscous sub-layer     :      12662
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10985E+02      48   0.77390E-01   0.19839E+02 0.25999E+02 
c  Velocity[X]                                      0.35753E+01 
c  Velocity[Y]                                      0.70446E+01 
c  Velocity[Z]                                      0.92196E+01 
c  Pressure     0.68373E-01     606   0.29625E-01   0.88264E-01 0.11195E+01 
c  k            0.30683E+00      19   0.30015E-03   0.76256E-02 0.24765E+02 
c  epsilon      0.33263E+04      11   0.39835E-03   0.61986E+07 0.11854E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.7317e-05                             2
a  epsilon                 -3.6162                             5
a  Local Time Step      3.7552e-08                        280614


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1826          14.684          1.5135         0.24591
v  Velocity[Y]              -25.07          24.137         0.89504         0.59672
v  Velocity[Z]             -41.704          27.981        -0.75747      -0.0050889
v  ǁVelocityǁ             0.012755          45.176           5.096          5.1476
v  Pressure                 -52080      1.6224e+05      1.0033e+05           85682
v  k                    9.3113e-07          7.6554        0.057301        0.047675
v  epsilon               0.0061965      1.1751e+06          1668.2          38.079
v  TurbVisc             3.4118e-12         0.32658       0.0017165        0.026338
v  CourantNb             0.0076114           26630          34.207          5.8724
v  FourierNb              0.022868      2.3655e+05          21.869         0.30797
v  total_pressure       4.4792e+05      6.6224e+05      6.0033e+05      5.8568e+05
v  Local Time Step           0.001         0.02425       0.0010033       0.0010243


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7286      2.3709e+05          56.076          6.1804


 TIME FOR THE TIME STEP              459:        0.94872E+02

===============================================================


 INSTANT    0.460000000E+01   TIME STEP NUMBER             460
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.174771579E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221364264E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46133E+02 0.61661E+01
   Friction velocity        uet   :  0.33186E-01 0.19014E+02
   Friction velocity        uk    :  0.32951E-01 0.19014E+02
   Dimensionless distance   yplus :  0.21591E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11008
   Nb of faces within the viscous sub-layer     :      12650
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10987E+02      43   0.77465E-01   0.19636E+02 0.25858E+02 
c  Velocity[X]                                      0.35348E+01 
c  Velocity[Y]                                      0.68776E+01 
c  Velocity[Z]                                      0.92236E+01 
c  Pressure     0.68824E-01     883   0.29619E-01   0.88910E-01 0.26455E+01 
c  k            0.30718E+00      20   0.31545E-03   0.14575E-01 0.40280E+02 
c  epsilon      0.33174E+04      12   0.23872E-03   0.28159E+07 0.80066E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010571                             3
a  epsilon                 -3.2848                             3
a  Local Time Step      3.8911e-08                        280578


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1225          13.303          1.5122         0.24576
v  Velocity[Y]             -26.808           24.64         0.89664         0.59672
v  Velocity[Z]             -35.791          28.775        -0.75469      -0.0045262
v  ǁVelocityǁ            0.0074994          38.408          5.0975          5.1475
v  Pressure                 -52256      1.6188e+05      1.0002e+05           85438
v  k                    1.1694e-06          7.7523        0.057159        0.047667
v  epsilon               0.0060655      1.1881e+06          1657.1          38.072
v  TurbVisc             3.3597e-12         0.32658       0.0017147        0.026339
v  CourantNb             0.0094937           25700          34.239          5.8762
v  FourierNb              0.022866      2.3655e+05          21.869         0.30787
v  total_pressure       4.4774e+05      6.6188e+05      6.0002e+05      5.8544e+05
v  Local Time Step           0.001        0.026675       0.0010034       0.0010251


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48769      2.3707e+05          56.107           6.184


 TIME FOR THE TIME STEP              460:        0.81698E+02

===============================================================


 INSTANT    0.461000000E+01   TIME STEP NUMBER             461
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.464840070E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221305171E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47112E+02 0.64707E+01
   Friction velocity        uet   :  0.34494E-01 0.20265E+02
   Friction velocity        uk    :  0.37192E-01 0.20265E+02
   Dimensionless distance   yplus :  0.15820E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11028
   Nb of faces within the viscous sub-layer     :      12645
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10984E+02      57   0.77681E-01   0.18735E+02 0.25282E+02 
c  Velocity[X]                                      0.33772E+01 
c  Velocity[Y]                                      0.64950E+01 
c  Velocity[Z]                                      0.88633E+01 
c  Pressure     0.68037E-01     480   0.29006E-01   0.87841E-01 0.86856E+00 
c  k            0.30732E+00      18   0.20631E-03   0.83095E-02 0.30448E+02 
c  epsilon      0.33090E+04      10   0.21811E-03   0.94027E+06 0.46297E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0004489                             5
a  epsilon                 -3.9125                             4
a  Local Time Step      3.8295e-08                        280605


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2064          14.625          1.5118         0.24569
v  Velocity[Y]             -26.333           24.86         0.89644         0.59699
v  Velocity[Z]             -39.295          31.559        -0.75093      -0.0042399
v  ǁVelocityǁ            0.0090976          42.895          5.0953          5.1479
v  Pressure                 -52146      1.6186e+05      1.0002e+05           85452
v  k                    1.8179e-06          7.9141        0.057109        0.047645
v  epsilon               0.0061415      1.1881e+06          1655.7           38.03
v  TurbVisc             3.2947e-12         0.32658       0.0017132        0.026338
v  CourantNb                     0           26113          34.247          5.8768
v  FourierNb              0.022864      2.3655e+05          21.868         0.30781
v  total_pressure       4.4785e+05      6.6186e+05      6.0002e+05      5.8545e+05
v  Local Time Step           0.001        0.029342       0.0010034       0.0010253


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88037      2.3655e+05          56.115          6.1846


 TIME FOR THE TIME STEP              461:        0.74951E+02

===============================================================


 INSTANT    0.462000000E+01   TIME STEP NUMBER             462
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.141908323E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221267058E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38326E+02 0.65003E+01
   Friction velocity        uet   :  0.27999E-01 0.18957E+02
   Friction velocity        uk    :  0.27824E-01 0.18957E+02
   Dimensionless distance   yplus :  0.17264E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11019
   Nb of faces within the viscous sub-layer     :      12653
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10983E+02      44   0.78786E-01   0.18598E+02 0.25185E+02 
c  Velocity[X]                                      0.34821E+01 
c  Velocity[Y]                                      0.63446E+01 
c  Velocity[Z]                                      0.87708E+01 
c  Pressure     0.66259E-01     519   0.28165E-01   0.85562E-01 0.77612E+00 
c  k            0.30746E+00      17   0.14508E-03   0.41943E-02 0.21666E+02 
c  epsilon      0.33142E+04      12   0.24425E-03   0.35839E+07 0.90328E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020189                             5
a  epsilon                 -4.5043                             6
a  Local Time Step      3.8187e-08                        280577


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.233           13.29          1.5102         0.24577
v  Velocity[Y]             -28.811          25.134         0.89477         0.59737
v  Velocity[Z]             -36.292          33.446        -0.74747      -0.0041836
v  ǁVelocityǁ            0.0072033           38.67          5.0944          5.1482
v  Pressure                 -51925      1.6181e+05      1.0002e+05           85462
v  k                    1.8325e-06          7.8917        0.056986         0.04762
v  epsilon               0.0061582      1.1989e+06          1653.1          37.983
v  TurbVisc             3.3086e-12         0.32658       0.0017118        0.026337
v  CourantNb              0.028446           26187          34.183          5.8779
v  FourierNb              0.022861      2.3655e+05           21.87         0.30798
v  total_pressure       4.4808e+05      6.6181e+05      6.0002e+05      5.8546e+05
v  Local Time Step           0.001        0.030965       0.0010034        0.001026


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75082      2.3694e+05          56.052          6.1858


 TIME FOR THE TIME STEP              462:        0.78264E+02

===============================================================


 INSTANT    0.463000000E+01   TIME STEP NUMBER             463
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.161911886E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221267191E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46313E+02 0.66468E+01
   Friction velocity        uet   :  0.22638E-01 0.16718E+02
   Friction velocity        uk    :  0.22613E-01 0.16718E+02
   Dimensionless distance   yplus :  0.20933E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11035
   Nb of faces within the viscous sub-layer     :      12636
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10980E+02      42   0.77888E-01   0.18221E+02 0.24928E+02 
c  Velocity[X]                                      0.33618E+01 
c  Velocity[Y]                                      0.63686E+01 
c  Velocity[Z]                                      0.84904E+01 
c  Pressure     0.65271E-01     356   0.27485E-01   0.84458E-01 0.75194E+00 
c  k            0.30741E+00      18   0.11820E-03   0.50365E-02 0.23499E+02 
c  epsilon      0.32963E+04      10   0.25433E-03   0.44823E+07 0.10144E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019242                             5
a  epsilon                 -1.6647                             4
a  Local Time Step      3.7812e-08                        280567


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2614           14.92          1.5103         0.24564
v  Velocity[Y]             -25.902          24.676         0.89186         0.59692
v  Velocity[Z]             -42.443          33.575         -0.7439      -0.0043558
v  ǁVelocityǁ            0.0098169          45.955          5.0918          5.1483
v  Pressure                 -51684      1.6179e+05      1.0002e+05           85473
v  k                    1.7548e-06          7.9523         0.05698        0.047596
v  epsilon               0.0061995      1.1598e+06          1647.6          37.961
v  TurbVisc             3.3455e-12         0.32658       0.0017103        0.026335
v  CourantNb             0.0095733           26447          34.158          5.8781
v  FourierNb              0.022859      2.3655e+05          21.869           0.308
v  total_pressure       4.4832e+05      6.6179e+05      6.0002e+05      5.8547e+05
v  Local Time Step           0.001        0.034062       0.0010035       0.0010266


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89154      2.3802e+05          56.027          6.1861


 TIME FOR THE TIME STEP              463:        0.66498E+02

===============================================================


 INSTANT    0.464000000E+01   TIME STEP NUMBER             464
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.533634587E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221263533E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47188E+02 0.68433E+01
   Friction velocity        uet   :  0.35702E-01 0.15722E+02
   Friction velocity        uk    :  0.43651E-01 0.15722E+02
   Dimensionless distance   yplus :  0.17793E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11032
   Nb of faces within the viscous sub-layer     :      12664
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10980E+02      43   0.77546E-01   0.18132E+02 0.24864E+02 
c  Velocity[X]                                      0.34560E+01 
c  Velocity[Y]                                      0.59399E+01 
c  Velocity[Z]                                      0.87359E+01 
c  Pressure     0.65475E-01     368   0.27324E-01   0.84744E-01 0.79920E+00 
c  k            0.30807E+00      19   0.11669E-03   0.29428E-02 0.17771E+02 
c  epsilon      0.32915E+04      10   0.21818E-03   0.19825E+07 0.67588E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001208                             3
a  epsilon                 -1.6282                             3
a  Local Time Step      3.8657e-08                        280582


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2106          13.282          1.5111         0.24562
v  Velocity[Y]              -28.12          26.235         0.88626          0.5962
v  Velocity[Z]             -34.997          31.495        -0.74024      -0.0046939
v  ǁVelocityǁ            0.0088456          37.589          5.0892           5.149
v  Pressure                 -51260      1.6178e+05      1.0002e+05           85487
v  k                    1.6904e-06          7.9169        0.056835        0.047587
v  epsilon               0.0061349      1.1956e+06          1639.4          37.934
v  TurbVisc             3.1564e-12         0.32658         0.00171        0.026333
v  CourantNb              0.029727           25868          34.104          5.8786
v  FourierNb               0.02286      2.3655e+05          21.869         0.30799
v  total_pressure       4.4874e+05      6.6178e+05      6.0002e+05      5.8549e+05
v  Local Time Step           0.001        0.037468       0.0010035       0.0010264


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61233      2.3796e+05          55.973          6.1866


 TIME FOR THE TIME STEP              464:        0.62186E+02

===============================================================


 INSTANT    0.465000000E+01   TIME STEP NUMBER             465
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.382056804E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221294800E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45347E+02 0.72348E+01
   Friction velocity        uet   :  0.35337E-01 0.15226E+02
   Friction velocity        uk    :  0.47172E-01 0.15226E+02
   Dimensionless distance   yplus :  0.11719E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11015
   Nb of faces within the viscous sub-layer     :      12683
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10977E+02      42   0.74181E-01   0.17915E+02 0.24724E+02 
c  Velocity[X]                                      0.33530E+01 
c  Velocity[Y]                                      0.60053E+01 
c  Velocity[Z]                                      0.85571E+01 
c  Pressure     0.64257E-01     353   0.26679E-01   0.83167E-01 0.82053E+00 
c  k            0.30847E+00      25   0.12506E-03   0.29378E-02 0.17800E+02 
c  epsilon      0.32845E+04      12   0.19252E-03   0.13948E+07 0.56891E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017288                             3
a  epsilon                 -1.5318                             3
a  Local Time Step      3.8958e-08                        280571


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2598          14.774          1.5111          0.2454
v  Velocity[Y]             -27.208           27.12         0.88073         0.59591
v  Velocity[Z]             -39.423          27.694        -0.73774      -0.0052312
v  ǁVelocityǁ             0.011769          43.047          5.0857          5.1492
v  Pressure                 -51062      1.6173e+05      1.0002e+05           85498
v  k                    1.7944e-07          7.9657        0.056809        0.047585
v  epsilon               0.0060188      1.1866e+06          1636.1          37.928
v  TurbVisc             3.3054e-12         0.32658       0.0017101        0.026332
v  CourantNb               0.00135           25668           34.07          5.8788
v  FourierNb              0.022861      2.3655e+05          21.868           0.308
v  total_pressure       4.4894e+05      6.6173e+05      6.0002e+05       5.855e+05
v  Local Time Step           0.001        0.029056       0.0010036       0.0010267


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56287      2.3758e+05          55.938          6.1868


 TIME FOR THE TIME STEP              465:        0.71806E+02

===============================================================


 INSTANT    0.466000000E+01   TIME STEP NUMBER             466
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.117313613E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221359442E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38771E+02 0.66523E+01
   Friction velocity        uet   :  0.35729E-01 0.18955E+02
   Friction velocity        uk    :  0.40389E-01 0.18955E+02
   Dimensionless distance   yplus :  0.24187E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11029
   Nb of faces within the viscous sub-layer     :      12671
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10980E+02      44   0.75325E-01   0.17492E+02 0.24422E+02 
c  Velocity[X]                                      0.31387E+01 
c  Velocity[Y]                                      0.60246E+01 
c  Velocity[Z]                                      0.83282E+01 
c  Pressure     0.63209E-01     698   0.26494E-01   0.81974E-01 0.34492E+01 
c  k            0.30819E+00      19   0.15037E-03   0.32338E-02 0.19207E+02 
c  epsilon      0.32863E+04      13   0.19986E-03   0.78816E+06 0.42747E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011429                             3
a  epsilon                 -3.2039                             3
a  Local Time Step      3.8557e-08                        280577


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2109           13.57          1.5126         0.24531
v  Velocity[Y]             -26.334           26.91         0.87436         0.59563
v  Velocity[Z]             -37.152          29.925        -0.73473      -0.0050025
v  ǁVelocityǁ             0.007911          39.565          5.0819           5.149
v  Pressure                 -51202      1.6124e+05           99572           85155
v  k                    4.2947e-07          7.9561        0.056844        0.047576
v  epsilon               0.0055277      1.1722e+06          1634.4          37.933
v  TurbVisc              3.519e-12         0.32658       0.0017115         0.02633
v  CourantNb             0.0070113           25936          34.016          5.8793
v  FourierNb              0.022865      2.3655e+05          21.869         0.30806
v  total_pressure        4.488e+05      6.6124e+05      5.9957e+05      5.8515e+05
v  Local Time Step           0.001        0.029716       0.0010037       0.0010275


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66862      2.3679e+05          55.885          6.1874


 TIME FOR THE TIME STEP              466:        0.79790E+02

===============================================================


 INSTANT    0.467000000E+01   TIME STEP NUMBER             467
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.582306201E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221327144E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43744E+02 0.57777E+01
   Friction velocity        uet   :  0.35653E-01 0.15795E+02
   Friction velocity        uk    :  0.35415E-01 0.15795E+02
   Dimensionless distance   yplus :  0.19845E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11040
   Nb of faces within the viscous sub-layer     :      12685
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10976E+02      43   0.78116E-01   0.18218E+02 0.24891E+02 
c  Velocity[X]                                      0.31976E+01 
c  Velocity[Y]                                      0.62014E+01 
c  Velocity[Z]                                      0.88194E+01 
c  Pressure     0.64971E-01     373   0.27418E-01   0.84140E-01 0.88162E+00 
c  k            0.30729E+00      18   0.17482E-03   0.45713E-02 0.22583E+02 
c  epsilon      0.32888E+04      11   0.26479E-03   0.34867E+07 0.89782E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011492                             3
a  epsilon                 -2.0525                             2
a  Local Time Step      3.7741e-08                        280565


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2625          15.922          1.5123         0.24539
v  Velocity[Y]             -24.495          27.482          0.8687         0.59538
v  Velocity[Z]             -46.468           30.49        -0.73227      -0.0050666
v  ǁVelocityǁ            0.0091921          50.102          5.0762          5.1483
v  Pressure                 -51165      1.6117e+05           99559           85168
v  k                    1.8061e-06          7.6217        0.056832        0.047562
v  epsilon               0.0052788      1.1769e+06          1635.7          37.888
v  TurbVisc             3.2017e-12         0.32658       0.0017122        0.026329
v  CourantNb              0.021641           26496          33.974          5.8791
v  FourierNb              0.022869      2.3655e+05          21.869         0.30817
v  total_pressure       4.4883e+05      6.6117e+05      5.9956e+05      5.8517e+05
v  Local Time Step           0.001        0.032687       0.0010038       0.0010285


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73995      2.3678e+05          55.843          6.1873


 TIME FOR THE TIME STEP              467:        0.62739E+02

===============================================================


 INSTANT    0.468000000E+01   TIME STEP NUMBER             468
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.140120166E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221338514E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54409E+02 0.54828E+01
   Friction velocity        uet   :  0.33479E-01 0.15038E+02
   Friction velocity        uk    :  0.38675E-01 0.15038E+02
   Dimensionless distance   yplus :  0.16376E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11053
   Nb of faces within the viscous sub-layer     :      12701
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10974E+02      49   0.76267E-01   0.18521E+02 0.25132E+02 
c  Velocity[X]                                      0.33434E+01 
c  Velocity[Y]                                      0.62200E+01 
c  Velocity[Z]                                      0.89580E+01 
c  Pressure     0.63301E-01     358   0.26797E-01   0.82023E-01 0.90087E+00 
c  k            0.30633E+00      17   0.16208E-03   0.42045E-02 0.21940E+02 
c  epsilon      0.32850E+04      10   0.34922E-03   0.47448E+07 0.10477E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.2773e-05                             2
a  epsilon                 -2.0891                             4
a  Local Time Step      3.7152e-08                        280569


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1805          13.284          1.5132         0.24543
v  Velocity[Y]             -25.592          25.756         0.86179         0.59526
v  Velocity[Z]             -34.166          28.482        -0.73143      -0.0053796
v  ǁVelocityǁ            0.0066244          36.777          5.0718          5.1479
v  Pressure                 -51347      1.6113e+05           99545           85183
v  k                    1.8367e-06          7.5079        0.056753        0.047547
v  epsilon                0.004287      1.1757e+06          1635.6          37.845
v  TurbVisc             3.2913e-12         0.32658       0.0017118        0.026327
v  CourantNb             0.0081362           26917          33.896           5.878
v  FourierNb              0.022872      2.3655e+05          21.868         0.30819
v  total_pressure       4.4865e+05      6.6113e+05      5.9954e+05      5.8518e+05
v  Local Time Step           0.001        0.033357       0.0010038        0.001029


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64709       2.368e+05          55.764          6.1862


 TIME FOR THE TIME STEP              468:        0.67268E+02

===============================================================


 INSTANT    0.469000000E+01   TIME STEP NUMBER             469
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.400577856E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221367473E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43397E+02 0.54542E+01
   Friction velocity        uet   :  0.35360E-01 0.16609E+02
   Friction velocity        uk    :  0.43203E-01 0.16609E+02
   Dimensionless distance   yplus :  0.15045E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11039
   Nb of faces within the viscous sub-layer     :      12717
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10971E+02      46   0.75489E-01   0.17260E+02 0.24257E+02 
c  Velocity[X]                                      0.31341E+01 
c  Velocity[Y]                                      0.59726E+01 
c  Velocity[Z]                                      0.81535E+01 
c  Pressure     0.63481E-01     379   0.27197E-01   0.82214E-01 0.80543E+00 
c  k            0.30598E+00      15   0.13699E-03   0.31271E-02 0.18663E+02 
c  epsilon      0.32847E+04      10   0.27839E-03   0.23854E+07 0.74532E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -8.201e-05                             3
a  epsilon                 -1.8072                             3
a  Local Time Step      3.6858e-08                        280564


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1761          15.092          1.5119          0.2452
v  Velocity[Y]             -26.241          26.418         0.85473         0.59508
v  Velocity[Z]              -40.38          28.043        -0.73064      -0.0057045
v  ǁVelocityǁ            0.0060747           44.05          5.0662          5.1475
v  Pressure                 -51637       1.611e+05           99528           85189
v  k                    1.8847e-06           7.505        0.056708        0.047544
v  epsilon                 0.00571      1.1733e+06          1631.3          37.815
v  TurbVisc             3.4188e-12         0.32658       0.0017106        0.026326
v  CourantNb              0.021541           27131          33.876          5.8772
v  FourierNb              0.022874      2.3655e+05          21.868         0.30817
v  total_pressure       4.4836e+05       6.611e+05      5.9953e+05      5.8519e+05
v  Local Time Step           0.001        0.035116       0.0010037       0.0010286


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49278      2.3724e+05          55.744          6.1854


 TIME FOR THE TIME STEP              469:        0.68462E+02

===============================================================


 INSTANT    0.470000000E+01   TIME STEP NUMBER             470
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.236172953E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221393606E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40944E+02 0.54381E+01
   Friction velocity        uet   :  0.32481E-01 0.18589E+02
   Friction velocity        uk    :  0.39206E-01 0.18589E+02
   Dimensionless distance   yplus :  0.23720E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11044
   Nb of faces within the viscous sub-layer     :      12727
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10972E+02      49   0.76130E-01   0.17599E+02 0.24487E+02 
c  Velocity[X]                                      0.31452E+01 
c  Velocity[Y]                                      0.62318E+01 
c  Velocity[Z]                                      0.82220E+01 
c  Pressure     0.62730E-01     467   0.27017E-01   0.81294E-01 0.82935E+00 
c  k            0.30595E+00      17   0.73019E-04   0.26341E-02 0.17358E+02 
c  epsilon      0.32920E+04      10   0.25863E-03   0.24271E+07 0.74968E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.3306e-05                             3
a  epsilon                 -2.3844                             3
a  Local Time Step      3.6977e-08                        280559


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1962          13.519          1.5128         0.24527
v  Velocity[Y]             -29.403          25.861         0.84747         0.59508
v  Velocity[Z]             -36.003          30.957        -0.73191      -0.0059846
v  ǁVelocityǁ             0.012301          38.416           5.063           5.147
v  Pressure                 -51796      1.6105e+05           99480           85180
v  k                    1.8434e-06          7.5019        0.056701         0.04755
v  epsilon               0.0057685      1.1705e+06          1635.1          37.816
v  TurbVisc             3.3804e-12         0.32658       0.0017098        0.026325
v  CourantNb             0.0037501           27044          33.807          5.8764
v  FourierNb              0.022874      2.3655e+05          21.868         0.30817
v  total_pressure        4.482e+05      6.6105e+05      5.9948e+05      5.8518e+05
v  Local Time Step           0.001        0.035897       0.0010038        0.001029


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47309      2.3767e+05          55.675          6.1846


 TIME FOR THE TIME STEP              470:        0.77515E+02

===============================================================


 INSTANT    0.471000000E+01   TIME STEP NUMBER             471
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.260016110E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221440178E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41182E+02 0.54040E+01
   Friction velocity        uet   :  0.36834E-01 0.16784E+02
   Friction velocity        uk    :  0.47656E-01 0.16784E+02
   Dimensionless distance   yplus :  0.14133E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11037
   Nb of faces within the viscous sub-layer     :      12760
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10970E+02      43   0.76120E-01   0.18453E+02 0.25081E+02 
c  Velocity[X]                                      0.32083E+01 
c  Velocity[Y]                                      0.65584E+01 
c  Velocity[Z]                                      0.86862E+01 
c  Pressure     0.62616E-01     410   0.27060E-01   0.81165E-01 0.75218E+00 
c  k            0.30545E+00      16   0.14723E-03   0.48890E-02 0.23742E+02 
c  epsilon      0.32862E+04      10   0.38051E-03   0.18678E+07 0.65934E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.2045e-05                             3
a  epsilon                 -2.0653                             2
a  Local Time Step      3.6687e-08                        280528


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1988            16.1          1.5132         0.24533
v  Velocity[Y]             -26.365          26.211         0.84022         0.59515
v  Velocity[Z]             -43.726          31.483        -0.73437      -0.0064723
v  ǁVelocityǁ             0.010869          47.148          5.0596          5.1469
v  Pressure                 -51762        1.61e+05           99457           85178
v  k                     1.961e-06          7.4976        0.056625        0.047551
v  epsilon               0.0057441      1.1453e+06          1635.1          37.767
v  TurbVisc             3.4331e-12         0.32658       0.0017086        0.026325
v  CourantNb             0.0059787           27257          33.791          5.8756
v  FourierNb              0.022872      2.3655e+05          21.866         0.30826
v  total_pressure       4.4824e+05        6.61e+05      5.9946e+05      5.8518e+05
v  Local Time Step           0.001        0.038217       0.0010038       0.0010294


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41316      2.3661e+05          55.657          6.1839


 TIME FOR THE TIME STEP              471:        0.72806E+02

===============================================================


 INSTANT    0.472000000E+01   TIME STEP NUMBER             472
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.727017953E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221499089E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.48929E+02 0.54405E+01
   Friction velocity        uet   :  0.37444E-01 0.15626E+02
   Friction velocity        uk    :  0.38269E-01 0.15626E+02
   Dimensionless distance   yplus :  0.15590E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11036
   Nb of faces within the viscous sub-layer     :      12775
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10972E+02      44   0.76058E-01   0.18812E+02 0.25315E+02 
c  Velocity[X]                                      0.33060E+01 
c  Velocity[Y]                                      0.65874E+01 
c  Velocity[Z]                                      0.89185E+01 
c  Pressure     0.64359E-01     824   0.27554E-01   0.83357E-01 0.38942E+01 
c  k            0.30517E+00      17   0.13190E-03   0.36942E-02 0.20577E+02 
c  epsilon      0.32877E+04      11   0.23275E-03   0.13874E+07 0.56818E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011025                             3
a  epsilon                 -79.617                             4
a  Local Time Step      3.6729e-08                        280506


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1415          13.153           1.513          0.2454
v  Velocity[Y]             -25.188          26.535         0.83395         0.59518
v  Velocity[Z]             -32.785          33.948         -0.7364      -0.0059097
v  ǁVelocityǁ            0.0093507          36.543          5.0584           5.146
v  Pressure                 -52204      1.6047e+05           98949           84785
v  k                    1.7701e-06          7.6346        0.056512        0.047556
v  epsilon               0.0024043      1.1788e+06          1627.3          37.727
v  TurbVisc             3.5225e-12         0.32658        0.001708        0.026326
v  CourantNb              0.016455           27226          33.755          5.8754
v  FourierNb              0.022866      2.3655e+05          21.866         0.30824
v  total_pressure        4.478e+05      6.6047e+05      5.9895e+05      5.8478e+05
v  Local Time Step           0.001        0.037817       0.0010038       0.0010289


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier            0.45      2.3793e+05          55.621          6.1836


 TIME FOR THE TIME STEP              472:        0.91738E+02

===============================================================


 INSTANT    0.473000000E+01   TIME STEP NUMBER             473
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.158884694E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221463949E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41815E+02 0.54152E+01
   Friction velocity        uet   :  0.36140E-01 0.18161E+02
   Friction velocity        uk    :  0.42796E-01 0.18161E+02
   Dimensionless distance   yplus :  0.16052E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11019
   Nb of faces within the viscous sub-layer     :      12775
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10967E+02      43   0.74373E-01   0.18510E+02 0.25117E+02 
c  Velocity[X]                                      0.33913E+01 
c  Velocity[Y]                                      0.65921E+01 
c  Velocity[Z]                                      0.85265E+01 
c  Pressure     0.64312E-01     442   0.27244E-01   0.83286E-01 0.86488E+00 
c  k            0.30518E+00      17   0.10526E-03   0.33331E-02 0.19538E+02 
c  epsilon      0.32677E+04      10   0.23821E-03   0.18221E+07 0.65422E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.6799e-05                             3
a  epsilon                 -1.6067                             4
a  Local Time Step      3.7311e-08                        280512


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1483          15.652          1.5123         0.24528
v  Velocity[Y]             -24.934           24.76         0.82832         0.59539
v  Velocity[Z]             -42.306          31.788        -0.74003      -0.0054392
v  ǁVelocityǁ            0.0086062          46.092          5.0588          5.1449
v  Pressure                 -52161      1.6046e+05           98925           84757
v  k                    1.7897e-06          7.8696        0.056509        0.047568
v  epsilon               0.0011242      1.1504e+06          1622.3          37.727
v  TurbVisc             3.2064e-12         0.32658       0.0017079        0.026327
v  CourantNb              0.073638           26802          33.762          5.8747
v  FourierNb               0.02286      2.3655e+05          21.866         0.30819
v  total_pressure       4.4784e+05      6.6046e+05      5.9892e+05      5.8476e+05
v  Local Time Step           0.001        0.038882       0.0010038       0.0010289


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48383      2.3758e+05          55.628          6.1829


 TIME FOR THE TIME STEP              473:        0.76849E+02

===============================================================


 INSTANT    0.474000000E+01   TIME STEP NUMBER             474
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.548102100E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221402323E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45267E+02 0.54269E+01
   Friction velocity        uet   :  0.36577E-01 0.16115E+02
   Friction velocity        uk    :  0.36347E-01 0.16115E+02
   Dimensionless distance   yplus :  0.18653E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11006
   Nb of faces within the viscous sub-layer     :      12797
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10964E+02      46   0.75924E-01   0.18402E+02 0.25048E+02 
c  Velocity[X]                                      0.32987E+01 
c  Velocity[Y]                                      0.66196E+01 
c  Velocity[Z]                                      0.84833E+01 
c  Pressure     0.62509E-01     452   0.26535E-01   0.80890E-01 0.96396E+00 
c  k            0.30526E+00      19   0.11994E-03   0.32331E-02 0.19309E+02 
c  epsilon      0.32819E+04      12   0.33366E-03   0.29357E+07 0.82595E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.1214e-05                             2
a  epsilon                 -4.4753                             5
a  Local Time Step      3.7393e-08                        280501


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0835          14.208          1.5111         0.24513
v  Velocity[Y]             -29.867          26.588          0.8247         0.59563
v  Velocity[Z]               -36.2          28.035        -0.74442      -0.0049401
v  ǁVelocityǁ            0.0084828          39.625          5.0615          5.1446
v  Pressure                 -52113      1.6042e+05           98919           84736
v  k                    1.7477e-06          8.0668        0.056527        0.047589
v  epsilon               0.0028947      1.1662e+06          1629.6          37.754
v  TurbVisc             3.3024e-12         0.32658       0.0017083         0.02633
v  CourantNb              0.016185           26743          33.771          5.8737
v  FourierNb              0.022853      2.3655e+05          21.865         0.30821
v  total_pressure       4.4789e+05      6.6042e+05      5.9892e+05      5.8474e+05
v  Local Time Step           0.001        0.041859       0.0010038       0.0010295


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65844       2.392e+05          55.637           6.182


 TIME FOR THE TIME STEP              474:        0.74880E+02

===============================================================


 INSTANT    0.475000000E+01   TIME STEP NUMBER             475
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.196172677E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221322100E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43331E+02 0.54367E+01
   Friction velocity        uet   :  0.36189E-01 0.23366E+02
   Friction velocity        uk    :  0.45719E-01 0.23366E+02
   Dimensionless distance   yplus :  0.20735E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11002
   Nb of faces within the viscous sub-layer     :      12791
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10962E+02      44   0.76492E-01   0.18795E+02 0.25287E+02 
c  Velocity[X]                                      0.33302E+01 
c  Velocity[Y]                                      0.67720E+01 
c  Velocity[Z]                                      0.86929E+01 
c  Pressure     0.62030E-01     468   0.26237E-01   0.80167E-01 0.10141E+01 
c  k            0.30541E+00      16   0.80201E-04   0.22710E-02 0.16141E+02 
c  epsilon      0.32814E+04      10   0.27873E-03   0.18984E+07 0.66633E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.2747e-05                             2
a  epsilon                 -4.9596                             3
a  Local Time Step      3.7027e-08                        280507


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1122          16.767          1.5114         0.24484
v  Velocity[Y]             -26.736           26.21         0.82315         0.59597
v  Velocity[Z]             -43.191          29.116        -0.75135      -0.0043549
v  ǁVelocityǁ             0.006158          47.205          5.0658          5.1439
v  Pressure                 -51811      1.6047e+05           98927           84731
v  k                    1.7791e-06          8.1187        0.056535         0.04761
v  epsilon               0.0056986      1.1654e+06            1623          37.765
v  TurbVisc             3.1747e-12         0.32658       0.0017094        0.026332
v  CourantNb             0.0011584           27007          33.812          5.8741
v  FourierNb              0.022846      2.3655e+05          21.867         0.30827
v  total_pressure       4.4819e+05      6.6047e+05      5.9893e+05      5.8473e+05
v  Local Time Step           0.001        0.046045       0.0010038       0.0010296


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61576      2.4003e+05          55.678          6.1824


 TIME FOR THE TIME STEP              475:        0.74031E+02

===============================================================


 INSTANT    0.476000000E+01   TIME STEP NUMBER             476
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.474209491E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221239897E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53141E+02 0.54476E+01
   Friction velocity        uet   :  0.35547E-01 0.19924E+02
   Friction velocity        uk    :  0.44199E-01 0.19924E+02
   Dimensionless distance   yplus :  0.25423E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11007
   Nb of faces within the viscous sub-layer     :      12797
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10957E+02      45   0.76073E-01   0.19086E+02 0.25508E+02 
c  Velocity[X]                                      0.34392E+01 
c  Velocity[Y]                                      0.69519E+01 
c  Velocity[Z]                                      0.86949E+01 
c  Pressure     0.63117E-01     618   0.26861E-01   0.81493E-01 0.10900E+01 
c  k            0.30549E+00      17   0.10233E-03   0.26531E-02 0.17475E+02 
c  epsilon      0.32854E+04      12   0.32724E-03   0.14212E+07 0.57595E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.0328e-05                             2
a  epsilon                 -1.3101                             2
a  Local Time Step      3.6219e-08                        280504


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1526          15.898          1.5102         0.24469
v  Velocity[Y]             -27.305          28.377         0.82225          0.5964
v  Velocity[Z]             -42.265          29.743        -0.75682      -0.0036803
v  ǁVelocityǁ             0.010191          46.106          5.0691          5.1431
v  Pressure                 -51338       1.605e+05           98944           84723
v  k                    1.8237e-06          7.6913        0.056559        0.047628
v  epsilon               0.0058488      1.1735e+06          1624.2            37.8
v  TurbVisc             3.2443e-12         0.32658       0.0017114        0.026335
v  CourantNb              0.021635           27610          33.854          5.8745
v  FourierNb              0.022843      2.3655e+05          21.867         0.30814
v  total_pressure       4.4866e+05       6.605e+05      5.9894e+05      5.8472e+05
v  Local Time Step           0.001        0.044609       0.0010038       0.0010286


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68668      2.3823e+05          55.721          6.1827


 TIME FOR THE TIME STEP              476:        0.84206E+02

===============================================================


 INSTANT    0.477000000E+01   TIME STEP NUMBER             477
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.263543327E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221131317E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56226E+02 0.54383E+01
   Friction velocity        uet   :  0.32952E-01 0.14755E+02
   Friction velocity        uk    :  0.46187E-01 0.14755E+02
   Dimensionless distance   yplus :  0.84684E-03 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11001
   Nb of faces within the viscous sub-layer     :      12810
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10955E+02      42   0.72977E-01   0.19095E+02 0.25523E+02 
c  Velocity[X]                                      0.33949E+01 
c  Velocity[Y]                                      0.69506E+01 
c  Velocity[Z]                                      0.87496E+01 
c  Pressure     0.62195E-01    1076   0.26675E-01   0.80239E-01 0.60670E+01 
c  k            0.30571E+00      18   0.75424E-04   0.25036E-02 0.16884E+02 
c  epsilon      0.32897E+04      12   0.22748E-03   0.11696E+07 0.52145E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.2526e-05                             2
a  epsilon                 -1.3163                             2
a  Local Time Step      3.8422e-08                        280515


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6814           16.04          1.5093         0.24463
v  Velocity[Y]             -26.462          26.185         0.82614          0.5971
v  Velocity[Z]             -38.301          28.363        -0.76331      -0.0044164
v  ǁVelocityǁ            0.0055132          42.045          5.0743          5.1439
v  Pressure                 -50765      1.6133e+05           99718           85343
v  k                    1.8558e-06          7.6848        0.056624        0.047642
v  epsilon               0.0043369      1.1613e+06          1626.3          37.826
v  TurbVisc             3.3572e-12         0.32658       0.0017126        0.026338
v  CourantNb            0.00098657           26027          33.881          5.8742
v  FourierNb              0.022843      2.3655e+05          21.865         0.30806
v  total_pressure       4.4923e+05      6.6133e+05      5.9972e+05      5.8534e+05
v  Local Time Step           0.001        0.031788       0.0010036       0.0010271


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6153      2.3988e+05          55.746          6.1823


 TIME FOR THE TIME STEP              477:        0.95029E+02

===============================================================


 INSTANT    0.478000000E+01   TIME STEP NUMBER             478
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.179820980E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221285797E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44400E+02 0.54508E+01
   Friction velocity        uet   :  0.38141E-01 0.14346E+02
   Friction velocity        uk    :  0.39231E-01 0.14346E+02
   Dimensionless distance   yplus :  0.18306E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10990
   Nb of faces within the viscous sub-layer     :      12813
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10961E+02      47   0.74625E-01   0.18652E+02 0.25195E+02 
c  Velocity[X]                                      0.33661E+01 
c  Velocity[Y]                                      0.65978E+01 
c  Velocity[Z]                                      0.86883E+01 
c  Pressure     0.62994E-01     414   0.27077E-01   0.81144E-01 0.12122E+01 
c  k            0.30572E+00      21   0.88261E-04   0.24930E-02 0.16944E+02 
c  epsilon      0.32884E+04      12   0.25562E-03   0.19278E+07 0.67008E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00032734                             3
a  epsilon                 -7.5487                             3
a  Local Time Step      3.8979e-08                        280534


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1969           14.33          1.5105         0.24462
v  Velocity[Y]             -26.973          29.207         0.82981         0.59743
v  Velocity[Z]              -35.76          28.713        -0.76857      -0.0047956
v  ǁVelocityǁ             0.011084          39.033           5.077          5.1448
v  Pressure                 -50915       1.614e+05           99734           85320
v  k                    1.7451e-06          7.5402        0.056682        0.047649
v  epsilon                0.005816      1.1736e+06          1629.4          37.855
v  TurbVisc             3.3454e-12         0.32658       0.0017137        0.026341
v  CourantNb                     0           25655          33.915          5.8767
v  FourierNb              0.022849      2.3655e+05          21.865         0.30824
v  total_pressure       4.4908e+05       6.614e+05      5.9973e+05      5.8532e+05
v  Local Time Step           0.001        0.031502       0.0010037       0.0010275


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58215       2.366e+05          55.781          6.1849


 TIME FOR THE TIME STEP              478:        0.79384E+02

===============================================================


 INSTANT    0.479000000E+01   TIME STEP NUMBER             479
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.174321327E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221217129E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40649E+02 0.54471E+01
   Friction velocity        uet   :  0.35992E-01 0.14387E+02
   Friction velocity        uk    :  0.37153E-01 0.14387E+02
   Dimensionless distance   yplus :  0.12617E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10987
   Nb of faces within the viscous sub-layer     :      12817
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10960E+02      50   0.74453E-01   0.19168E+02 0.25562E+02 
c  Velocity[X]                                      0.34344E+01 
c  Velocity[Y]                                      0.70064E+01 
c  Velocity[Z]                                      0.87273E+01 
c  Pressure     0.65123E-01     461   0.28082E-01   0.83825E-01 0.12801E+01 
c  k            0.30586E+00      16   0.82281E-04   0.26395E-02 0.17337E+02 
c  epsilon      0.33068E+04      12   0.37693E-03   0.53448E+07 0.11070E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.4796e-05                             2
a  epsilon                 -1.4913                             2
a  Local Time Step      3.9443e-08                        280516


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0916          14.932          1.5115         0.24498
v  Velocity[Y]             -24.852          26.113         0.83538         0.59768
v  Velocity[Z]             -36.328          28.213        -0.77456       -0.004786
v  ǁVelocityǁ            0.0063813          39.327            5.08          5.1452
v  Pressure                 -51109      1.6142e+05           99756           85290
v  k                    2.0019e-06          7.5935        0.056895        0.047647
v  epsilon               0.0055919      1.1649e+06          1648.3          37.875
v  TurbVisc             3.2332e-12         0.32658       0.0017147        0.026343
v  CourantNb               0.01217           25353          33.951          5.8764
v  FourierNb              0.022862      2.3655e+05          21.865          0.3083
v  total_pressure       4.4889e+05      6.6142e+05      5.9976e+05      5.8529e+05
v  Local Time Step           0.001        0.034111       0.0010038       0.0010282


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73072      2.3853e+05          55.816          6.1847


 TIME FOR THE TIME STEP              479:        0.73809E+02

===============================================================


 INSTANT    0.480000000E+01   TIME STEP NUMBER             480
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.316887608E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221191690E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40605E+02 0.57278E+01
   Friction velocity        uet   :  0.28225E-01 0.15032E+02
   Friction velocity        uk    :  0.37740E-01 0.15032E+02
   Dimensionless distance   yplus :  0.15829E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10978
   Nb of faces within the viscous sub-layer     :      12807
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10964E+02      45   0.75236E-01   0.19637E+02 0.25856E+02 
c  Velocity[X]                                      0.34438E+01 
c  Velocity[Y]                                      0.72457E+01 
c  Velocity[Z]                                      0.89472E+01 
c  Pressure     0.65818E-01     396   0.28331E-01   0.84845E-01 0.11776E+01 
c  k            0.30606E+00      18   0.11162E-03   0.31778E-02 0.18816E+02 
c  epsilon      0.33091E+04      12   0.33809E-03   0.34584E+07 0.89269E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.4306e-05                             3
a  epsilon                  -2.906                             3
a  Local Time Step      3.9538e-08                        280535


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1792          14.717          1.5095         0.24531
v  Velocity[Y]             -25.636           28.85         0.83988          0.5974
v  Velocity[Z]             -38.422          29.855         -0.7781      -0.0044448
v  ǁVelocityǁ            0.0047916          41.789          5.0789          5.1456
v  Pressure                 -51306      1.6144e+05           99785           85264
v  k                    1.7442e-06          7.6477        0.056904        0.047653
v  epsilon               0.0057285      1.1846e+06            1646          37.904
v  TurbVisc              3.607e-12         0.32658       0.0017166        0.026344
v  CourantNb              0.039845           25292          34.007          5.8772
v  FourierNb              0.022882      2.3655e+05          21.866         0.30836
v  total_pressure       4.4869e+05      6.6144e+05      5.9979e+05      5.8526e+05
v  Local Time Step           0.001        0.035115       0.0010038       0.0010284


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63335      2.3876e+05          55.873          6.1856


 TIME FOR THE TIME STEP              480:        0.73600E+02

===============================================================


 INSTANT    0.481000000E+01   TIME STEP NUMBER             481
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.154782033E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221129489E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42197E+02 0.58754E+01
   Friction velocity        uet   :  0.35051E-01 0.17431E+02
   Friction velocity        uk    :  0.44853E-01 0.17431E+02
   Dimensionless distance   yplus :  0.22242E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10970
   Nb of faces within the viscous sub-layer     :      12782
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10961E+02      52   0.75510E-01   0.19703E+02 0.25919E+02 
c  Velocity[X]                                      0.34851E+01 
c  Velocity[Y]                                      0.72288E+01 
c  Velocity[Z]                                      0.89892E+01 
c  Pressure     0.66530E-01     453   0.28913E-01   0.85687E-01 0.10292E+01 
c  k            0.30615E+00      21   0.70641E-04   0.23515E-02 0.16300E+02 
c  epsilon      0.33145E+04      10   0.26566E-03   0.26390E+07 0.77826E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.6386e-05                             2
a  epsilon                 -2.4405                             4
a  Local Time Step      3.9678e-08                        280548


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1768          14.802            1.51         0.24575
v  Velocity[Y]             -26.296          26.116         0.84348         0.59685
v  Velocity[Z]             -34.818          28.036        -0.78156      -0.0035868
v  ǁVelocityǁ              0.00566          37.997          5.0791           5.146
v  Pressure                 -51617      1.6148e+05           99821           85253
v  k                    1.7923e-06          7.6548        0.057046        0.047664
v  epsilon               0.0059219      1.1696e+06          1649.9          37.947
v  TurbVisc             3.1688e-12         0.32658         0.00172        0.026345
v  CourantNb                     0           25203          34.011          5.8773
v  FourierNb              0.022907      2.3655e+05          21.867         0.30831
v  total_pressure       4.4838e+05      6.6148e+05      5.9982e+05      5.8525e+05
v  Local Time Step           0.001        0.038627       0.0010038       0.0010284


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66695      2.3807e+05          55.878          6.1856


 TIME FOR THE TIME STEP              481:        0.67292E+02

===============================================================


 INSTANT    0.482000000E+01   TIME STEP NUMBER             482
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.157091833E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221049166E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37732E+02 0.59440E+01
   Friction velocity        uet   :  0.37632E-01 0.15141E+02
   Friction velocity        uk    :  0.44272E-01 0.15141E+02
   Dimensionless distance   yplus :  0.19320E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10979
   Nb of faces within the viscous sub-layer     :      12772
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10961E+02      45   0.75055E-01   0.19701E+02 0.25897E+02 
c  Velocity[X]                                      0.35128E+01 
c  Velocity[Y]                                      0.73716E+01 
c  Velocity[Z]                                      0.88161E+01 
c  Pressure     0.68231E-01     967   0.29562E-01   0.87825E-01 0.77665E+01 
c  k            0.30624E+00      25   0.74414E-04   0.23110E-02 0.16186E+02 
c  epsilon      0.33243E+04      11   0.84309E-03   0.81045E+07 0.13541E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -5.946e-05                             2
a  epsilon                 -3.2114                             3
a  Local Time Step      3.9465e-08                        280579


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1445          14.321          1.5093         0.24624
v  Velocity[Y]             -29.017          28.497         0.84672         0.59636
v  Velocity[Z]              -35.66          31.445        -0.78179      -0.0045192
v  ǁVelocityǁ            0.0049822          38.917          5.0793          5.1482
v  Pressure                 -50843      1.6253e+05      1.0087e+05           86057
v  k                     1.741e-06          7.6208        0.057272        0.047684
v  epsilon               0.0059153      1.1757e+06          1664.8          38.039
v  TurbVisc             3.3203e-12         0.32658       0.0017247        0.026347
v  CourantNb              0.040803           25339          34.032          5.8775
v  FourierNb              0.022936      2.3655e+05          21.867         0.30837
v  total_pressure       4.4916e+05      6.6253e+05      6.0087e+05      5.8606e+05
v  Local Time Step           0.001        0.037314       0.0010038       0.0010285


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60925      2.3817e+05          55.899          6.1859


 TIME FOR THE TIME STEP              482:        0.94495E+02

===============================================================


 INSTANT    0.483000000E+01   TIME STEP NUMBER             483
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.734484114E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221281731E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43743E+02 0.60489E+01
   Friction velocity        uet   :  0.35604E-01 0.16928E+02
   Friction velocity        uk    :  0.50037E-01 0.16928E+02
   Dimensionless distance   yplus :  0.21600E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10977
   Nb of faces within the viscous sub-layer     :      12774
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10971E+02      47   0.77046E-01   0.19837E+02 0.25995E+02 
c  Velocity[X]                                      0.35225E+01 
c  Velocity[Y]                                      0.73368E+01 
c  Velocity[Z]                                      0.89774E+01 
c  Pressure     0.68934E-01     392   0.29883E-01   0.88678E-01 0.10505E+01 
c  k            0.30634E+00      20   0.10747E-03   0.31720E-02 0.18867E+02 
c  epsilon      0.33362E+04      12   0.50576E-03   0.47548E+07 0.10398E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00057178                             2
a  epsilon                 -3.8327                             6
a  Local Time Step      3.9944e-08                        280569


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.199          15.728          1.5109         0.24647
v  Velocity[Y]             -27.097          29.469         0.84807         0.59608
v  Velocity[Z]             -37.397          28.714        -0.78059      -0.0048244
v  ǁVelocityǁ            0.0083175          41.291           5.078          5.1494
v  Pressure                 -51070      1.6248e+05      1.0088e+05           86030
v  k                    1.7888e-06          7.4696        0.057317        0.047704
v  epsilon               0.0058978      1.1864e+06          1658.3          38.105
v  TurbVisc             3.1109e-12         0.32658       0.0017302        0.026348
v  CourantNb              0.034603           25035          34.046          5.8802
v  FourierNb              0.022966      2.3655e+05          21.868         0.30822
v  total_pressure       4.4893e+05      6.6248e+05      6.0088e+05      5.8603e+05
v  Local Time Step           0.001        0.039401       0.0010037       0.0010269


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4757      2.3741e+05          55.914          6.1885


 TIME FOR THE TIME STEP              483:        0.76277E+02

===============================================================


 INSTANT    0.484000000E+01   TIME STEP NUMBER             484
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.141840273E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221218675E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39241E+02 0.62863E+01
   Friction velocity        uet   :  0.37669E-01 0.20330E+02
   Friction velocity        uk    :  0.42094E-01 0.20330E+02
   Dimensionless distance   yplus :  0.25941E-02 0.16027E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10977
   Nb of faces within the viscous sub-layer     :      12744
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10973E+02      46   0.76738E-01   0.19766E+02 0.25940E+02 
c  Velocity[X]                                      0.35053E+01 
c  Velocity[Y]                                      0.72938E+01 
c  Velocity[Z]                                      0.89666E+01 
c  Pressure     0.68512E-01     376   0.29852E-01   0.88116E-01 0.10631E+01 
c  k            0.30656E+00      19   0.21240E-03   0.46878E-02 0.21414E+02 
c  epsilon      0.33343E+04      17   0.36205E-03   0.39421E+07 0.94470E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021697                             2
a  epsilon                 -5.0356                             3
a  Local Time Step      3.8547e-08                        280547


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1887          14.459          1.5119         0.24671
v  Velocity[Y]             -27.117          27.611         0.84879         0.59597
v  Velocity[Z]             -37.094          29.132        -0.77655      -0.0046597
v  ǁVelocityǁ            0.0092052          40.469          5.0737            5.15
v  Pressure                 -51268       1.625e+05      1.0089e+05           85996
v  k                    1.7926e-06          7.5245        0.057559         0.04772
v  epsilon               0.0058677      1.1878e+06          1671.8           38.16
v  TurbVisc             3.3527e-12         0.32658       0.0017356         0.02635
v  CourantNb              0.013783           25943          34.039          5.8798
v  FourierNb              0.022995      2.3655e+05          21.868          0.3082
v  total_pressure       4.4873e+05       6.625e+05      6.0089e+05        5.86e+05
v  Local Time Step           0.001        0.026405       0.0010036       0.0010266


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.80608      2.3687e+05          55.908           6.188


 TIME FOR THE TIME STEP              484:        0.77288E+02

===============================================================


 INSTANT    0.485000000E+01   TIME STEP NUMBER             485
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.221624163E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221196081E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43834E+02 0.67752E+01
   Friction velocity        uet   :  0.28347E-01 0.14500E+02
   Friction velocity        uk    :  0.30561E-01 0.14500E+02
   Dimensionless distance   yplus :  0.17425E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10990
   Nb of faces within the viscous sub-layer     :      12731
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10974E+02      56   0.76319E-01   0.20207E+02 0.26227E+02 
c  Velocity[X]                                      0.36663E+01 
c  Velocity[Y]                                      0.71997E+01 
c  Velocity[Z]                                      0.93405E+01 
c  Pressure     0.68387E-01     491   0.29749E-01   0.87935E-01 0.98030E+00 
c  k            0.30757E+00      20   0.24193E-03   0.46123E-02 0.20543E+02 
c  epsilon      0.33367E+04      11   0.26055E-03   0.36246E+07 0.90457E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010765                             3
a  epsilon                 -6.8044                             8
a  Local Time Step       3.792e-08                        280535


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2228           16.38           1.513         0.24663
v  Velocity[Y]             -25.999          29.975         0.84794         0.59587
v  Velocity[Z]             -39.057          31.005        -0.77293      -0.0042601
v  ǁVelocityǁ            0.0063657          43.145           5.072          5.1501
v  Pressure                 -51406      1.6255e+05      1.0089e+05           85986
v  k                    1.7862e-06          7.6861        0.057559        0.047743
v  epsilon               0.0046014      1.1624e+06          1667.6          38.199
v  TurbVisc             3.2445e-12         0.32658       0.0017407        0.026351
v  CourantNb              0.028605           26371          34.004           5.879
v  FourierNb              0.023019      2.3655e+05          21.871         0.30838
v  total_pressure       4.4859e+05      6.6255e+05      6.0089e+05      5.8599e+05
v  Local Time Step           0.001        0.029045       0.0010037       0.0010269


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70188      2.3679e+05          55.875          6.1874


 TIME FOR THE TIME STEP              485:        0.85232E+02

===============================================================


 INSTANT    0.486000000E+01   TIME STEP NUMBER             486
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.212349956E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221184343E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40916E+02 0.80009E+01
   Friction velocity        uet   :  0.37899E-01 0.17214E+02
   Friction velocity        uk    :  0.47353E-01 0.17214E+02
   Dimensionless distance   yplus :  0.13550E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11025
   Nb of faces within the viscous sub-layer     :      12720
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10974E+02      46   0.76793E-01   0.19634E+02 0.25854E+02 
c  Velocity[X]                                      0.35875E+01 
c  Velocity[Y]                                      0.72073E+01 
c  Velocity[Z]                                      0.88391E+01 
c  Pressure     0.67610E-01     582   0.29402E-01   0.86915E-01 0.98272E+00 
c  k            0.30935E+00      19   0.53008E-03   0.10140E-01 0.27112E+02 
c  epsilon      0.33401E+04      11   0.26814E-03   0.16216E+07 0.59820E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.5692e-05                             3
a  epsilon                 -5.0672                             6
a  Local Time Step      3.7698e-08                        280507


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.171          14.161          1.5122         0.24652
v  Velocity[Y]             -26.909          27.091         0.84928         0.59592
v  Velocity[Z]             -35.151          28.996        -0.76718      -0.0041277
v  ǁVelocityǁ            0.0061841           38.44          5.0708          5.1505
v  Pressure                 -51464      1.6255e+05       1.009e+05           86005
v  k                    1.9666e-06          7.6506        0.057692        0.047782
v  epsilon               0.0057895      1.1802e+06          1670.8          38.281
v  TurbVisc             3.2485e-12         0.32658       0.0017463        0.026353
v  CourantNb              0.011526           26527          33.982          5.8788
v  FourierNb              0.023035      2.3655e+05          21.874         0.30835
v  total_pressure       4.4854e+05      6.6255e+05       6.009e+05        5.86e+05
v  Local Time Step           0.001         0.03195       0.0010037       0.0010267


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85519      2.3697e+05          55.856          6.1872


 TIME FOR THE TIME STEP              486:        0.84199E+02

===============================================================


 INSTANT    0.487000000E+01   TIME STEP NUMBER             487
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.715064957E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221176434E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42666E+02 0.80127E+01
   Friction velocity        uet   :  0.36229E-01 0.17062E+02
   Friction velocity        uk    :  0.43787E-01 0.17062E+02
   Dimensionless distance   yplus :  0.13438E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11029
   Nb of faces within the viscous sub-layer     :      12694
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10976E+02      48   0.77846E-01   0.19884E+02 0.26028E+02 
c  Velocity[X]                                      0.36670E+01 
c  Velocity[Y]                                      0.72310E+01 
c  Velocity[Z]                                      0.89856E+01 
c  Pressure     0.68963E-01     479   0.29615E-01   0.88662E-01 0.11197E+01 
c  k            0.31171E+00      16   0.38610E-03   0.62354E-02 0.22791E+02 
c  epsilon      0.33354E+04      10   0.22009E-03   0.85142E+06 0.43024E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.2164e-05                             2
a  epsilon                 -4.5192                             7
a  Local Time Step      3.7864e-08                        280556


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2034          15.442           1.513         0.24632
v  Velocity[Y]             -24.321          25.494          0.8538          0.5962
v  Velocity[Z]             -36.612          27.725        -0.76411      -0.0040902
v  ǁVelocityǁ            0.0086449           40.01          5.0723          5.1507
v  Pressure                 -51545      1.6252e+05       1.009e+05           86039
v  k                    1.8235e-06          7.6632        0.057664        0.047824
v  epsilon               0.0057297      1.2006e+06          1666.8          38.329
v  TurbVisc             3.5845e-12         0.32658       0.0017508        0.026355
v  CourantNb                     0           26410          33.968          5.8782
v  FourierNb              0.023041      2.3655e+05          21.877          0.3085
v  total_pressure       4.4846e+05      6.6252e+05       6.009e+05      5.8604e+05
v  Local Time Step           0.001        0.031186       0.0010038       0.0010276


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89337      2.3798e+05          55.845          6.1867


 TIME FOR THE TIME STEP              487:        0.75640E+02

===============================================================


 INSTANT    0.488000000E+01   TIME STEP NUMBER             488
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.144171148E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221204682E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41107E+02 0.81358E+01
   Friction velocity        uet   :  0.38376E-01 0.16704E+02
   Friction velocity        uk    :  0.43068E-01 0.16704E+02
   Dimensionless distance   yplus :  0.19668E-02 0.16082E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11056
   Nb of faces within the viscous sub-layer     :      12680
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10976E+02      44   0.77742E-01   0.20355E+02 0.26329E+02 
c  Velocity[X]                                      0.38256E+01 
c  Velocity[Y]                                      0.75929E+01 
c  Velocity[Z]                                      0.89367E+01 
c  Pressure     0.68550E-01     517   0.29134E-01   0.87977E-01 0.12897E+01 
c  k            0.31319E+00      18   0.12624E-03   0.44600E-02 0.21878E+02 
c  epsilon      0.33336E+04      11   0.39798E-03   0.22753E+07 0.71557E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.6866e-05                             3
a  epsilon                 -3.8335                             6
a  Local Time Step       3.921e-08                        280578


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2649          15.365          1.5139         0.24622
v  Velocity[Y]             -25.382          26.884         0.86007         0.59652
v  Velocity[Z]             -38.108          27.688        -0.76209      -0.0043735
v  ǁVelocityǁ            0.0044489          41.485          5.0751          5.1508
v  Pressure                 -51646      1.6244e+05      1.0087e+05           86079
v  k                    1.8142e-06          7.6852        0.057721        0.047869
v  epsilon               0.0056351      1.1719e+06          1667.2          38.416
v  TurbVisc             3.2968e-12         0.32658       0.0017523        0.026358
v  CourantNb              0.059455           25504          33.945          5.8782
v  FourierNb              0.023039      2.3655e+05          21.878         0.30837
v  total_pressure       4.4835e+05      6.6244e+05      6.0087e+05      5.8608e+05
v  Local Time Step           0.001        0.034305       0.0010038       0.0010283


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.79757      2.3741e+05          55.823          6.1865


 TIME FOR THE TIME STEP              488:        0.94987E+02

===============================================================


 INSTANT    0.489000000E+01   TIME STEP NUMBER             489
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.554283583E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221266461E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41674E+02 0.73482E+01
   Friction velocity        uet   :  0.36533E-01 0.15944E+02
   Friction velocity        uk    :  0.47162E-01 0.15944E+02
   Dimensionless distance   yplus :  0.11329E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11070
   Nb of faces within the viscous sub-layer     :      12687
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10979E+02      50   0.77893E-01   0.20845E+02 0.26640E+02 
c  Velocity[X]                                      0.36999E+01 
c  Velocity[Y]                                      0.80067E+01 
c  Velocity[Z]                                      0.91383E+01 
c  Pressure     0.71058E-01     593   0.30075E-01   0.91395E-01 0.13385E+01 
c  k            0.31110E+00      21   0.60073E-03   0.26780E-01 0.48593E+02 
c  epsilon      0.33241E+04      15   0.24294E-03   0.15580E+07 0.58622E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014194                             3
a  epsilon                 -5.7807                             6
a  Local Time Step      3.8943e-08                        280561


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1953          14.756          1.5136           0.246
v  Velocity[Y]             -26.594          25.721         0.86771         0.59659
v  Velocity[Z]             -36.177          27.998        -0.76386      -0.0054393
v  ǁVelocityǁ            0.0079513          39.255          5.0786           5.151
v  Pressure                 -51713       1.624e+05      1.0083e+05           86096
v  k                    1.8043e-06           7.769         0.05758        0.047888
v  epsilon                0.005518      1.1904e+06          1658.7          38.364
v  TurbVisc             3.3127e-12         0.32658       0.0017507        0.026361
v  CourantNb               0.03747           25679          33.965          5.8781
v  FourierNb               0.02303      2.3655e+05          21.876         0.30844
v  total_pressure       4.4829e+05       6.624e+05      6.0083e+05       5.861e+05
v  Local Time Step           0.001        0.031585       0.0010037       0.0010277


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.80824      2.3706e+05          55.841          6.1866


 TIME FOR THE TIME STEP              489:        0.81271E+02

===============================================================


 INSTANT    0.490000000E+01   TIME STEP NUMBER             490
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.441408455E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221354567E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40121E+02 0.59411E+01
   Friction velocity        uet   :  0.22057E-01 0.16467E+02
   Friction velocity        uk    :  0.21919E-01 0.16467E+02
   Dimensionless distance   yplus :  0.17827E-02 0.16027E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11071
   Nb of faces within the viscous sub-layer     :      12690
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10985E+02      42   0.77600E-01   0.19975E+02 0.26063E+02 
c  Velocity[X]                                      0.36719E+01 
c  Velocity[Y]                                      0.72469E+01 
c  Velocity[Z]                                      0.90561E+01 
c  Pressure     0.70972E-01     653   0.30459E-01   0.91380E-01 0.14328E+01 
c  k            0.30777E+00      19   0.61427E-03   0.28768E-01 0.57144E+02 
c  epsilon      0.33120E+04      14   0.30962E-03   0.29457E+07 0.82099E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019235                             5
a  epsilon                 -4.2244                             5
a  Local Time Step      3.7322e-08                        280562


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2376          14.696          1.5132         0.24585
v  Velocity[Y]             -30.144          24.084          0.8734         0.59658
v  Velocity[Z]             -36.056          28.472        -0.76621      -0.0067629
v  ǁVelocityǁ             0.010553          39.268          5.0826          5.1523
v  Pressure                 -51693      1.6225e+05      1.0071e+05           86053
v  k                     1.751e-06          7.6236        0.057544        0.047893
v  epsilon               0.0053997        1.18e+06          1656.9          38.307
v  TurbVisc              3.259e-12         0.32658       0.0017462        0.026364
v  CourantNb              0.058509           26794          33.975          5.8783
v  FourierNb              0.023016      2.3655e+05          21.874         0.30845
v  total_pressure       4.4831e+05      6.6225e+05      6.0071e+05      5.8605e+05
v  Local Time Step           0.001        0.030427       0.0010036       0.0010269


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61634      2.3721e+05          55.849          6.1868


 TIME FOR THE TIME STEP              490:        0.92209E+02

===============================================================


 INSTANT    0.491000000E+01   TIME STEP NUMBER             491
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.748430007E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221507368E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44207E+02 0.54534E+01
   Friction velocity        uet   :  0.36875E-01 0.14979E+02
   Friction velocity        uk    :  0.40050E-01 0.14979E+02
   Dimensionless distance   yplus :  0.18621E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11076
   Nb of faces within the viscous sub-layer     :      12684
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10988E+02      42   0.78141E-01   0.19840E+02 0.25987E+02 
c  Velocity[X]                                      0.36070E+01 
c  Velocity[Y]                                      0.73522E+01 
c  Velocity[Z]                                      0.88806E+01 
c  Pressure     0.69943E-01    1450   0.29955E-01   0.90136E-01 0.65953E+01 
c  k            0.30646E+00      20   0.27236E-03   0.83902E-02 0.30552E+02 
c  epsilon      0.32982E+04      11   0.21320E-03   0.19875E+07 0.67697E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010977                             3
a  epsilon                 -4.0332                             6
a  Local Time Step       3.707e-08                        280539


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2957            15.1           1.512         0.24543
v  Velocity[Y]             -26.297           24.14         0.87872         0.59671
v  Velocity[Z]             -36.255          28.336        -0.76818      -0.0067206
v  ǁVelocityǁ            0.0047343          39.285          5.0867          5.1512
v  Pressure                 -52386      1.6136e+05           99845           85383
v  k                    1.7869e-06          7.6712        0.057461        0.047895
v  epsilon               0.0053056      1.1644e+06          1650.6          38.256
v  TurbVisc             3.1878e-12         0.32658       0.0017406        0.026367
v  CourantNb              0.011877           26976          33.994          5.8796
v  FourierNb                 0.023      2.3655e+05          21.871         0.30827
v  total_pressure       4.4761e+05      6.6136e+05      5.9984e+05      5.8538e+05
v  Local Time Step           0.001        0.033216       0.0010037       0.0010271


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39761       2.366e+05          55.865          6.1879


 TIME FOR THE TIME STEP              491:        0.12493E+03

===============================================================


 INSTANT    0.492000000E+01   TIME STEP NUMBER             492
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.165264165E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221386837E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40345E+02 0.54848E+01
   Friction velocity        uet   :  0.38677E-01 0.14847E+02
   Friction velocity        uk    :  0.44579E-01 0.14847E+02
   Dimensionless distance   yplus :  0.10799E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11096
   Nb of faces within the viscous sub-layer     :      12695
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10985E+02      44   0.76584E-01   0.19560E+02 0.25808E+02 
c  Velocity[X]                                      0.35606E+01 
c  Velocity[Y]                                      0.69702E+01 
c  Velocity[Z]                                      0.90295E+01 
c  Pressure     0.69009E-01     897   0.29402E-01   0.88954E-01 0.53887E+01 
c  k            0.30606E+00      18   0.14932E-03   0.37700E-02 0.20239E+02 
c  epsilon      0.33043E+04      12   0.19823E-03   0.16905E+07 0.62351E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010536                             3
a  epsilon                 -4.2321                             6
a  Local Time Step      3.7664e-08                        280518


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2998          15.475          1.5088         0.24514
v  Velocity[Y]             -24.961          25.226         0.88235          0.5966
v  Velocity[Z]             -38.381          29.446        -0.76694      -0.0056765
v  ǁVelocityǁ            0.0056076          41.734           5.088          5.1498
v  Pressure                 -52828      1.6057e+05           99123           84852
v  k                    2.2454e-06          7.7806        0.057338        0.047895
v  epsilon               0.0052149       1.197e+06          1645.5          38.236
v  TurbVisc             3.2575e-12         0.32658       0.0017359         0.02637
v  CourantNb               0.02748           26550          34.026          5.8786
v  FourierNb              0.022983      2.3655e+05          21.869         0.30834
v  total_pressure       4.4717e+05      6.6057e+05      5.9912e+05      5.8485e+05
v  Local Time Step           0.001         0.03175       0.0010037       0.0010278


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48999      2.3835e+05          55.895          6.1869


 TIME FOR THE TIME STEP              492:        0.97046E+02

===============================================================


 INSTANT    0.493000000E+01   TIME STEP NUMBER             493
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.530282191E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221379839E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42101E+02 0.54331E+01
   Friction velocity        uet   :  0.36891E-01 0.15810E+02
   Friction velocity        uk    :  0.48928E-01 0.15810E+02
   Dimensionless distance   yplus :  0.12728E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11081
   Nb of faces within the viscous sub-layer     :      12699
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10978E+02      44   0.75293E-01   0.18926E+02 0.25399E+02 
c  Velocity[X]                                      0.34380E+01 
c  Velocity[Y]                                      0.64962E+01 
c  Velocity[Z]                                      0.89915E+01 
c  Pressure     0.68351E-01     415   0.28979E-01   0.88248E-01 0.99314E+00 
c  k            0.30609E+00      21   0.93199E-04   0.25599E-02 0.16622E+02 
c  epsilon      0.32967E+04      10   0.19335E-03   0.77818E+06 0.42405E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010408                             2
a  epsilon                 -4.0778                             6
a  Local Time Step       3.845e-08                        280523


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1402           14.63          1.5058         0.24493
v  Velocity[Y]              -26.31            25.1         0.88562         0.59643
v  Velocity[Z]             -34.529          30.564        -0.76704      -0.0048342
v  ǁVelocityǁ             0.007437          37.509          5.0891          5.1487
v  Pressure                 -52703      1.6055e+05           99100           84884
v  k                     1.817e-06          7.6883        0.057247          0.0479
v  epsilon               0.0051371      1.1519e+06          1641.7          38.201
v  TurbVisc             4.0295e-12         0.32658       0.0017326        0.026372
v  CourantNb             0.0074988           26008          34.018          5.8788
v  FourierNb              0.022969      2.3655e+05          21.868         0.30833
v  total_pressure        4.473e+05      6.6055e+05       5.991e+05      5.8488e+05
v  Local Time Step           0.001        0.034924       0.0010037       0.0010279


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62215      2.3872e+05          55.886          6.1872


 TIME FOR THE TIME STEP              493:        0.71874E+02

===============================================================


 INSTANT    0.494000000E+01   TIME STEP NUMBER             494
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.281684099E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221325512E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37133E+02 0.54424E+01
   Friction velocity        uet   :  0.29190E-01 0.14509E+02
   Friction velocity        uk    :  0.29006E-01 0.14509E+02
   Dimensionless distance   yplus :  0.18514E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11085
   Nb of faces within the viscous sub-layer     :      12718
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10977E+02      47   0.75834E-01   0.17750E+02 0.24593E+02 
c  Velocity[X]                                      0.32391E+01 
c  Velocity[Y]                                      0.63394E+01 
c  Velocity[Z]                                      0.81712E+01 
c  Pressure     0.66007E-01     369   0.28143E-01   0.85370E-01 0.80808E+00 
c  k            0.30641E+00      18   0.10929E-03   0.35489E-02 0.19346E+02 
c  epsilon      0.32949E+04      10   0.17494E-03   0.98474E+06 0.47741E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.0492e-05                             2
a  epsilon                 -3.3419                             3
a  Local Time Step      3.8157e-08                        280546


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3012          15.006          1.5054         0.24499
v  Velocity[Y]              -30.01          25.988          0.8856          0.5964
v  Velocity[Z]             -36.901          28.272        -0.76665        -0.00443
v  ǁVelocityǁ            0.0094596          40.126          5.0908           5.148
v  Pressure                 -52614      1.6053e+05           99095           84894
v  k                    1.7333e-06          7.6894        0.057158        0.047917
v  epsilon               0.0050589      1.1716e+06          1636.9          38.204
v  TurbVisc             3.2021e-12         0.32658       0.0017312        0.026375
v  CourantNb              0.025801           26208          34.015          5.8789
v  FourierNb              0.022959      2.3655e+05          21.868         0.30838
v  total_pressure       4.4739e+05      6.6053e+05       5.991e+05      5.8489e+05
v  Local Time Step           0.001        0.034683       0.0010036       0.0010269


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53867      2.3832e+05          55.883          6.1872


 TIME FOR THE TIME STEP              494:        0.66285E+02

===============================================================


 INSTANT    0.495000000E+01   TIME STEP NUMBER             495
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.733597760E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221278411E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43598E+02 0.54672E+01
   Friction velocity        uet   :  0.22603E-01 0.16626E+02
   Friction velocity        uk    :  0.49013E-01 0.16626E+02
   Dimensionless distance   yplus :  0.20838E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11086
   Nb of faces within the viscous sub-layer     :      12732
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10974E+02      46   0.75222E-01   0.17573E+02 0.24475E+02 
c  Velocity[X]                                      0.32992E+01 
c  Velocity[Y]                                      0.62696E+01 
c  Velocity[Z]                                      0.80040E+01 
c  Pressure     0.65601E-01     347   0.27626E-01   0.84943E-01 0.66449E+00 
c  k            0.30667E+00      22   0.10857E-03   0.35066E-02 0.19442E+02 
c  epsilon      0.33060E+04      10   0.19828E-03   0.12636E+07 0.53947E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.7116e-05                             2
a  epsilon                 -1.8898                             4
a  Local Time Step      3.9677e-08                        280543


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.204          14.841          1.5047          0.2451
v  Velocity[Y]             -26.366          25.471         0.88395         0.59628
v  Velocity[Z]             -35.939          28.024        -0.76752      -0.0042321
v  ǁVelocityǁ            0.0088305          38.959          5.0906          5.1475
v  Pressure                 -52505      1.6051e+05           99094           84893
v  k                    1.8141e-06          7.7899        0.057113        0.047929
v  epsilon                0.004984       1.181e+06          1638.1          38.196
v  TurbVisc              3.173e-12         0.32658       0.0017316        0.026379
v  CourantNb             0.0072978           25204          34.035          5.8791
v  FourierNb              0.022952      2.3655e+05          21.868         0.30831
v  total_pressure       4.4749e+05      6.6051e+05      5.9909e+05      5.8489e+05
v  Local Time Step           0.001        0.038151       0.0010036       0.0010274


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59117      2.3818e+05          55.902          6.1874


 TIME FOR THE TIME STEP              495:        0.67879E+02

===============================================================


 INSTANT    0.496000000E+01   TIME STEP NUMBER             496
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.318748025E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221269056E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39570E+02 0.54657E+01
   Friction velocity        uet   :  0.19806E-01 0.15142E+02
   Friction velocity        uk    :  0.19683E-01 0.15142E+02
   Dimensionless distance   yplus :  0.19321E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11070
   Nb of faces within the viscous sub-layer     :      12718
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10971E+02      42   0.74075E-01   0.17159E+02 0.24184E+02 
c  Velocity[X]                                      0.32572E+01 
c  Velocity[Y]                                      0.57314E+01 
c  Velocity[Z]                                      0.81701E+01 
c  Pressure     0.64342E-01     344   0.26886E-01   0.83390E-01 0.62956E+00 
c  k            0.30693E+00      16   0.17022E-03   0.53531E-02 0.24127E+02 
c  epsilon      0.33034E+04      11   0.19835E-03   0.99614E+06 0.48006E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.6888e-05                             2
a  epsilon                 -4.8552                             3
a  Local Time Step      3.9532e-08                        280540


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2445          15.396          1.5051         0.24536
v  Velocity[Y]             -24.839          26.703         0.88123          0.5962
v  Velocity[Z]             -37.567          27.746        -0.76739      -0.0041304
v  ǁVelocityǁ            0.0026985          41.023          5.0914          5.1473
v  Pressure                 -52354      1.6051e+05           99097           84891
v  k                    1.7743e-06          7.7292         0.05708         0.04795
v  epsilon               0.0049019       1.179e+06          1633.2          38.202
v  TurbVisc             3.3175e-12         0.32658       0.0017327        0.026384
v  CourantNb              0.023508           25296          34.024          5.8791
v  FourierNb              0.022951      2.3655e+05          21.867         0.30824
v  total_pressure       4.4765e+05      6.6051e+05       5.991e+05      5.8489e+05
v  Local Time Step           0.001        0.029649       0.0010036       0.0010268


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53275      2.3853e+05          55.891          6.1874


 TIME FOR THE TIME STEP              496:        0.67768E+02

===============================================================


 INSTANT    0.497000000E+01   TIME STEP NUMBER             497
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.232557336E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221244825E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44066E+02 0.54371E+01
   Friction velocity        uet   :  0.38607E-02 0.19961E+02
   Friction velocity        uk    :  0.36747E-01 0.19961E+02
   Dimensionless distance   yplus :  0.12945E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11090
   Nb of faces within the viscous sub-layer     :      12720
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10971E+02      43   0.73597E-01   0.16874E+02 0.23977E+02 
c  Velocity[X]                                      0.31279E+01 
c  Velocity[Y]                                      0.54609E+01 
c  Velocity[Z]                                      0.82852E+01 
c  Pressure     0.62538E-01     270   0.25856E-01   0.81105E-01 0.56442E+00 
c  k            0.30754E+00      17   0.13440E-03   0.57279E-02 0.24825E+02 
c  epsilon      0.33034E+04      11   0.21324E-03   0.11784E+07 0.52116E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0756e-05                             2
a  epsilon                -0.83823                             2
a  Local Time Step      3.9327e-08                        280524


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3359          14.792          1.5055         0.24555
v  Velocity[Y]             -26.135          24.801         0.87742         0.59618
v  Velocity[Z]             -35.505          28.208        -0.76819      -0.0041412
v  ǁVelocityǁ            0.0050756          38.522          5.0901          5.1474
v  Pressure                 -52202      1.6053e+05           99099           84893
v  k                    1.8018e-06          7.7366        0.057154        0.047988
v  epsilon               0.0048357      1.1563e+06          1636.9          38.242
v  TurbVisc             3.2074e-12         0.32658       0.0017361        0.026389
v  CourantNb             0.0043555           25428          34.052          5.8792
v  FourierNb              0.022954      2.3655e+05          21.868         0.30832
v  total_pressure        4.478e+05      6.6053e+05       5.991e+05      5.8489e+05
v  Local Time Step           0.001        0.030775       0.0010036       0.0010271


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.628      2.3755e+05           55.92          6.1875


 TIME FOR THE TIME STEP              497:        0.63784E+02

===============================================================


 INSTANT    0.498000000E+01   TIME STEP NUMBER             498
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.146812241E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221241219E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38805E+02 0.61257E+01
   Friction velocity        uet   :  0.39087E-01 0.13588E+02
   Friction velocity        uk    :  0.42674E-01 0.13588E+02
   Dimensionless distance   yplus :  0.64043E-03 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11061
   Nb of faces within the viscous sub-layer     :      12713
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10969E+02      43   0.74800E-01   0.16434E+02 0.23661E+02 
c  Velocity[X]                                      0.31532E+01 
c  Velocity[Y]                                      0.54851E+01 
c  Velocity[Z]                                      0.77959E+01 
c  Pressure     0.62337E-01     297   0.25802E-01   0.80827E-01 0.54508E+00 
c  k            0.30808E+00      15   0.17648E-03   0.63252E-02 0.26151E+02 
c  epsilon      0.33078E+04      10   0.21172E-03   0.12458E+07 0.53577E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -4.31e-05                             2
a  epsilon                 -1.0348                             3
a  Local Time Step       3.991e-08                        280504


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3452          15.127          1.5056         0.24579
v  Velocity[Y]             -30.281          25.678         0.87345         0.59616
v  Velocity[Z]             -37.155            28.4        -0.76669       -0.004304
v  ǁVelocityǁ            0.0068928          40.419          5.0894           5.147
v  Pressure                 -52086       1.605e+05           99105           84898
v  k                     2.095e-06          7.8419        0.057146        0.048025
v  epsilon               0.0047872      1.1936e+06          1635.5          38.266
v  TurbVisc              3.303e-12         0.32658       0.0017406        0.026395
v  CourantNb              0.015009           25056          34.026          5.8791
v  FourierNb               0.02296      2.3655e+05          21.869         0.30828
v  total_pressure       4.4791e+05       6.605e+05      5.9911e+05       5.849e+05
v  Local Time Step           0.001        0.030868       0.0010036       0.0010264


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70229      2.3898e+05          55.895          6.1874


 TIME FOR THE TIME STEP              498:        0.76319E+02

===============================================================


 INSTANT    0.499000000E+01   TIME STEP NUMBER             499
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.461883089E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245135E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44091E+02 0.61048E+01
   Friction velocity        uet   :  0.28126E-01 0.19150E+02
   Friction velocity        uk    :  0.45261E-01 0.19150E+02
   Dimensionless distance   yplus :  0.18218E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11036
   Nb of faces within the viscous sub-layer     :      12712
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10967E+02      41   0.75724E-01   0.16566E+02 0.23766E+02 
c  Velocity[X]                                      0.30567E+01 
c  Velocity[Y]                                      0.56317E+01 
c  Velocity[Z]                                      0.78777E+01 
c  Pressure     0.62475E-01     234   0.25641E-01   0.80901E-01 0.54325E+00 
c  k            0.30874E+00      17   0.14637E-03   0.46200E-02 0.22183E+02 
c  epsilon      0.33158E+04      10   0.20156E-03   0.86275E+06 0.44467E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.0425e-06                             1
a  epsilon                -0.48547                             2
a  Local Time Step      4.0831e-08                        280512


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.251           14.67          1.5066         0.24575
v  Velocity[Y]             -27.518          25.451           0.869         0.59594
v  Velocity[Z]              -36.34          28.034        -0.76571      -0.0044737
v  ǁVelocityǁ             0.010874          39.395          5.0872          5.1465
v  Pressure                 -51995      1.6054e+05           99109           84893
v  k                    1.6871e-06          7.7439        0.057209         0.04806
v  epsilon               0.0047539      1.1749e+06          1639.7          38.294
v  TurbVisc             3.7853e-12         0.32658        0.001746        0.026402
v  CourantNb              0.013982           24491          34.023          5.8786
v  FourierNb              0.022971      2.3655e+05          21.869         0.30851
v  total_pressure       4.4801e+05      6.6054e+05      5.9911e+05      5.8489e+05
v  Local Time Step           0.001        0.031839       0.0010037       0.0010272


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59693      2.3854e+05          55.892          6.1871


 TIME FOR THE TIME STEP              499:        0.60817E+02

===============================================================


 INSTANT    0.500000000E+01   TIME STEP NUMBER             500
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.644316982E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221237925E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40213E+02 0.60786E+01
   Friction velocity        uet   :  0.38718E-01 0.19050E+02
   Friction velocity        uk    :  0.38738E-01 0.19050E+02
   Dimensionless distance   yplus :  0.17907E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11057
   Nb of faces within the viscous sub-layer     :      12714
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10965E+02      47   0.76131E-01   0.16684E+02 0.23843E+02 
c  Velocity[X]                                      0.32025E+01 
c  Velocity[Y]                                      0.56220E+01 
c  Velocity[Z]                                      0.78592E+01 
c  Pressure     0.61602E-01     383   0.25340E-01   0.79828E-01 0.58255E+00 
c  k            0.30873E+00      17   0.14597E-03   0.43516E-02 0.21840E+02 
c  epsilon      0.33097E+04      10   0.24459E-03   0.15274E+07 0.59286E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012486                             2
a  epsilon                 -4.0321                             3
a  Local Time Step      4.0782e-08                        280513


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2815          15.182          1.5073         0.24582
v  Velocity[Y]             -26.195          26.111         0.86343         0.59572
v  Velocity[Z]             -36.425           28.38        -0.76274      -0.0044963
v  ǁVelocityǁ            0.0067722          40.102          5.0836          5.1458
v  Pressure                 -51964      1.6057e+05           99114           84901
v  k                    1.8264e-06          7.7828         0.05722         0.04809
v  epsilon               0.0047396      1.1778e+06          1637.8          38.295
v  TurbVisc             3.0196e-12         0.32658        0.001752        0.026409
v  CourantNb              0.022315           24521          33.975          5.8779
v  FourierNb              0.022985      2.3655e+05          21.871          0.3087
v  total_pressure       4.4804e+05      6.6057e+05      5.9911e+05       5.849e+05
v  Local Time Step           0.001        0.034114       0.0010038        0.001028


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43496      2.3993e+05          55.846          6.1866


 TIME FOR THE TIME STEP              500:        0.83602E+02

===============================================================


 INSTANT    0.501000000E+01   TIME STEP NUMBER             501
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.334153378E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221242387E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42044E+02 0.56766E+01
   Friction velocity        uet   :  0.37118E-01 0.18383E+02
   Friction velocity        uk    :  0.45726E-01 0.18383E+02
   Dimensionless distance   yplus :  0.15084E-02 0.16028E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11033
   Nb of faces within the viscous sub-layer     :      12718
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.11062E+02      41   0.73664E-01   0.60855E+03 0.12788E+03 
c  Velocity[X]                                      0.26192E+02 
c  Velocity[Y]                                      0.53018E+02 
c  Velocity[Z]                                      0.52934E+03 
c  Pressure     0.70067E-01    1829   0.30819E+00   0.90721E-01 0.62038E+03 
c  k            0.41709E+00      23   0.16514E-02   0.39439E+00 0.18340E+03 
c  epsilon      0.33175E+04      15   0.34080E-03   0.22576E+07 0.72481E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.8595e-05                             2
a  epsilon                 -2.6644                             1
a  Local Time Step      4.0865e-08                        280506


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1354          17.104           1.647         0.28983
v  Velocity[Y]             -25.827           28.95          1.0278         0.69181
v  Velocity[Z]             -38.447          32.601        -0.79416      0.00060785
v  ǁVelocityǁ               0.0107          42.069          5.3729          5.8152
v  Pressure                 190.97      4.6037e+05      2.5791e+05      2.4109e+05
v  k                    1.6898e-06          7.7924        0.057874        0.051955
v  epsilon               0.0047474      1.0939e+06          1656.1          39.301
v  TurbVisc             3.4122e-12         0.32658       0.0017571        0.026416
v  CourantNb              0.015893           24471          33.952          5.8766
v  FourierNb              0.023004      2.3655e+05          21.871         0.30867
v  total_pressure       5.0019e+05      9.6037e+05      7.5791e+05      7.4109e+05
v  Local Time Step           0.001        0.027102       0.0010037       0.0010268


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45303      2.3946e+05          55.824          6.1852


 TIME FOR THE TIME STEP              501:        0.15678E+03

===============================================================


 INSTANT    0.502000000E+01   TIME STEP NUMBER             502
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.201333713E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270935952E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46293E+02 0.59291E+01
   Friction velocity        uet   :  0.22869E-01 0.28211E+02
   Friction velocity        uk    :  0.21973E-01 0.28211E+02
   Dimensionless distance   yplus :  0.29291E-02 0.17469E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11913
   Nb of faces within the viscous sub-layer     :      12389
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14359E+02      80   0.70899E-01   0.25503E+03 0.78121E+02 
c  Velocity[X]                                      0.25971E+02 
c  Velocity[Y]                                      0.45342E+02 
c  Velocity[Z]                                      0.18371E+03 
c  Pressure     0.26347E+00    1572   0.10762E+00   0.33012E+00 0.24799E+03 
c  k            0.45835E+00      23   0.57318E-03   0.19360E+00 0.11630E+03 
c  epsilon      0.40103E+04      19   0.25020E-02   0.94026E+08 0.38778E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013538                             7
a  epsilon                 -13.236                             5
a  Local Time Step      4.2273e-08                        280729


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4061          16.902          1.7251         0.30787
v  Velocity[Y]              -26.53          29.001          1.1135         0.74323
v  Velocity[Z]             -40.445          28.247        -0.76699        0.014434
v  ǁVelocityǁ             0.010078          45.395          5.5146          6.1847
v  Pressure                 -100.1      3.5675e+05       2.115e+05      1.9007e+05
v  k                    1.7392e-06          8.8536        0.062523        0.055905
v  epsilon               0.0034826      2.9298e+06          2039.6          43.615
v  TurbVisc             3.3782e-12         0.39846       0.0018235        0.028027
v  CourantNb                     0           20446          36.494          6.7135
v  FourierNb              0.023033      2.3656e+05          21.871         0.30941
v  total_pressure        4.999e+05      8.5675e+05       7.115e+05      6.9007e+05
v  Local Time Step           0.001        0.029812       0.0010017       0.0010116


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46868      2.4231e+05          58.365          7.0229


 TIME FOR THE TIME STEP              502:        0.15918E+03

===============================================================


 INSTANT    0.503000000E+01   TIME STEP NUMBER             503
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.109227250E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270835511E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56141E+02 0.57644E+01
   Friction velocity        uet   :  0.24215E-01 0.35394E+02
   Friction velocity        uk    :  0.24134E-01 0.35394E+02
   Dimensionless distance   yplus :  0.43998E-02 0.18961E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12294
   Nb of faces within the viscous sub-layer     :      12189
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14557E+02      74   0.70734E-01   0.64387E+02 0.38904E+02 
c  Velocity[X]                                      0.14222E+02 
c  Velocity[Y]                                      0.26128E+02 
c  Velocity[Z]                                      0.24037E+02 
c  Pressure     0.15028E+00    1521   0.17685E+00   0.18116E+00 0.48070E+03 
c  k            0.47773E+00      21   0.41145E-03   0.10103E+00 0.79351E+02 
c  epsilon      0.41175E+04      16   0.14599E-02   0.49893E+08 0.30258E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0012571                             2
a  epsilon                 -5.4415                             6
a  Local Time Step      3.0912e-08                        280778


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6123          16.622          1.7571         0.30732
v  Velocity[Y]             -27.415          30.885          1.1113         0.74728
v  Velocity[Z]             -38.733          30.393        -0.78016       0.0054363
v  ǁVelocityǁ             0.012783           43.17          5.5947          6.2356
v  Pressure                 -40430       2.248e+05       1.461e+05       1.222e+05
v  k                    1.7965e-06          7.9661        0.061671         0.05873
v  epsilon               0.0015117      1.3864e+06          1909.9          44.074
v  TurbVisc              3.286e-12         0.41564       0.0018503        0.029013
v  CourantNb              0.011353           32350          36.663          6.7683
v  FourierNb              0.023071      2.3655e+05          21.871         0.31061
v  total_pressure       4.5957e+05       7.248e+05       6.461e+05       6.222e+05
v  Local Time Step           0.001        0.031356       0.0010017       0.0010116


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49302      2.5234e+05          58.533           7.079


 TIME FOR THE TIME STEP              503:        0.14970E+03

===============================================================


 INSTANT    0.504000000E+01   TIME STEP NUMBER             504
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.368529171E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271127562E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46978E+02 0.56695E+01
   Friction velocity        uet   :  0.21171E-01 0.39526E+02
   Friction velocity        uk    :  0.21729E-01 0.39526E+02
   Dimensionless distance   yplus :  0.43773E-02 0.19592E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12420
   Nb of faces within the viscous sub-layer     :      12038
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13859E+02      77   0.74420E-01   0.63300E+02 0.38886E+02 
c  Velocity[X]                                      0.11369E+02 
c  Velocity[Y]                                      0.23236E+02 
c  Velocity[Z]                                      0.28696E+02 
c  Pressure     0.18823E+00    1478   0.12071E+00   0.21920E+00 0.20801E+03 
c  k            0.49137E+00      19   0.25822E-03   0.62401E-01 0.60030E+02 
c  epsilon      0.41360E+04      18   0.91076E-03   0.33197E+08 0.23570E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00033881                             2
a  epsilon                 -2.3229                             8
a  Local Time Step      3.0672e-08                        280761


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6466          17.323          1.7674         0.30374
v  Velocity[Y]             -28.328          31.102          1.0578         0.73552
v  Velocity[Z]             -46.177          29.304        -0.80285      -0.0046152
v  ǁVelocityǁ             0.015059          50.556          5.6394          6.1751
v  Pressure                 -69965      2.0027e+05      1.2097e+05           97403
v  k                    2.6003e-07          8.3884        0.063378        0.060941
v  epsilon               0.0042761      1.6409e+06          2038.3          45.144
v  TurbVisc             3.2276e-12         0.41785       0.0018644        0.029776
v  CourantNb              0.020197           32603          36.894           6.816
v  FourierNb              0.023119      2.3655e+05          21.872         0.31128
v  total_pressure       4.3003e+05      7.0027e+05      6.2097e+05       5.974e+05
v  Local Time Step           0.001        0.017395       0.0010017       0.0010112


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54375      2.3849e+05          58.766          7.1273


 TIME FOR THE TIME STEP              504:        0.15044E+03

===============================================================


 INSTANT    0.505000000E+01   TIME STEP NUMBER             505
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.258717915E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270907435E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69337E+02 0.58260E+01
   Friction velocity        uet   :  0.33737E-01 0.37879E+02
   Friction velocity        uk    :  0.32728E-01 0.37879E+02
   Dimensionless distance   yplus :  0.37443E-02 0.19808E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12398
   Nb of faces within the viscous sub-layer     :      11921
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13413E+02      75   0.77955E-01   0.52988E+02 0.35743E+02 
c  Velocity[X]                                      0.94189E+01 
c  Velocity[Y]                                      0.20033E+02 
c  Velocity[Z]                                      0.23537E+02 
c  Pressure     0.15131E+00    1536   0.69927E-01   0.17154E+00 0.48630E+02 
c  k            0.50103E+00      19   0.15588E-03   0.41079E-01 0.47412E+02 
c  epsilon      0.42158E+04      13   0.87281E-03   0.16251E+08 0.16288E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.8502e-05                             2
a  epsilon                 -6.4118                             8
a  Local Time Step      3.2835e-08                        280785


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6372          19.022          1.7708         0.30264
v  Velocity[Y]             -30.187          31.512          1.0059         0.72799
v  Velocity[Z]             -49.583          32.249         -0.8141      -0.0077177
v  ǁVelocityǁ              0.01325          54.422           5.682          6.1379
v  Pressure                 -68032      2.0649e+05      1.2601e+05      1.0329e+05
v  k                    1.5101e-06          8.7805        0.063837        0.062694
v  epsilon               0.0042037      1.6511e+06          2062.3          45.712
v  TurbVisc             3.2629e-12          0.4182       0.0018832        0.030486
v  CourantNb             0.0068164           30455           37.32          6.8445
v  FourierNb              0.023183      2.3655e+05          21.874         0.31219
v  total_pressure       4.3197e+05      7.0649e+05      6.2601e+05      6.0329e+05
v  Local Time Step           0.001        0.018043       0.0010017       0.0010114


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46239      2.4192e+05          59.194          7.1566


 TIME FOR THE TIME STEP              505:        0.14822E+03

===============================================================


 INSTANT    0.506000000E+01   TIME STEP NUMBER             506
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.989578667E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270952768E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75411E+02 0.58858E+01
   Friction velocity        uet   :  0.29980E-01 0.35136E+02
   Friction velocity        uk    :  0.35725E-01 0.35136E+02
   Dimensionless distance   yplus :  0.41901E-02 0.19875E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12434
   Nb of faces within the viscous sub-layer     :      11861
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13363E+02      80   0.81287E-01   0.46177E+02 0.33254E+02 
c  Velocity[X]                                      0.83534E+01 
c  Velocity[Y]                                      0.18187E+02 
c  Velocity[Z]                                      0.19637E+02 
c  Pressure     0.12379E+00    1433   0.60183E-01   0.13678E+00 0.84147E+02 
c  k            0.50799E+00      18   0.14320E-03   0.31509E-01 0.40699E+02 
c  epsilon      0.43867E+04      20   0.15669E-02   0.86110E+08 0.34681E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00035226                             3
a  epsilon                 -2.0731                             6
a  Local Time Step      3.4414e-08                        280842


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1712          17.739          1.7785         0.30362
v  Velocity[Y]             -31.988          34.167         0.97513         0.72769
v  Velocity[Z]             -46.794          30.718        -0.81703      -0.0063192
v  ǁVelocityǁ             0.014017          50.271          5.7328          6.1437
v  Pressure                 -59396       2.188e+05      1.3693e+05       1.145e+05
v  k                    1.8255e-06          9.7826        0.064958        0.064163
v  epsilon                0.004233      3.9188e+06          2199.4          46.338
v  TurbVisc              3.196e-12         0.41829       0.0018991        0.031166
v  CourantNb              0.011915           29058          37.739          6.8718
v  FourierNb              0.023256      2.3655e+05          21.873         0.31287
v  total_pressure        4.406e+05       7.188e+05      6.3693e+05       6.145e+05
v  Local Time Step           0.001        0.016356       0.0010017       0.0010116


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49815      2.3993e+05          59.612          7.1847


 TIME FOR THE TIME STEP              506:        0.13668E+03

===============================================================


 INSTANT    0.507000000E+01   TIME STEP NUMBER             507
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.691419529E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271018024E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74930E+02 0.59681E+01
   Friction velocity        uet   :  0.15107E-01 0.32736E+02
   Friction velocity        uk    :  0.35434E-01 0.32736E+02
   Dimensionless distance   yplus :  0.41575E-02 0.20016E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12501
   Nb of faces within the viscous sub-layer     :      11771
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13466E+02      79   0.82615E-01   0.43790E+02 0.32318E+02 
c  Velocity[X]                                      0.79800E+01 
c  Velocity[Y]                                      0.17027E+02 
c  Velocity[Z]                                      0.18783E+02 
c  Pressure     0.11362E+00    1332   0.52542E-01   0.12277E+00 0.40735E+02 
c  k            0.51317E+00      21   0.11434E-03   0.23413E-01 0.34543E+02 
c  epsilon      0.44812E+04      14   0.14153E-02   0.42225E+08 0.24910E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014108                             2
a  epsilon                 -5.6628                             5
a  Local Time Step      3.4309e-08                        280849


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9634           18.41          1.7847         0.30375
v  Velocity[Y]             -31.467          34.243         0.96296          0.7301
v  Velocity[Z]             -46.515          32.377        -0.82076      -0.0038622
v  ǁVelocityǁ             0.013708          51.695          5.7829          6.1657
v  Pressure                 -55833      2.2563e+05      1.4255e+05      1.1998e+05
v  k                    1.8874e-06          10.331        0.065716        0.065433
v  epsilon               0.0043221      2.0149e+06          2218.9          46.898
v  TurbVisc             3.3173e-12         0.41833       0.0019124        0.031803
v  CourantNb               0.01492           29147          38.168          6.9023
v  FourierNb               0.02333      2.3655e+05          21.871         0.31377
v  total_pressure       4.4417e+05      7.2563e+05      6.4255e+05      6.1998e+05
v  Local Time Step           0.001        0.017991       0.0010018       0.0010121


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46044      2.3889e+05           60.04          7.2161


 TIME FOR THE TIME STEP              507:        0.13925E+03

===============================================================


 INSTANT    0.508000000E+01   TIME STEP NUMBER             508
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.145005607E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270933044E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70068E+02 0.59639E+01
   Friction velocity        uet   :  0.34895E-01 0.32123E+02
   Friction velocity        uk    :  0.44869E-01 0.32123E+02
   Dimensionless distance   yplus :  0.38915E-02 0.20151E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12566
   Nb of faces within the viscous sub-layer     :      11707
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13549E+02      81   0.84056E-01   0.39728E+02 0.30669E+02 
c  Velocity[X]                                      0.73293E+01 
c  Velocity[Y]                                      0.15930E+02 
c  Velocity[Z]                                      0.16469E+02 
c  Pressure     0.10753E+00    1305   0.46582E-01   0.11396E+00 0.10068E+02 
c  k            0.51691E+00      19   0.10174E-03   0.18562E-01 0.30381E+02 
c  epsilon      0.46619E+04      16   0.14820E-02   0.50236E+08 0.25802E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.0689e-05                             3
a  epsilon                 -2.3113                             5
a  Local Time Step      3.4398e-08                        280889


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9756           17.05          1.7915         0.30324
v  Velocity[Y]             -34.156          36.225         0.96068         0.73208
v  Velocity[Z]             -45.519          30.876        -0.83426      -0.0034342
v  ǁVelocityǁ              0.01526          49.672          5.8308          6.1856
v  Pressure                 -56675      2.2791e+05      1.4385e+05      1.2108e+05
v  k                    1.9355e-06          10.885        0.066885        0.066534
v  epsilon               0.0044978      2.8102e+06          2329.2          47.512
v  TurbVisc             3.4742e-12         0.41835       0.0019329        0.032391
v  CourantNb             0.0038245           29071          38.581          6.9289
v  FourierNb               0.02335      2.3656e+05          21.874         0.31451
v  total_pressure       4.4333e+05      7.2791e+05      6.4385e+05      6.2108e+05
v  Local Time Step           0.001         0.01979       0.0010018       0.0010124


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.2813      2.4123e+05          60.456          7.2434


 TIME FOR THE TIME STEP              508:        0.15545E+03

===============================================================


 INSTANT    0.509000000E+01   TIME STEP NUMBER             509
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.301111320E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270983900E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59463E+02 0.62562E+01
   Friction velocity        uet   :  0.13249E-01 0.30245E+02
   Friction velocity        uk    :  0.40938E-01 0.30245E+02
   Dimensionless distance   yplus :  0.38593E-02 0.20213E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12605
   Nb of faces within the viscous sub-layer     :      11693
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13575E+02      69   0.84349E-01   0.40729E+02 0.30967E+02 
c  Velocity[X]                                      0.75610E+01 
c  Velocity[Y]                                      0.16935E+02 
c  Velocity[Z]                                      0.16233E+02 
c  Pressure     0.10684E+00     976   0.43904E-01   0.11146E+00 0.48753E+01 
c  k            0.51989E+00      19   0.81258E-04   0.12232E-01 0.24430E+02 
c  epsilon      0.47560E+04      17   0.91428E-03   0.26292E+08 0.18624E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010776                             3
a  epsilon                 -12.343                             7
a  Local Time Step      3.6101e-08                        280886


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.9789          18.751          1.7976         0.30246
v  Velocity[Y]             -32.281           37.43         0.96137         0.73281
v  Velocity[Z]             -49.913          34.591        -0.85389      -0.0047579
v  ǁVelocityǁ             0.015444          54.855          5.8747          6.1989
v  Pressure                 -59449      2.2831e+05      1.4346e+05      1.2063e+05
v  k                    2.0235e-06          10.823        0.067694        0.067479
v  epsilon                0.004751      2.3079e+06          2375.4              48
v  TurbVisc             3.5157e-12         0.41836       0.0019541        0.032928
v  CourantNb             0.0025804           27700          38.955          6.9539
v  FourierNb              0.023352      2.3656e+05          21.877         0.31512
v  total_pressure       4.4055e+05      7.2831e+05      6.4346e+05      6.2063e+05
v  Local Time Step           0.001        0.021769       0.0010019       0.0010127


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56492      2.4212e+05          60.832           7.269


 TIME FOR THE TIME STEP              509:        0.11082E+03

===============================================================


 INSTANT    0.510000000E+01   TIME STEP NUMBER             510
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.162152579E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271064383E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.78797E+02 0.61681E+01
   Friction velocity        uet   :  0.35488E-01 0.26682E+02
   Friction velocity        uk    :  0.34617E-01 0.26682E+02
   Dimensionless distance   yplus :  0.34024E-02 0.20239E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12640
   Nb of faces within the viscous sub-layer     :      11675
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13575E+02      77   0.82618E-01   0.45082E+02 0.32418E+02 
c  Velocity[X]                                      0.73560E+01 
c  Velocity[Y]                                      0.18193E+02 
c  Velocity[Z]                                      0.19534E+02 
c  Pressure     0.10509E+00     946   0.41749E-01   0.10811E+00 0.34287E+01 
c  k            0.52214E+00      18   0.70847E-04   0.10359E-01 0.22316E+02 
c  epsilon      0.48268E+04      13   0.56755E-03   0.17775E+08 0.15145E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.7972e-05                             2
a  epsilon                 -1.0085                             3
a  Local Time Step      3.7721e-08                        280934


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0215           18.53          1.8017         0.30158
v  Velocity[Y]             -31.984          39.894         0.96434         0.73292
v  Velocity[Z]             -51.257          31.701        -0.87599      -0.0058388
v  ǁVelocityǁ             0.009134           54.55          5.9143          6.2081
v  Pressure                 -61889      2.2846e+05      1.4306e+05      1.2036e+05
v  k                    2.0807e-06          10.788        0.068337        0.068314
v  epsilon               0.0050365      2.3782e+06            2397          48.495
v  TurbVisc             3.5273e-12         0.41837       0.0019737        0.033416
v  CourantNb             0.0015458           26510          39.256          6.9762
v  FourierNb              0.023353      2.3656e+05          21.878         0.31579
v  total_pressure       4.3811e+05      7.2846e+05      6.4306e+05      6.2036e+05
v  Local Time Step           0.001        0.022588       0.0010019       0.0010128


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57538      2.3971e+05          61.133           7.292


 TIME FOR THE TIME STEP              510:        0.10596E+03

===============================================================


 INSTANT    0.511000000E+01   TIME STEP NUMBER             511
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.848417717E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271107401E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.86353E+02 0.62157E+01
   Friction velocity        uet   :  0.40277E-01 0.26200E+02
   Friction velocity        uk    :  0.39255E-01 0.26200E+02
   Dimensionless distance   yplus :  0.32219E-02 0.20249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12682
   Nb of faces within the viscous sub-layer     :      11611
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13578E+02      75   0.86798E-01   0.47200E+02 0.33234E+02 
c  Velocity[X]                                      0.74997E+01 
c  Velocity[Y]                                      0.18861E+02 
c  Velocity[Z]                                      0.20840E+02 
c  Pressure     0.10545E+00     721   0.41228E-01   0.10716E+00 0.28849E+01 
c  k            0.52399E+00      19   0.98897E-04   0.97734E-02 0.21531E+02 
c  epsilon      0.48989E+04      18   0.48585E-03   0.11213E+08 0.11892E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022825                             2
a  epsilon                 -1.4398                             5
a  Local Time Step      3.7811e-08                        280941


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0049          18.419          1.8053         0.30096
v  Velocity[Y]             -29.738          37.104         0.96651         0.73276
v  Velocity[Z]             -49.202          33.761        -0.89749      -0.0060442
v  ǁVelocityǁ             0.013359          52.735           5.951          6.2166
v  Pressure                 -63464      2.2876e+05      1.4298e+05      1.2043e+05
v  k                    2.2519e-06          10.454        0.069392        0.069054
v  epsilon               0.0044984      2.3462e+06          2458.1          49.012
v  TurbVisc             3.8235e-12         0.41837       0.0019943        0.033863
v  CourantNb              0.013748           26447          39.569          6.9979
v  FourierNb              0.023354      2.3656e+05          21.882         0.31641
v  total_pressure       4.3654e+05      7.2876e+05      6.4298e+05      6.2043e+05
v  Local Time Step           0.001        0.024807       0.0010019       0.0010131


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71521      2.3882e+05          61.451          7.3144


 TIME FOR THE TIME STEP              511:        0.96244E+02

===============================================================


 INSTANT    0.512000000E+01   TIME STEP NUMBER             512
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.960207139E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271029192E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74952E+02 0.62211E+01
   Friction velocity        uet   :  0.43101E-01 0.25959E+02
   Friction velocity        uk    :  0.52906E-01 0.25959E+02
   Dimensionless distance   yplus :  0.18193E-02 0.20253E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12697
   Nb of faces within the viscous sub-layer     :      11558
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13574E+02      70   0.87768E-01   0.45638E+02 0.32643E+02 
c  Velocity[X]                                      0.74201E+01 
c  Velocity[Y]                                      0.19834E+02 
c  Velocity[Z]                                      0.18384E+02 
c  Pressure     0.10786E+00     744   0.41473E-01   0.10848E+00 0.27765E+01 
c  k            0.52554E+00      17   0.77980E-04   0.89027E-02 0.20488E+02 
c  epsilon      0.49627E+04      21   0.42996E-03   0.16619E+08 0.14281E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.3708e-05                             1
a  epsilon                 -3.4124                             6
a  Local Time Step      3.9249e-08                        280976


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1224           17.36          1.8073         0.30069
v  Velocity[Y]              -32.72          36.879         0.96608         0.73313
v  Velocity[Z]             -46.458          33.788        -0.91607      -0.0049254
v  ǁVelocityǁ             0.014085           50.46          5.9817          6.2232
v  Pressure                 -63740      2.2903e+05      1.4298e+05      1.2052e+05
v  k                    1.4327e-06           10.14        0.070088        0.069719
v  epsilon                0.005826      2.4103e+06            2503          49.466
v  TurbVisc             3.8116e-12         0.41838       0.0020123        0.034271
v  CourantNb              0.012765           25479           39.89          7.0177
v  FourierNb              0.023344      2.3656e+05          21.884         0.31696
v  total_pressure       4.3626e+05      7.2903e+05      6.4298e+05      6.2052e+05
v  Local Time Step           0.001        0.027288        0.001002       0.0010134


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54921      2.4141e+05          61.774          7.3346


 TIME FOR THE TIME STEP              512:        0.95400E+02

===============================================================


 INSTANT    0.513000000E+01   TIME STEP NUMBER             513
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.205654538E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270837984E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64979E+02 0.62282E+01
   Friction velocity        uet   :  0.42460E-01 0.26129E+02
   Friction velocity        uk    :  0.45977E-01 0.26129E+02
   Dimensionless distance   yplus :  0.33341E-02 0.20254E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12739
   Nb of faces within the viscous sub-layer     :      11485
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13568E+02      65   0.87168E-01   0.47051E+02 0.33116E+02 
c  Velocity[X]                                      0.79589E+01 
c  Velocity[Y]                                      0.19887E+02 
c  Velocity[Z]                                      0.19204E+02 
c  Pressure     0.11163E+00    1311   0.42548E-01   0.11128E+00 0.77197E+01 
c  k            0.52660E+00      17   0.79090E-04   0.82742E-02 0.19686E+02 
c  epsilon      0.50234E+04      13   0.48768E-03   0.12772E+08 0.12400E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                      -0.00013                             4
a  epsilon                 -3.9844                             8
a  Local Time Step      4.2255e-08                        280956


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1247          19.394          1.8097         0.30113
v  Velocity[Y]              -30.14          33.659         0.96386         0.73373
v  Velocity[Z]             -50.195          32.858        -0.92993      -0.0048567
v  ǁVelocityǁ             0.014478          55.555          6.0078           6.232
v  Pressure                 -63956      2.3035e+05      1.4416e+05      1.2156e+05
v  k                    2.3615e-06          10.144        0.070755        0.070294
v  epsilon               0.0061792      2.3577e+06          2543.1          49.806
v  TurbVisc             3.9581e-12         0.41838       0.0020296        0.034642
v  CourantNb              0.035734           23666          40.174          7.0335
v  FourierNb              0.023273      2.3657e+05          21.886         0.31762
v  total_pressure       4.3604e+05      7.3035e+05      6.4416e+05      6.2156e+05
v  Local Time Step           0.001        0.030017        0.001002       0.0010136


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50555      2.4171e+05           62.06          7.3511


 TIME FOR THE TIME STEP              513:        0.12424E+03

===============================================================


 INSTANT    0.514000000E+01   TIME STEP NUMBER             514
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.371195206E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270949499E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74177E+02 0.61885E+01
   Friction velocity        uet   :  0.41545E-01 0.29832E+02
   Friction velocity        uk    :  0.43975E-01 0.29832E+02
   Dimensionless distance   yplus :  0.37888E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12774
   Nb of faces within the viscous sub-layer     :      11417
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13576E+02      58   0.88176E-01   0.52866E+02 0.34971E+02 
c  Velocity[X]                                      0.87347E+01 
c  Velocity[Y]                                      0.22595E+02 
c  Velocity[Z]                                      0.21536E+02 
c  Pressure     0.11597E+00     616   0.44050E-01   0.11503E+00 0.19891E+01 
c  k            0.52766E+00      17   0.88623E-04   0.82471E-02 0.19590E+02 
c  epsilon      0.50729E+04      19   0.82389E-03   0.20812E+08 0.15607E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.1383e-05                             2
a  epsilon                 -2.5994                             5
a  Local Time Step      4.2272e-08                        280962


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4729          18.418          1.8146          0.3018
v  Velocity[Y]             -34.259          40.977         0.96142          0.7336
v  Velocity[Z]              -51.11          37.523        -0.94054      -0.0038176
v  ǁVelocityǁ             0.012683          54.605          6.0292           6.239
v  Pressure                 -65364      2.3043e+05       1.442e+05      1.2158e+05
v  k                    2.8967e-06          9.8641        0.071704        0.070815
v  epsilon               0.0066014      2.3942e+06          2615.2          50.208
v  TurbVisc             4.0566e-12         0.41838       0.0020471         0.03498
v  CourantNb              0.054085           23196          40.395          7.0511
v  FourierNb              0.023193      2.3657e+05          21.888         0.31792
v  total_pressure       4.3464e+05      7.3043e+05       6.442e+05      6.2158e+05
v  Local Time Step           0.001        0.033018        0.001002        0.001014


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.50155      2.4094e+05          62.282           7.369


 TIME FOR THE TIME STEP              514:        0.86290E+02

===============================================================


 INSTANT    0.515000000E+01   TIME STEP NUMBER             515
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.717662410E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270759109E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.86356E+02 0.61808E+01
   Friction velocity        uet   :  0.40126E-01 0.31845E+02
   Friction velocity        uk    :  0.43333E-01 0.31845E+02
   Dimensionless distance   yplus :  0.40634E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12798
   Nb of faces within the viscous sub-layer     :      11374
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13573E+02      63   0.91080E-01   0.55573E+02 0.35929E+02 
c  Velocity[X]                                      0.95206E+01 
c  Velocity[Y]                                      0.25131E+02 
c  Velocity[Z]                                      0.20921E+02 
c  Pressure     0.12127E+00     857   0.46253E-01   0.11985E+00 0.72817E+01 
c  k            0.52857E+00      20   0.10090E-03   0.80582E-02 0.19322E+02 
c  epsilon      0.51298E+04      15   0.55472E-03   0.11904E+08 0.11738E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011142                             3
a  epsilon                -0.60114                             5
a  Local Time Step      4.2272e-08                        280982


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1768          19.052          1.8175         0.30237
v  Velocity[Y]             -32.648           34.94         0.95856         0.73345
v  Velocity[Z]              -49.47          36.521        -0.94829      -0.0044642
v  ǁVelocityǁ             0.010271          54.896          6.0459           6.247
v  Pressure                 -65751      2.3174e+05      1.4548e+05      1.2259e+05
v  k                    1.4619e-06          10.112        0.072124         0.07128
v  epsilon               0.0069794      2.3361e+06          2628.9          50.509
v  TurbVisc             3.4105e-12         0.41838       0.0020646        0.035285
v  CourantNb              0.016855           23260          40.604          7.0646
v  FourierNb              0.023114      2.3657e+05           21.89         0.31837
v  total_pressure       4.3425e+05      7.3174e+05      6.4548e+05      6.2259e+05
v  Local Time Step           0.001         0.03632        0.001002       0.0010143


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71846      2.4151e+05          62.494          7.3829


 TIME FOR THE TIME STEP              515:        0.10543E+03

===============================================================


 INSTANT    0.516000000E+01   TIME STEP NUMBER             516
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.906205516E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270862732E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72394E+02 0.61981E+01
   Friction velocity        uet   :  0.40979E-01 0.37517E+02
   Friction velocity        uk    :  0.44860E-01 0.37517E+02
   Dimensionless distance   yplus :  0.47871E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12853
   Nb of faces within the viscous sub-layer     :      11343
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13575E+02      64   0.89219E-01   0.54939E+02 0.35646E+02 
c  Velocity[X]                                      0.97083E+01 
c  Velocity[Y]                                      0.26403E+02 
c  Velocity[Z]                                      0.18828E+02 
c  Pressure     0.12509E+00     541   0.48442E-01   0.12360E+00 0.21298E+01 
c  k            0.52917E+00      19   0.10495E-03   0.87303E-02 0.20053E+02 
c  epsilon      0.52079E+04      15   0.55440E-03   0.17022E+08 0.13783E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.1384e-05                             3
a  epsilon                  -43.49                             6
a  Local Time Step      4.1879e-08                        280991


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4728          17.666          1.8248         0.30249
v  Velocity[Y]             -32.235          47.929          0.9559         0.73345
v  Velocity[Z]             -47.722          33.247        -0.95746      -0.0039562
v  ǁVelocityǁ            0.0061175          51.988          6.0585          6.2534
v  Pressure                 -67202      2.3169e+05      1.4551e+05      1.2257e+05
v  k                    3.0928e-06          10.264        0.073036        0.071695
v  epsilon               0.0073548      2.4199e+06          2698.2           50.84
v  TurbVisc             3.6044e-12         0.41838       0.0020849         0.03556
v  CourantNb              0.071916           23878          40.795           7.078
v  FourierNb               0.02304      2.3657e+05           21.89         0.31892
v  total_pressure        4.328e+05      7.3169e+05      6.4551e+05      6.2257e+05
v  Local Time Step           0.001        0.039952        0.001002       0.0010145


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77109      2.4331e+05          62.685          7.3969


 TIME FOR THE TIME STEP              516:        0.84771E+02

===============================================================


 INSTANT    0.517000000E+01   TIME STEP NUMBER             517
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.562124261E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270806865E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75145E+02 0.61743E+01
   Friction velocity        uet   :  0.39679E-01 0.44041E+02
   Friction velocity        uk    :  0.42771E-01 0.44041E+02
   Dimensionless distance   yplus :  0.28344E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12869
   Nb of faces within the viscous sub-layer     :      11294
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13574E+02      58   0.90632E-01   0.55001E+02 0.35682E+02 
c  Velocity[X]                                      0.97402E+01 
c  Velocity[Y]                                      0.25300E+02 
c  Velocity[Z]                                      0.19961E+02 
c  Pressure     0.13004E+00     854   0.50399E-01   0.12801E+00 0.24077E+01 
c  k            0.52989E+00      18   0.11458E-03   0.11511E-01 0.22977E+02 
c  epsilon      0.52823E+04      15   0.12506E-02   0.47940E+08 0.22588E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00092748                             5
a  epsilon                 -3.8448                             5
a  Local Time Step      4.1023e-08                        280983


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6603          19.383          1.8278         0.30251
v  Velocity[Y]             -32.517          37.097         0.95615         0.73316
v  Velocity[Z]             -54.389          30.738         -0.9631      -0.0030578
v  ǁVelocityǁ            0.0065404           59.08          6.0664          6.2581
v  Pressure                 -68172      2.3184e+05      1.4576e+05      1.2274e+05
v  k                    2.1246e-06          10.543        0.073702        0.072065
v  epsilon               0.0047495      4.1707e+06          2781.1          51.084
v  TurbVisc             3.7352e-12         0.41838       0.0021057        0.035808
v  CourantNb               0.02893           24377          40.972          7.0881
v  FourierNb              0.022976      2.3657e+05          21.895         0.31921
v  total_pressure       4.3183e+05      7.3184e+05      6.4576e+05      6.2274e+05
v  Local Time Step           0.001        0.043947        0.001002       0.0010149


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71587      2.4385e+05          62.867          7.4073


 TIME FOR THE TIME STEP              517:        0.87813E+02

===============================================================


 INSTANT    0.518000000E+01   TIME STEP NUMBER             518
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.653289121E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270732503E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76148E+02 0.62101E+01
   Friction velocity        uet   :  0.40029E-01 0.43675E+02
   Friction velocity        uk    :  0.42305E-01 0.43675E+02
   Dimensionless distance   yplus :  0.49625E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12912
   Nb of faces within the viscous sub-layer     :      11265
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13569E+02      62   0.90060E-01   0.55925E+02 0.35885E+02 
c  Velocity[X]                                      0.95563E+01 
c  Velocity[Y]                                      0.24246E+02 
c  Velocity[Z]                                      0.22123E+02 
c  Pressure     0.13484E+00     788   0.52534E-01   0.13243E+00 0.41693E+01 
c  k            0.53055E+00      18   0.12689E-03   0.13145E-01 0.24506E+02 
c  epsilon      0.53142E+04      14   0.87958E-03   0.23570E+08 0.16022E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00088735                             6
a  epsilon                 -24.065                             5
a  Local Time Step      4.0731e-08                        281007


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8435          18.552          1.8321         0.30276
v  Velocity[Y]             -31.835          36.543         0.95907         0.73253
v  Velocity[Z]             -50.747          31.131        -0.96641      -0.0029747
v  ǁVelocityǁ              0.01084          55.034          6.0727           6.263
v  Pressure                 -68463      2.3247e+05      1.4643e+05      1.2328e+05
v  k                    1.8855e-06          10.627        0.074027        0.072399
v  epsilon               0.0079207      2.4008e+06          2756.4           51.25
v  TurbVisc             4.5299e-12         0.41838       0.0021265         0.03603
v  CourantNb              0.029057           24551          41.073          7.0949
v  FourierNb              0.022922      2.3657e+05          21.898         0.31971
v  total_pressure       4.3154e+05      7.3247e+05      6.4643e+05      6.2328e+05
v  Local Time Step           0.001        0.048342        0.001002       0.0010153


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54222      2.4532e+05          62.972          7.4146


 TIME FOR THE TIME STEP              518:        0.99290E+02

===============================================================


 INSTANT    0.519000000E+01   TIME STEP NUMBER             519
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.279205458E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270762860E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85899E+02 0.61582E+01
   Friction velocity        uet   :  0.28504E-01 0.38879E+02
   Friction velocity        uk    :  0.28202E-01 0.38879E+02
   Dimensionless distance   yplus :  0.49609E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12931
   Nb of faces within the viscous sub-layer     :      11220
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13576E+02      58   0.90153E-01   0.55213E+02 0.35724E+02 
c  Velocity[X]                                      0.98081E+01 
c  Velocity[Y]                                      0.24338E+02 
c  Velocity[Z]                                      0.21067E+02 
c  Pressure     0.13744E+00     514   0.53491E-01   0.13455E+00 0.19308E+01 
c  k            0.53091E+00      24   0.10407E-03   0.13584E-01 0.24883E+02 
c  epsilon      0.53566E+04      13   0.49727E-03   0.15287E+08 0.12750E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.3871e-05                             1
a  epsilon               -0.047496                             2
a  Local Time Step      3.8764e-08                        281020


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5467          18.923          1.8358         0.30275
v  Velocity[Y]             -30.413          41.167         0.96557          0.7308
v  Velocity[Z]              -50.79          30.924        -0.96312      -0.0028415
v  ǁVelocityǁ             0.010811          56.165          6.0748          6.2668
v  Pressure                 -69230      2.3243e+05      1.4646e+05      1.2334e+05
v  k                    2.3711e-06          10.505        0.074687        0.072692
v  epsilon               0.0081224      2.3368e+06          2816.1          51.429
v  TurbVisc             3.6611e-12         0.41838       0.0021462         0.03623
v  CourantNb              0.014787           25797          41.106          7.1016
v  FourierNb               0.02288      2.3657e+05          21.899         0.31997
v  total_pressure       4.3077e+05      7.3243e+05      6.4646e+05      6.2334e+05
v  Local Time Step           0.001        0.053176       0.0010021        0.001016


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.24977      2.4501e+05          63.005          7.4216


 TIME FOR THE TIME STEP              519:        0.79904E+02

===============================================================


 INSTANT    0.520000000E+01   TIME STEP NUMBER             520
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.110175298E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270795082E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72874E+02 0.61792E+01
   Friction velocity        uet   :  0.35497E-01 0.39298E+02
   Friction velocity        uk    :  0.34008E-01 0.39298E+02
   Dimensionless distance   yplus :  0.44172E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12986
   Nb of faces within the viscous sub-layer     :      11183
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13576E+02      60   0.89586E-01   0.54395E+02 0.35413E+02 
c  Velocity[X]                                      0.10138E+02 
c  Velocity[Y]                                      0.25032E+02 
c  Velocity[Z]                                      0.19226E+02 
c  Pressure     0.13665E+00    1033   0.52344E-01   0.13340E+00 0.24789E+01 
c  k            0.53097E+00      19   0.17155E-03   0.16961E-01 0.27816E+02 
c  epsilon      0.53774E+04      16   0.30634E-03   0.79971E+07 0.92258E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00087265                             5
a  epsilon                 -3.1784                             6
a  Local Time Step      3.6094e-08                        281035


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.619          18.282          1.8369         0.30211
v  Velocity[Y]             -30.523          28.502         0.97415          0.7294
v  Velocity[Z]             -50.126          31.008        -0.95818      -0.0031872
v  ǁVelocityǁ             0.014547          54.012          6.0786          6.2712
v  Pressure                 -69390      2.3271e+05      1.4672e+05      1.2359e+05
v  k                    2.3932e-06          10.299         0.07477         0.07295
v  epsilon               0.0083029      2.4117e+06          2795.8          51.487
v  TurbVisc             4.3523e-12         0.41838       0.0021668        0.036408
v  CourantNb              0.027908           27705          41.103          7.1061
v  FourierNb              0.022848      2.3657e+05          21.902         0.32039
v  total_pressure       4.3061e+05      7.3271e+05      6.4672e+05      6.2359e+05
v  Local Time Step           0.001        0.058494       0.0010021       0.0010163


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57523      2.4548e+05          63.006          7.4265


 TIME FOR THE TIME STEP              520:        0.11596E+03

===============================================================


 INSTANT    0.521000000E+01   TIME STEP NUMBER             521
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.295572312E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270856519E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.77722E+02 0.61297E+01
   Friction velocity        uet   :  0.30574E-01 0.39137E+02
   Friction velocity        uk    :  0.29509E-01 0.39137E+02
   Dimensionless distance   yplus :  0.44010E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13017
   Nb of faces within the viscous sub-layer     :      11173
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13589E+02      59   0.88307E-01   0.59056E+02 0.36887E+02 
c  Velocity[X]                                      0.10311E+02 
c  Velocity[Y]                                      0.27377E+02 
c  Velocity[Z]                                      0.21369E+02 
c  Pressure     0.13472E+00     639   0.51072E-01   0.13133E+00 0.18632E+01 
c  k            0.53119E+00      19   0.13231E-03   0.17037E-01 0.27888E+02 
c  epsilon      0.53118E+04      12   0.28614E-03   0.99813E+07 0.10394E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0361e-05                             1
a  epsilon                 -5.5017                             2
a  Local Time Step      3.5386e-08                        281047


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5743          18.727          1.8364         0.30179
v  Velocity[Y]             -31.434          36.446         0.98197         0.72861
v  Velocity[Z]             -55.605          35.604        -0.94884      -0.0042523
v  ǁVelocityǁ               0.0148          60.259           6.082           6.275
v  Pressure                 -69739      2.3272e+05      1.4671e+05      1.2362e+05
v  k                    2.3658e-06          10.364        0.074905        0.073194
v  epsilon               0.0084757      2.3031e+06          2774.5          51.536
v  TurbVisc             3.8858e-12         0.41838       0.0021876        0.036567
v  CourantNb              0.034445           28260          41.076          7.1127
v  FourierNb              0.022824      2.3657e+05          21.903         0.32071
v  total_pressure       4.3026e+05      7.3272e+05      6.4671e+05      6.2362e+05
v  Local Time Step           0.001        0.064343       0.0010022       0.0010167


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6315      2.4688e+05          62.979          7.4334


 TIME FOR THE TIME STEP              521:        0.10004E+03

===============================================================


 INSTANT    0.522000000E+01   TIME STEP NUMBER             522
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.298692734E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270960028E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.77775E+02 0.66490E+01
   Friction velocity        uet   :  0.35586E-01 0.39216E+02
   Friction velocity        uk    :  0.34089E-01 0.39216E+02
   Dimensionless distance   yplus :  0.50040E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13038
   Nb of faces within the viscous sub-layer     :      11143
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13592E+02      58   0.89216E-01   0.66418E+02 0.38993E+02 
c  Velocity[X]                                      0.11216E+02 
c  Velocity[Y]                                      0.30488E+02 
c  Velocity[Z]                                      0.24714E+02 
c  Pressure     0.13878E+00     634   0.51922E-01   0.13527E+00 0.20332E+01 
c  k            0.53154E+00      23   0.10291E-03   0.16353E-01 0.27292E+02 
c  epsilon      0.52999E+04      18   0.21425E-03   0.35433E+07 0.61961E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00046393                             2
a  epsilon                 -10.267                             3
a  Local Time Step      3.4545e-08                        281092


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4883          17.967          1.8376         0.30215
v  Velocity[Y]             -36.685          35.335         0.98619         0.72845
v  Velocity[Z]             -56.427          30.933        -0.94176      -0.0059961
v  ǁVelocityǁ             0.017637          59.816          6.0874          6.2796
v  Pressure                 -70052       2.328e+05      1.4664e+05      1.2368e+05
v  k                    2.3525e-06          10.604        0.075016        0.073412
v  epsilon               0.0087492      2.3896e+06          2771.2          51.564
v  TurbVisc              3.994e-12         0.41838       0.0022101        0.036709
v  CourantNb              0.034813           28947          41.066          7.1174
v  FourierNb              0.022807      2.3657e+05          21.905         0.32108
v  total_pressure       4.2995e+05       7.328e+05      6.4664e+05      6.2368e+05
v  Local Time Step           0.001        0.070778       0.0010021       0.0010167


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76541      2.4646e+05           62.97          7.4384


 TIME FOR THE TIME STEP              522:        0.87143E+02

===============================================================


 INSTANT    0.523000000E+01   TIME STEP NUMBER             523
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.772378701E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271153178E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.90625E+02 0.63977E+01
   Friction velocity        uet   :  0.34490E-01 0.39195E+02
   Friction velocity        uk    :  0.34088E-01 0.39195E+02
   Dimensionless distance   yplus :  0.32895E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13051
   Nb of faces within the viscous sub-layer     :      11140
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13606E+02      60   0.91036E-01   0.67271E+02 0.39351E+02 
c  Velocity[X]                                      0.11758E+02 
c  Velocity[Y]                                      0.32857E+02 
c  Velocity[Z]                                      0.22656E+02 
c  Pressure     0.13954E+00    1512   0.53035E-01   0.13605E+00 0.86217E+01 
c  k            0.53185E+00      21   0.11336E-03   0.15223E-01 0.26324E+02 
c  epsilon      0.52798E+04      12   0.27595E-03   0.61026E+07 0.81524E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021762                             2
a  epsilon                 -3.7651                             2
a  Local Time Step       3.345e-08                        281085


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6343          17.914          1.8375         0.30242
v  Velocity[Y]             -31.229          27.214         0.98657         0.72848
v  Velocity[Z]              -50.05          35.522        -0.92996       -0.005931
v  ǁVelocityǁ             0.018844          54.916           6.092          6.2814
v  Pressure                 -71906      2.3133e+05      1.4502e+05      1.2246e+05
v  k                    2.3815e-06          10.639        0.075082        0.073615
v  epsilon               0.0090452      2.3265e+06          2763.7          51.607
v  TurbVisc             3.9635e-12         0.41838       0.0022319        0.036834
v  CourantNb                0.1419           29896          41.047           7.124
v  FourierNb              0.022797      2.3657e+05          21.905         0.32133
v  total_pressure       4.2809e+05      7.3133e+05      6.4502e+05      6.2246e+05
v  Local Time Step           0.001        0.077856       0.0010021       0.0010164


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.80978      2.4761e+05          62.953          7.4453


 TIME FOR THE TIME STEP              523:        0.13358E+03

===============================================================


 INSTANT    0.524000000E+01   TIME STEP NUMBER             524
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.931332779E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270964475E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70608E+02 0.60448E+01
   Friction velocity        uet   :  0.36070E-01 0.36486E+02
   Friction velocity        uk    :  0.41659E-01 0.36486E+02
   Dimensionless distance   yplus :  0.23296E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13079
   Nb of faces within the viscous sub-layer     :      11156
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13598E+02      56   0.90201E-01   0.64001E+02 0.38334E+02 
c  Velocity[X]                                      0.12392E+02 
c  Velocity[Y]                                      0.31770E+02 
c  Velocity[Z]                                      0.19839E+02 
c  Pressure     0.14678E+00     962   0.56426E-01   0.14312E+00 0.29007E+01 
c  k            0.53248E+00      22   0.13881E-03   0.16716E-01 0.27539E+02 
c  epsilon      0.52436E+04      12   0.31487E-03   0.92310E+07 0.10101E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0054398                             4
a  epsilon                 -4.5597                             3
a  Local Time Step      3.1673e-08                        281096


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4465          17.697          1.8391         0.30246
v  Velocity[Y]              -30.22          34.381         0.98537         0.72875
v  Velocity[Z]             -51.071          31.885        -0.91963      -0.0056628
v  ǁVelocityǁ             0.019777          55.494          6.0981           6.283
v  Pressure                 -72533      2.3097e+05      1.4453e+05      1.2222e+05
v  k                    2.2681e-06          10.928        0.074985        0.073812
v  epsilon               0.0094818      2.3653e+06          2722.3          51.628
v  TurbVisc             3.9621e-12         0.41838       0.0022549        0.036945
v  CourantNb              0.054582           31572          41.016          7.1269
v  FourierNb              0.022791      2.3657e+05          21.907         0.32167
v  total_pressure       4.2747e+05      7.3097e+05      6.4453e+05      6.2222e+05
v  Local Time Step           0.001        0.062563       0.0010021       0.0010159


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77527      2.4652e+05          62.923          7.4485


 TIME FOR THE TIME STEP              524:        0.10552E+03

===============================================================


 INSTANT    0.525000000E+01   TIME STEP NUMBER             525
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.129077199E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271067017E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80657E+02 0.65035E+01
   Friction velocity        uet   :  0.33538E-01 0.34181E+02
   Friction velocity        uk    :  0.33493E-01 0.34181E+02
   Dimensionless distance   yplus :  0.35681E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13097
   Nb of faces within the viscous sub-layer     :      11128
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13606E+02      59   0.89151E-01   0.64282E+02 0.38419E+02 
c  Velocity[X]                                      0.12463E+02 
c  Velocity[Y]                                      0.31405E+02 
c  Velocity[Z]                                      0.20414E+02 
c  Pressure     0.15887E+00     490   0.61070E-01   0.15462E+00 0.23297E+01 
c  k            0.53283E+00      23   0.10743E-03   0.14661E-01 0.25815E+02 
c  epsilon      0.52307E+04      25   0.50046E-03   0.99956E+07 0.10538E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1874e-05                             1
a  epsilon                 -4.1505                             2
a  Local Time Step      3.1135e-08                        281102


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3184          17.943          1.8413         0.30262
v  Velocity[Y]             -33.512          28.886         0.98719         0.72968
v  Velocity[Z]             -52.302          38.962        -0.90996      -0.0059108
v  ǁVelocityǁ             0.019695          56.685          6.1088          6.2863
v  Pressure                 -72584       2.311e+05      1.4446e+05      1.2231e+05
v  k                    2.2966e-06          11.055        0.075169        0.073974
v  epsilon                0.010177      2.3182e+06            2709           51.74
v  TurbVisc             3.7861e-12         0.41838       0.0022775        0.037043
v  CourantNb                     0           32118          40.992          7.1311
v  FourierNb               0.02279      2.3657e+05          21.909         0.32178
v  total_pressure       4.2742e+05       7.311e+05      6.4446e+05      6.2231e+05
v  Local Time Step           0.001          0.0382        0.001002       0.0010146


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51264      2.4221e+05            62.9          7.4529


 TIME FOR THE TIME STEP              525:        0.81082E+02

===============================================================


 INSTANT    0.526000000E+01   TIME STEP NUMBER             526
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.405799809E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271091983E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71006E+02 0.67694E+01
   Friction velocity        uet   :  0.37772E-01 0.29159E+02
   Friction velocity        uk    :  0.43177E-01 0.29159E+02
   Dimensionless distance   yplus :  0.36909E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13118
   Nb of faces within the viscous sub-layer     :      11064
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13613E+02      55   0.90101E-01   0.63335E+02 0.38118E+02 
c  Velocity[X]                                      0.12592E+02 
c  Velocity[Y]                                      0.28597E+02 
c  Velocity[Z]                                      0.22146E+02 
c  Pressure     0.16601E+00     816   0.62423E-01   0.16066E+00 0.26967E+01 
c  k            0.53247E+00      20   0.17893E-03   0.32801E-01 0.38636E+02 
c  epsilon      0.52264E+04      14   0.47365E-03   0.14050E+08 0.12517E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0026275                            24
a  epsilon                 -163.69                             4
a  Local Time Step      3.0632e-08                        281099


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3237          16.161          1.8434         0.30246
v  Velocity[Y]             -37.398          27.269         0.99006         0.73148
v  Velocity[Z]             -50.787          31.717        -0.90514       -0.006049
v  ǁVelocityǁ             0.018618          53.936          6.1224            6.29
v  Pressure                 -72823      2.3095e+05      1.4404e+05       1.221e+05
v  k                    5.8311e-07          10.897        0.074996        0.074085
v  epsilon                0.010866       2.344e+06          2705.4          51.734
v  TurbVisc             3.8402e-12         0.41838       0.0022863        0.037127
v  CourantNb              0.073657           32645          41.031          7.1361
v  FourierNb              0.022791      2.3657e+05          21.909         0.32208
v  total_pressure       4.2718e+05      7.3095e+05      6.4404e+05       6.221e+05
v  Local Time Step           0.001        0.026261       0.0010019       0.0010141


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41581       2.415e+05          62.939          7.4582


 TIME FOR THE TIME STEP              526:        0.10344E+03

===============================================================


 INSTANT    0.527000000E+01   TIME STEP NUMBER             527
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.262471098E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271113603E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74598E+02 0.66030E+01
   Friction velocity        uet   :  0.38205E-01 0.27981E+02
   Friction velocity        uk    :  0.48907E-01 0.27981E+02
   Dimensionless distance   yplus :  0.35704E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13161
   Nb of faces within the viscous sub-layer     :      11029
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13615E+02      59   0.87857E-01   0.58518E+02 0.36600E+02 
c  Velocity[X]                                      0.11868E+02 
c  Velocity[Y]                                      0.24631E+02 
c  Velocity[Z]                                      0.22019E+02 
c  Pressure     0.16285E+00     897   0.59549E-01   0.15612E+00 0.28940E+01 
c  k            0.53269E+00      24   0.16077E-03   0.25302E-01 0.33908E+02 
c  epsilon      0.52239E+04      14   0.45445E-03   0.10726E+08 0.10953E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019801                             1
a  epsilon                 -4.0101                             8
a  Local Time Step      2.9397e-08                        281110


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4439          18.093          1.8451          0.3023
v  Velocity[Y]             -35.261          26.324         0.99168         0.73269
v  Velocity[Z]             -52.654          36.812        -0.90183      -0.0061547
v  ǁVelocityǁ             0.020368          57.739          6.1345          6.2932
v  Pressure                 -73096      2.3069e+05      1.4353e+05      1.2182e+05
v  k                     2.824e-07          10.828        0.074766        0.074156
v  epsilon               0.0087187       2.303e+06          2695.7          51.724
v  TurbVisc             3.7694e-12         0.41838       0.0022886        0.037199
v  CourantNb              0.017765           34017          41.118          7.1414
v  FourierNb              0.022794      2.3656e+05          21.906         0.32222
v  total_pressure        4.269e+05      7.3069e+05      6.4353e+05      6.2182e+05
v  Local Time Step           0.001        0.028887       0.0010019        0.001014


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53151      2.3925e+05          63.024          7.4636


 TIME FOR THE TIME STEP              527:        0.10168E+03

===============================================================


 INSTANT    0.528000000E+01   TIME STEP NUMBER             528
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.210818792E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271148248E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76950E+02 0.76428E+01
   Friction velocity        uet   :  0.39156E-01 0.26765E+02
   Friction velocity        uk    :  0.54297E-01 0.26765E+02
   Dimensionless distance   yplus :  0.34152E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13228
   Nb of faces within the viscous sub-layer     :      11040
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13621E+02      56   0.88655E-01   0.51478E+02 0.34294E+02 
c  Velocity[X]                                      0.10599E+02 
c  Velocity[Y]                                      0.21413E+02 
c  Velocity[Z]                                      0.19467E+02 
c  Pressure     0.14807E+00    1040   0.52689E-01   0.14063E+00 0.34856E+01 
c  k            0.53278E+00      21   0.17503E-03   0.19248E-01 0.29601E+02 
c  epsilon      0.51950E+04      13   0.57853E-03   0.13964E+08 0.12540E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012209                             2
a  epsilon                 -4.0963                             6
a  Local Time Step      2.8222e-08                        281130


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4087          17.202          1.8449         0.30157
v  Velocity[Y]             -34.418          25.633         0.99154          0.7335
v  Velocity[Z]             -51.099          31.833        -0.89811      -0.0056295
v  ǁVelocityǁ            0.0092556          55.854          6.1407           6.296
v  Pressure                 -73228      2.3021e+05      1.4285e+05       1.214e+05
v  k                    2.2917e-06          10.975        0.074566        0.074228
v  epsilon              0.00081857      2.3492e+06          2681.4           51.77
v  TurbVisc             3.7121e-12         0.41838       0.0022875        0.037259
v  CourantNb              0.040835           35433          41.213          7.1455
v  FourierNb                0.0228      2.3656e+05          21.902         0.32223
v  total_pressure       4.2677e+05      7.3021e+05      6.4285e+05       6.214e+05
v  Local Time Step           0.001        0.031775       0.0010018       0.0010133


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36132      2.3893e+05          63.115          7.4678


 TIME FOR THE TIME STEP              528:        0.10321E+03

===============================================================


 INSTANT    0.529000000E+01   TIME STEP NUMBER             529
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.460456473E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271095789E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75976E+02 0.69280E+01
   Friction velocity        uet   :  0.38463E-01 0.28353E+02
   Friction velocity        uk    :  0.51633E-01 0.28353E+02
   Dimensionless distance   yplus :  0.36178E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13233
   Nb of faces within the viscous sub-layer     :      11013
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13619E+02      56   0.87128E-01   0.52794E+02 0.34697E+02 
c  Velocity[X]                                      0.10412E+02 
c  Velocity[Y]                                      0.21474E+02 
c  Velocity[Z]                                      0.20908E+02 
c  Pressure     0.14688E+00     614   0.50697E-01   0.13870E+00 0.16601E+01 
c  k            0.53326E+00      21   0.90601E-04   0.10510E-01 0.21846E+02 
c  epsilon      0.51778E+04      14   0.74041E-03   0.88283E+07 0.99873E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.4254e-05                             2
a  epsilon                 -3.4302                             7
a  Local Time Step      2.8411e-08                        281127


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4696          18.333          1.8454         0.30043
v  Velocity[Y]             -30.369           24.19         0.98972         0.73384
v  Velocity[Z]              -55.15          38.014        -0.89693      -0.0060605
v  ǁVelocityǁ             0.019805          59.906          6.1491           6.299
v  Pressure                 -72889      2.3034e+05      1.4277e+05      1.2142e+05
v  k                    2.3216e-06          10.896        0.074528        0.074309
v  epsilon                0.012605      2.2793e+06            2687          51.814
v  TurbVisc             3.8713e-12         0.41838       0.0022909        0.037311
v  CourantNb              0.030686           35197          41.193          7.1493
v  FourierNb              0.022808      2.3656e+05          21.899         0.32242
v  total_pressure       4.2711e+05      7.3034e+05      6.4277e+05      6.2142e+05
v  Local Time Step           0.001        0.019546       0.0010017       0.0010128


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38397      2.3701e+05          63.092          7.4718


 TIME FOR THE TIME STEP              529:        0.85516E+02

===============================================================


 INSTANT    0.530000000E+01   TIME STEP NUMBER             530
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.567627223E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271095888E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88165E+02 0.72320E+01
   Friction velocity        uet   :  0.39245E-01 0.25374E+02
   Friction velocity        uk    :  0.46138E-01 0.25374E+02
   Dimensionless distance   yplus :  0.29994E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13246
   Nb of faces within the viscous sub-layer     :      10990
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13625E+02      54   0.88876E-01   0.53697E+02 0.35008E+02 
c  Velocity[X]                                      0.10606E+02 
c  Velocity[Y]                                      0.20826E+02 
c  Velocity[Z]                                      0.22264E+02 
c  Pressure     0.13769E+00     769   0.48129E-01   0.12948E+00 0.22058E+01 
c  k            0.53328E+00      21   0.79208E-04   0.75080E-02 0.18456E+02 
c  epsilon      0.51869E+04      12   0.46034E-03   0.94310E+07 0.10290E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016855                             2
a  epsilon                 -3.5829                             8
a  Local Time Step      2.8167e-08                        281130


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4026          15.284          1.8457         0.30007
v  Velocity[Y]             -30.476          23.944         0.99009         0.73392
v  Velocity[Z]             -47.107           32.15        -0.89688      -0.0064558
v  ǁVelocityǁ             0.010314          50.068          6.1564          6.3011
v  Pressure                 -72545      2.3003e+05      1.4239e+05      1.2121e+05
v  k                    2.3193e-06          10.997        0.074757        0.074418
v  epsilon                0.013094      2.3378e+06          2699.3           51.95
v  TurbVisc               3.79e-12         0.41838       0.0023007        0.037357
v  CourantNb              0.043882           35502          41.272          7.1535
v  FourierNb              0.022819      2.3656e+05          21.899         0.32261
v  total_pressure       4.2745e+05      7.3003e+05      6.4239e+05      6.2121e+05
v  Local Time Step           0.001        0.021501       0.0010017       0.0010124


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63303      2.3859e+05          63.171          7.4762


 TIME FOR THE TIME STEP              530:        0.89422E+02

===============================================================


 INSTANT    0.531000000E+01   TIME STEP NUMBER             531
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.208894936E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271129014E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65745E+02 0.72204E+01
   Friction velocity        uet   :  0.31759E-01 0.23845E+02
   Friction velocity        uk    :  0.42837E-01 0.23845E+02
   Dimensionless distance   yplus :  0.23901E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13260
   Nb of faces within the viscous sub-layer     :      10995
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13621E+02      54   0.87129E-01   0.52961E+02 0.34758E+02 
c  Velocity[X]                                      0.11149E+02 
c  Velocity[Y]                                      0.20861E+02 
c  Velocity[Z]                                      0.20950E+02 
c  Pressure     0.13643E+00     721   0.48434E-01   0.12804E+00 0.15656E+01 
c  k            0.53377E+00      18   0.66586E-04   0.64947E-02 0.17124E+02 
c  epsilon      0.51933E+04      12   0.33489E-03   0.95999E+07 0.10363E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023051                             2
a  epsilon                 -2.3262                             9
a  Local Time Step      2.8844e-08                        281117


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3605          18.154          1.8443          0.3008
v  Velocity[Y]             -32.611          23.719         0.99557         0.73409
v  Velocity[Z]             -53.592          37.898        -0.89739       -0.006878
v  ǁVelocityǁ            0.0038434          58.807          6.1626           6.302
v  Pressure                 -72104      2.3009e+05      1.4225e+05      1.2119e+05
v  k                    2.4597e-06          11.172         0.07495        0.074539
v  epsilon                0.013595      2.2809e+06          2701.4          52.116
v  TurbVisc             3.9302e-12         0.41838       0.0023171          0.0374
v  CourantNb             0.0096358           34669          41.321          7.1582
v  FourierNb              0.022833      2.3656e+05          21.898         0.32271
v  total_pressure        4.279e+05      7.3009e+05      6.4225e+05      6.2119e+05
v  Local Time Step           0.001        0.019764       0.0010016       0.0010121


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40909      2.3686e+05          63.219          7.4809


 TIME FOR THE TIME STEP              531:        0.80241E+02

===============================================================


 INSTANT    0.532000000E+01   TIME STEP NUMBER             532
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.450539121E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271142257E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.81280E+02 0.77775E+01
   Friction velocity        uet   :  0.33356E-01 0.21305E+02
   Friction velocity        uk    :  0.33915E-01 0.21305E+02
   Dimensionless distance   yplus :  0.25876E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13261
   Nb of faces within the viscous sub-layer     :      10975
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13622E+02      54   0.87561E-01   0.50451E+02 0.33921E+02 
c  Velocity[X]                                      0.11140E+02 
c  Velocity[Y]                                      0.19514E+02 
c  Velocity[Z]                                      0.19797E+02 
c  Pressure     0.13473E+00     527   0.48502E-01   0.12634E+00 0.16111E+01 
c  k            0.53376E+00      18   0.81358E-04   0.65484E-02 0.17232E+02 
c  epsilon      0.52039E+04      12   0.24563E-03   0.70166E+07 0.88412E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014649                             3
a  epsilon                 -2.8697                            10
a  Local Time Step      2.8621e-08                        281118


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2953          15.188          1.8432          0.3017
v  Velocity[Y]             -36.799          25.303          1.0042         0.73479
v  Velocity[Z]              -43.54          32.392        -0.90203      -0.0068522
v  ǁVelocityǁ            0.0071753          47.555          6.1698          6.3017
v  Pressure                 -71531      2.3026e+05       1.422e+05      1.2117e+05
v  k                    2.4236e-06          10.938        0.075222        0.074635
v  epsilon                0.011768      2.3287e+06          2717.4          52.247
v  TurbVisc             4.0281e-12         0.41838       0.0023354        0.037439
v  CourantNb            4.1115e-05           34940          41.398          7.1607
v  FourierNb              0.022849      2.3656e+05          21.899         0.32302
v  total_pressure       4.2847e+05      7.3026e+05       6.422e+05      6.2117e+05
v  Local Time Step           0.001        0.016956       0.0010016       0.0010119


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.35199      2.3841e+05          63.297          7.4837


 TIME FOR THE TIME STEP              532:        0.77153E+02

===============================================================


 INSTANT    0.533000000E+01   TIME STEP NUMBER             533
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.569416195E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271166476E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65047E+02 0.68925E+01
   Friction velocity        uet   :  0.26613E-01 0.21025E+02
   Friction velocity        uk    :  0.30815E-01 0.21025E+02
   Dimensionless distance   yplus :  0.21780E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13263
   Nb of faces within the viscous sub-layer     :      10949
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13624E+02      53   0.85817E-01   0.50745E+02 0.34013E+02 
c  Velocity[X]                                      0.11041E+02 
c  Velocity[Y]                                      0.19273E+02 
c  Velocity[Z]                                      0.20432E+02 
c  Pressure     0.13110E+00     560   0.47331E-01   0.12265E+00 0.17335E+01 
c  k            0.53356E+00      19   0.87763E-04   0.72114E-02 0.18094E+02 
c  epsilon      0.52175E+04      11   0.26256E-03   0.63515E+07 0.83922E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.0248e-05                             2
a  epsilon                  -3.992                            10
a  Local Time Step      2.8689e-08                        281147


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1876          18.322          1.8394         0.30203
v  Velocity[Y]             -32.771          26.337          1.0147         0.73518
v  Velocity[Z]             -55.438          39.304        -0.90892      -0.0066963
v  ǁVelocityǁ             0.010537          60.709          6.1791          6.3011
v  Pressure                 -71099      2.3043e+05      1.4216e+05      1.2112e+05
v  k                    2.4676e-06          11.079        0.075502        0.074704
v  epsilon               0.0059098      2.2767e+06          2727.4           52.38
v  TurbVisc              4.012e-12         0.41838        0.002354        0.037472
v  CourantNb                     0           34857           41.49          7.1632
v  FourierNb              0.022867      2.3656e+05            21.9         0.32314
v  total_pressure        4.289e+05      7.3043e+05      6.4216e+05      6.2112e+05
v  Local Time Step           0.001        0.016508       0.0010016       0.0010116


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52057      2.3699e+05           63.39          7.4863


 TIME FOR THE TIME STEP              533:        0.78850E+02

===============================================================


 INSTANT    0.534000000E+01   TIME STEP NUMBER             534
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.192050245E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271103664E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84041E+02 0.66568E+01
   Friction velocity        uet   :  0.33909E-01 0.20370E+02
   Friction velocity        uk    :  0.44915E-01 0.20370E+02
   Dimensionless distance   yplus :  0.22932E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13307
   Nb of faces within the viscous sub-layer     :      10963
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13620E+02      52   0.89572E-01   0.50249E+02 0.33855E+02 
c  Velocity[X]                                      0.10889E+02 
c  Velocity[Y]                                      0.19700E+02 
c  Velocity[Z]                                      0.19660E+02 
c  Pressure     0.12136E+00     554   0.44465E-01   0.11348E+00 0.17288E+01 
c  k            0.53265E+00      20   0.72225E-04   0.62411E-02 0.16834E+02 
c  epsilon      0.52419E+04      13   0.28853E-03   0.45969E+07 0.71073E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -6.446e-05                             1
a  epsilon                 -2.8239                            10
a  Local Time Step      2.9069e-08                        281163


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2175           15.17          1.8356         0.30161
v  Velocity[Y]             -29.437          29.733          1.0254         0.73519
v  Velocity[Z]              -43.02          32.412        -0.91745      -0.0062604
v  ǁVelocityǁ               0.0211          46.673          6.1876          6.3003
v  Pressure                 -70747      2.3064e+05      1.4216e+05      1.2108e+05
v  k                     2.536e-06          11.027         0.07587        0.074739
v  epsilon                0.015167      2.3219e+06          2750.5          52.439
v  TurbVisc             4.0206e-12         0.41838       0.0023718          0.0375
v  CourantNb              0.092133           34401          41.612           7.165
v  FourierNb               0.02289      2.3656e+05          21.901         0.32332
v  total_pressure       4.2925e+05      7.3064e+05      6.4216e+05      6.2108e+05
v  Local Time Step           0.001        0.014969       0.0010016       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62436      2.3922e+05          63.513          7.4884


 TIME FOR THE TIME STEP              534:        0.89975E+02

===============================================================


 INSTANT    0.535000000E+01   TIME STEP NUMBER             535
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.115634239E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271027068E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59382E+02 0.63885E+01
   Friction velocity        uet   :  0.15005E-01 0.18790E+02
   Friction velocity        uk    :  0.34508E-01 0.18790E+02
   Dimensionless distance   yplus :  0.20745E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13324
   Nb of faces within the viscous sub-layer     :      10939
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13616E+02      50   0.90082E-01   0.51112E+02 0.34158E+02 
c  Velocity[X]                                      0.11004E+02 
c  Velocity[Y]                                      0.20647E+02 
c  Velocity[Z]                                      0.19461E+02 
c  Pressure     0.12058E+00     575   0.44005E-01   0.11282E+00 0.18141E+01 
c  k            0.53259E+00      18   0.48231E-04   0.48264E-02 0.14818E+02 
c  epsilon      0.52738E+04      13   0.34908E-03   0.70393E+07 0.87415E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.9989e-05                             1
a  epsilon                 -2.6626                             7
a  Local Time Step      2.9384e-08                        281155


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2386          18.332          1.8293          0.3007
v  Velocity[Y]             -30.986          31.948          1.0349         0.73509
v  Velocity[Z]             -55.477          34.862        -0.92613      -0.0052962
v  ǁVelocityǁ              0.01651          60.783          6.1951          6.2994
v  Pressure                 -70648      2.3077e+05      1.4218e+05      1.2105e+05
v  k                    2.5156e-06          11.122        0.076223        0.074763
v  epsilon                0.015373      2.2997e+06          2775.1          52.528
v  TurbVisc             4.2033e-12         0.41838       0.0023881        0.037522
v  CourantNb             0.0044738           34033          41.698          7.1661
v  FourierNb              0.022917      2.3656e+05          21.903         0.32344
v  total_pressure       4.2935e+05      7.3077e+05      6.4218e+05      6.2105e+05
v  Local Time Step           0.001        0.016466       0.0010016       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62636      2.4019e+05          63.602          7.4895


 TIME FOR THE TIME STEP              535:        0.89622E+02

===============================================================


 INSTANT    0.536000000E+01   TIME STEP NUMBER             536
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.293276200E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270857403E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84008E+02 0.74949E+01
   Friction velocity        uet   :  0.73328E-02 0.18800E+02
   Friction velocity        uk    :  0.34650E-01 0.18800E+02
   Dimensionless distance   yplus :  0.12644E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13333
   Nb of faces within the viscous sub-layer     :      10940
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13609E+02      56   0.87190E-01   0.52109E+02 0.34500E+02 
c  Velocity[X]                                      0.10816E+02 
c  Velocity[Y]                                      0.21949E+02 
c  Velocity[Z]                                      0.19344E+02 
c  Pressure     0.11823E+00     982   0.43408E-01   0.11070E+00 0.40721E+01 
c  k            0.53307E+00      19   0.66281E-04   0.54051E-02 0.15617E+02 
c  epsilon      0.52868E+04      13   0.30897E-03   0.11125E+08 0.10944E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.3866e-05                             1
a  epsilon                 -1.4803                             6
a  Local Time Step      2.9088e-08                        281168


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.202          15.099          1.8289         0.30015
v  Velocity[Y]             -32.741          33.488          1.0431         0.73522
v  Velocity[Z]             -43.223          32.476        -0.93356      -0.0046089
v  ǁVelocityǁ             0.017133          46.551          6.2067          6.2992
v  Pressure                 -69843      2.3165e+05      1.4284e+05      1.2157e+05
v  k                    2.5613e-06          11.251        0.076569        0.074795
v  epsilon                0.015314      2.3051e+06          2790.1          52.649
v  TurbVisc             4.0766e-12         0.41838       0.0024038         0.03754
v  CourantNb              0.010124           34379          41.792          7.1673
v  FourierNb              0.022949      2.3656e+05          21.903         0.32351
v  total_pressure       4.3016e+05      7.3165e+05      6.4284e+05      6.2157e+05
v  Local Time Step           0.001        0.015694       0.0010015        0.001011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56659       2.391e+05          63.695          7.4908


 TIME FOR THE TIME STEP              536:        0.10844E+03

===============================================================


 INSTANT    0.537000000E+01   TIME STEP NUMBER             537
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.903962396E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270804369E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62322E+02 0.76925E+01
   Friction velocity        uet   :  0.18212E-01 0.17906E+02
   Friction velocity        uk    :  0.40266E-01 0.17906E+02
   Dimensionless distance   yplus :  0.11040E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13355
   Nb of faces within the viscous sub-layer     :      10930
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13613E+02      54   0.88617E-01   0.54656E+02 0.35334E+02 
c  Velocity[X]                                      0.11042E+02 
c  Velocity[Y]                                      0.24063E+02 
c  Velocity[Z]                                      0.19550E+02 
c  Pressure     0.12383E+00     832   0.45096E-01   0.11616E+00 0.33842E+01 
c  k            0.53338E+00      22   0.44535E-04   0.39108E-02 0.13315E+02 
c  epsilon      0.53119E+04      11   0.24331E-03   0.44279E+07 0.68904E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -12.156                             6
a  Local Time Step       2.874e-08                        281174


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -7.13          18.292          1.8249         0.30002
v  Velocity[Y]             -31.442          31.365          1.0515         0.73551
v  Velocity[Z]             -55.617          39.963        -0.94116      -0.0043163
v  ǁVelocityǁ             0.013288            60.9          6.2162          6.2984
v  Pressure                 -69414      2.3232e+05      1.4339e+05      1.2197e+05
v  k                    1.5592e-06          11.046        0.076799        0.074817
v  epsilon                0.015088      2.2871e+06            2800          52.723
v  TurbVisc             4.2475e-12         0.41838       0.0024219        0.037555
v  CourantNb            0.00053083           34795           41.88          7.1702
v  FourierNb              0.022982      2.3656e+05          21.906         0.32383
v  total_pressure       4.3059e+05      7.3232e+05      6.4339e+05      6.2197e+05
v  Local Time Step           0.001        0.016167       0.0010015       0.0010109


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56506      2.3964e+05          63.786           7.494


 TIME FOR THE TIME STEP              537:        0.96931E+02

===============================================================


 INSTANT    0.538000000E+01   TIME STEP NUMBER             538
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.646334866E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270785751E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84528E+02 0.73334E+01
   Friction velocity        uet   :  0.35614E-01 0.18759E+02
   Friction velocity        uk    :  0.43725E-01 0.18759E+02
   Dimensionless distance   yplus :  0.15751E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13375
   Nb of faces within the viscous sub-layer     :      10929
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13611E+02      49   0.87993E-01   0.55585E+02 0.35619E+02 
c  Velocity[X]                                      0.11572E+02 
c  Velocity[Y]                                      0.23926E+02 
c  Velocity[Z]                                      0.20087E+02 
c  Pressure     0.12681E+00     446   0.46527E-01   0.11925E+00 0.17355E+01 
c  k            0.53300E+00      22   0.42607E-04   0.36938E-02 0.12933E+02 
c  epsilon      0.53240E+04      11   0.26165E-03   0.70030E+07 0.86280E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -3.2354                             7
a  Local Time Step      2.8232e-08                        281197


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1291          15.025          1.8237         0.30026
v  Velocity[Y]             -33.401          36.298          1.0582         0.73527
v  Velocity[Z]             -44.421          32.286        -0.95004      -0.0033485
v  ǁVelocityǁ            0.0048379          47.059          6.2266          6.2968
v  Pressure                 -69449      2.3238e+05      1.4343e+05      1.2196e+05
v  k                     4.345e-07          11.024        0.077099        0.074838
v  epsilon               0.0080327      2.3149e+06          2815.8          52.773
v  TurbVisc             4.3119e-12         0.41838       0.0024394        0.037568
v  CourantNb              0.021851           35420          41.954          7.1709
v  FourierNb              0.023016      2.3656e+05          21.908         0.32378
v  total_pressure       4.3055e+05      7.3238e+05      6.4343e+05      6.2196e+05
v  Local Time Step           0.001         0.01643       0.0010015        0.001011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57864      2.4032e+05          63.862          7.4947


 TIME FOR THE TIME STEP              538:        0.78851E+02

===============================================================


 INSTANT    0.539000000E+01   TIME STEP NUMBER             539
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.100563682E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270697470E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64032E+02 0.69124E+01
   Friction velocity        uet   :  0.34870E-01 0.18787E+02
   Friction velocity        uk    :  0.41859E-01 0.18787E+02
   Dimensionless distance   yplus :  0.23972E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13391
   Nb of faces within the viscous sub-layer     :      10901
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13606E+02      52   0.88796E-01   0.56231E+02 0.35853E+02 
c  Velocity[X]                                      0.11510E+02 
c  Velocity[Y]                                      0.25325E+02 
c  Velocity[Z]                                      0.19396E+02 
c  Pressure     0.13341E+00     901   0.48849E-01   0.12571E+00 0.51608E+01 
c  k            0.53315E+00      17   0.47563E-04   0.34057E-02 0.12418E+02 
c  epsilon      0.53365E+04      11   0.25230E-03   0.46476E+07 0.70140E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -3.3912                             9
a  Local Time Step      2.8217e-08                        281204


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1514          18.132           1.825         0.30086
v  Velocity[Y]             -31.851          31.915          1.0635          0.7355
v  Velocity[Z]             -55.218          33.254        -0.95617      -0.0036941
v  ǁVelocityǁ             0.018286          60.495          6.2361          6.2963
v  Pressure                 -68895      2.3331e+05      1.4433e+05      1.2267e+05
v  k                    1.9809e-06          11.201        0.077432        0.074863
v  epsilon               0.0051081      2.2899e+06          2829.2          52.878
v  TurbVisc             4.1733e-12         0.41838       0.0024569        0.037579
v  CourantNb              0.061729           35439          41.998          7.1716
v  FourierNb              0.023045      2.3656e+05          21.911         0.32403
v  total_pressure       4.3111e+05      7.3331e+05      6.4433e+05      6.2267e+05
v  Local Time Step           0.001        0.016488       0.0010016       0.0010112


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78111      2.3827e+05          63.909          7.4956


 TIME FOR THE TIME STEP              539:        0.85218E+02

===============================================================


 INSTANT    0.540000000E+01   TIME STEP NUMBER             540
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.591251297E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270770748E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83435E+02 0.73691E+01
   Friction velocity        uet   :  0.28543E-01 0.19174E+02
   Friction velocity        uk    :  0.40496E-01 0.19174E+02
   Dimensionless distance   yplus :  0.20851E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13383
   Nb of faces within the viscous sub-layer     :      10855
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13609E+02      46   0.89854E-01   0.55224E+02 0.35519E+02 
c  Velocity[X]                                      0.10731E+02 
c  Velocity[Y]                                      0.25432E+02 
c  Velocity[Z]                                      0.19060E+02 
c  Pressure     0.13754E+00     667   0.51268E-01   0.13016E+00 0.25750E+01 
c  k            0.53339E+00      19   0.78207E-04   0.43339E-02 0.14010E+02 
c  epsilon      0.53445E+04      11   0.27604E-03   0.38367E+07 0.63570E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                -0.56066                             6
a  Local Time Step       2.895e-08                        281208


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1924          15.034          1.8294         0.30122
v  Velocity[Y]             -33.131          34.509          1.0674         0.73488
v  Velocity[Z]             -47.247          32.267        -0.96328       -0.004528
v  ǁVelocityǁ            0.0092218          49.907           6.245           6.296
v  Pressure                 -68680      2.3365e+05       1.447e+05      1.2294e+05
v  k                    2.5638e-06          11.133        0.077725        0.074884
v  epsilon                0.015672      2.3218e+06          2840.1          52.956
v  TurbVisc             4.1365e-12         0.41838         0.00247        0.037589
v  CourantNb                     0           34542          42.108          7.1728
v  FourierNb              0.023067      2.3656e+05          21.911         0.32407
v  total_pressure       4.3132e+05      7.3365e+05       6.447e+05      6.2294e+05
v  Local Time Step           0.001        0.017296       0.0010015       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75383      2.3676e+05          64.019          7.4968


 TIME FOR THE TIME STEP              540:        0.81029E+02

===============================================================


 INSTANT    0.541000000E+01   TIME STEP NUMBER             541
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.230564870E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270944143E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70968E+02 0.73238E+01
   Friction velocity        uet   :  0.35825E-01 0.17860E+02
   Friction velocity        uk    :  0.37841E-01 0.17860E+02
   Dimensionless distance   yplus :  0.22790E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13390
   Nb of faces within the viscous sub-layer     :      10872
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13608E+02      50   0.88190E-01   0.55590E+02 0.35646E+02 
c  Velocity[X]                                      0.10487E+02 
c  Velocity[Y]                                      0.25178E+02 
c  Velocity[Z]                                      0.19925E+02 
c  Pressure     0.14049E+00     391   0.52603E-01   0.13359E+00 0.17223E+01 
c  k            0.53402E+00      18   0.10687E-03   0.51793E-02 0.15105E+02 
c  epsilon      0.53551E+04      11   0.22472E-03   0.31970E+07 0.57964E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.5236e-06                             1
a  epsilon                 -12.994                             7
a  Local Time Step      2.8057e-08                        281211


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2118          17.913          1.8315         0.30169
v  Velocity[Y]             -31.424          31.564          1.0684         0.73395
v  Velocity[Z]             -55.119          33.742        -0.96646      -0.0053364
v  ǁVelocityǁ             0.021585          60.273          6.2516          6.2959
v  Pressure                 -68857      2.3361e+05       1.447e+05      1.2293e+05
v  k                    1.5236e-06          11.379        0.077734        0.074914
v  epsilon                0.015545      2.2875e+06          2839.3          52.978
v  TurbVisc             4.2282e-12         0.41838       0.0024796        0.037596
v  CourantNb             0.0073048           35642          42.207          7.1757
v  FourierNb               0.02308      2.3656e+05          21.911         0.32421
v  total_pressure       4.3114e+05      7.3361e+05       6.447e+05      6.2293e+05
v  Local Time Step           0.001          0.0181       0.0010015       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53064      2.3885e+05          64.118          7.4999


 TIME FOR THE TIME STEP              541:        0.66098E+02

===============================================================


 INSTANT    0.542000000E+01   TIME STEP NUMBER             542
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.823725063E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270939531E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83964E+02 0.79980E+01
   Friction velocity        uet   :  0.35780E-01 0.25132E+02
   Friction velocity        uk    :  0.35331E-01 0.25132E+02
   Dimensionless distance   yplus :  0.26639E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13430
   Nb of faces within the viscous sub-layer     :      10837
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13616E+02      49   0.89778E-01   0.55609E+02 0.35628E+02 
c  Velocity[X]                                      0.10146E+02 
c  Velocity[Y]                                      0.23881E+02 
c  Velocity[Z]                                      0.21583E+02 
c  Pressure     0.14011E+00     301   0.53407E-01   0.13356E+00 0.16841E+01 
c  k            0.53493E+00      21   0.12591E-03   0.57572E-02 0.16033E+02 
c  epsilon      0.53574E+04      11   0.21766E-03   0.33894E+07 0.59543E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.5353e-07                             1
a  epsilon                 -5.8123                             7
a  Local Time Step      2.7845e-08                        281193


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3032          15.081          1.8351         0.30205
v  Velocity[Y]             -32.013          34.971          1.0687         0.73324
v  Velocity[Z]             -48.175          36.808         -0.9695      -0.0060613
v  ǁVelocityǁ             0.015944          51.064           6.256          6.2966
v  Pressure                 -68953      2.3351e+05       1.447e+05      1.2293e+05
v  k                    4.5353e-07          11.298        0.077968        0.074967
v  epsilon                0.011977      2.2989e+06          2849.5          53.103
v  TurbVisc             4.2053e-12         0.41838       0.0024838        0.037604
v  CourantNb             0.0098355           35913          42.249          7.1755
v  FourierNb              0.023084      2.3656e+05          21.911         0.32426
v  total_pressure       4.3105e+05      7.3351e+05       6.447e+05      6.2293e+05
v  Local Time Step           0.001        0.018605       0.0010015       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59033      2.3973e+05          64.159          7.4998


 TIME FOR THE TIME STEP              542:        0.67725E+02

===============================================================


 INSTANT    0.543000000E+01   TIME STEP NUMBER             543
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.636358888E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271003746E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68289E+02 0.80470E+01
   Friction velocity        uet   :  0.37263E-01 0.22237E+02
   Friction velocity        uk    :  0.37370E-01 0.22237E+02
   Dimensionless distance   yplus :  0.26137E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13419
   Nb of faces within the viscous sub-layer     :      10823
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13615E+02      53   0.89282E-01   0.52096E+02 0.34483E+02 
c  Velocity[X]                                      0.10040E+02 
c  Velocity[Y]                                      0.21674E+02 
c  Velocity[Z]                                      0.20382E+02 
c  Pressure     0.13858E+00     364   0.53646E-01   0.13275E+00 0.16306E+01 
c  k            0.53550E+00      19   0.70396E-04   0.38953E-02 0.13186E+02 
c  epsilon      0.53528E+04      12   0.17283E-03   0.18486E+07 0.44073E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.8115e-05                             1
a  epsilon                 -10.264                             7
a  Local Time Step      2.6973e-08                        281198


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3843          17.456          1.8351         0.30218
v  Velocity[Y]             -32.438          30.955          1.0678         0.73262
v  Velocity[Z]             -53.463          35.166        -0.97111      -0.0067293
v  ǁVelocityǁ             0.016674          58.478          6.2573          6.2969
v  Pressure                 -69072      2.3339e+05      1.4469e+05      1.2293e+05
v  k                    2.4452e-06          11.094        0.077981        0.075034
v  epsilon              0.00014923      2.3056e+06          2842.7          53.186
v  TurbVisc             4.0911e-12         0.41838       0.0024876        0.037612
v  CourantNb             0.0027839           37074          42.268          7.1778
v  FourierNb              0.023078      2.3656e+05          21.911         0.32429
v  total_pressure       4.3093e+05      7.3339e+05      6.4469e+05      6.2293e+05
v  Local Time Step           0.001        0.019293       0.0010015       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68171      2.3934e+05          64.179          7.5021


 TIME FOR THE TIME STEP              543:        0.63513E+02

===============================================================


 INSTANT    0.544000000E+01   TIME STEP NUMBER             544
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.573455588E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271067759E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.78216E+02 0.81526E+01
   Friction velocity        uet   :  0.35740E-01 0.16829E+02
   Friction velocity        uk    :  0.41671E-01 0.16829E+02
   Dimensionless distance   yplus :  0.15772E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13423
   Nb of faces within the viscous sub-layer     :      10802
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13622E+02      47   0.89393E-01   0.48683E+02 0.33293E+02 
c  Velocity[X]                                      0.89892E+01 
c  Velocity[Y]                                      0.20711E+02 
c  Velocity[Z]                                      0.18983E+02 
c  Pressure     0.13764E+00     298   0.53014E-01   0.13229E+00 0.14823E+01 
c  k            0.53718E+00      20   0.18665E-03   0.82442E-02 0.19230E+02 
c  epsilon      0.53368E+04      11   0.18799E-03   0.26296E+07 0.52677E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.4155e-05                             1
a  epsilon                 -4.9038                             5
a  Local Time Step      2.6917e-08                        281189


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4018          15.263          1.8388         0.30225
v  Velocity[Y]             -31.568           37.35          1.0689         0.73201
v  Velocity[Z]             -45.625          38.861        -0.97182      -0.0072925
v  ǁVelocityǁ            0.0079336          49.695          6.2624          6.2984
v  Pressure                 -68909      2.3326e+05      1.4468e+05      1.2293e+05
v  k                    2.4622e-06          10.682        0.078087        0.075127
v  epsilon               0.0076956      2.3165e+06          2838.2          53.309
v  TurbVisc             4.0171e-12         0.41838       0.0024905        0.037621
v  CourantNb             0.0078096           37151          42.244          7.1789
v  FourierNb              0.023065      2.3656e+05           21.91         0.32437
v  total_pressure       4.3109e+05      7.3326e+05      6.4468e+05      6.2293e+05
v  Local Time Step           0.001        0.020551       0.0010015       0.0010114


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57111      2.3956e+05          64.154          7.5033


 TIME FOR THE TIME STEP              544:        0.62168E+02

===============================================================


 INSTANT    0.545000000E+01   TIME STEP NUMBER             545
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.165038464E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271120490E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71250E+02 0.81799E+01
   Friction velocity        uet   :  0.36242E-01 0.22454E+02
   Friction velocity        uk    :  0.39179E-01 0.22454E+02
   Dimensionless distance   yplus :  0.28652E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13420
   Nb of faces within the viscous sub-layer     :      10797
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13620E+02      51   0.93126E-01   0.47275E+02 0.32844E+02 
c  Velocity[X]                                      0.86985E+01 
c  Velocity[Y]                                      0.18905E+02 
c  Velocity[Z]                                      0.19672E+02 
c  Pressure     0.13181E+00     251   0.49269E-01   0.12703E+00 0.13676E+01 
c  k            0.53751E+00      18   0.49601E-04   0.42678E-02 0.13822E+02 
c  epsilon      0.53370E+04      13   0.18858E-03   0.17563E+07 0.43004E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.5099e-05                             1
a  epsilon                 -5.7919                             5
a  Local Time Step      2.6247e-08                        281207


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.316          17.641          1.8414         0.30216
v  Velocity[Y]             -31.782          31.365          1.0713         0.73139
v  Velocity[Z]             -54.833          34.719        -0.96876      -0.0076139
v  ǁVelocityǁ             0.015121          59.805          6.2642          6.2989
v  Pressure                 -68673      2.3324e+05      1.4467e+05      1.2293e+05
v  k                    2.4557e-06          10.842        0.078308        0.075225
v  epsilon                0.015093      2.2634e+06          2843.7          53.496
v  TurbVisc             4.0408e-12         0.41838       0.0024958        0.037631
v  CourantNb              0.029348           38100          42.271          7.1831
v  FourierNb              0.023047      2.3656e+05          21.911         0.32443
v  total_pressure       4.3133e+05      7.3324e+05      6.4467e+05      6.2293e+05
v  Local Time Step           0.001        0.018016       0.0010014       0.0010111


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38195      2.3989e+05          64.182          7.5076


 TIME FOR THE TIME STEP              545:        0.76231E+02

===============================================================


 INSTANT    0.546000000E+01   TIME STEP NUMBER             546
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.363970827E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271204616E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.82427E+02 0.78277E+01
   Friction velocity        uet   :  0.35668E-01 0.18229E+02
   Friction velocity        uk    :  0.40569E-01 0.18229E+02
   Dimensionless distance   yplus :  0.20649E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13438
   Nb of faces within the viscous sub-layer     :      10810
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13619E+02      48   0.88822E-01   0.45708E+02 0.32285E+02 
c  Velocity[X]                                      0.79596E+01 
c  Velocity[Y]                                      0.17144E+02 
c  Velocity[Z]                                      0.20604E+02 
c  Pressure     0.12886E+00     278   0.46881E-01   0.12432E+00 0.12893E+01 
c  k            0.53656E+00      18   0.10730E-03   0.55003E-02 0.15687E+02 
c  epsilon      0.53284E+04      13   0.24322E-03   0.43461E+07 0.67753E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.5538e-05                             1
a  epsilon                 -4.6296                             3
a  Local Time Step      2.6346e-08                        281202


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3265          15.131          1.8412         0.30196
v  Velocity[Y]              -31.85           37.73          1.0743         0.73095
v  Velocity[Z]             -46.877          40.279        -0.96454      -0.0076432
v  ǁVelocityǁ             0.014386          49.745          6.2659          6.3003
v  Pressure                 -68394      2.3319e+05      1.4465e+05      1.2291e+05
v  k                    2.4504e-06          10.792        0.078299        0.075297
v  epsilon                 0.01539      2.3307e+06          2835.5          53.564
v  TurbVisc             4.0464e-12         0.41838       0.0025027        0.037641
v  CourantNb             0.0093558           37957          42.265          7.1853
v  FourierNb              0.023027      2.3656e+05          21.912         0.32452
v  total_pressure       4.3161e+05      7.3319e+05      6.4465e+05      6.2291e+05
v  Local Time Step           0.001        0.017243       0.0010014       0.0010112


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59435      2.3672e+05          64.177          7.5098


 TIME FOR THE TIME STEP              546:        0.58304E+02

===============================================================


 INSTANT    0.547000000E+01   TIME STEP NUMBER             547
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.596977217E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271223863E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65232E+02 0.75188E+01
   Friction velocity        uet   :  0.23251E-01 0.21742E+02
   Friction velocity        uk    :  0.31840E-01 0.21742E+02
   Dimensionless distance   yplus :  0.27743E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13463
   Nb of faces within the viscous sub-layer     :      10803
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13618E+02      48   0.88254E-01   0.41952E+02 0.30947E+02 
c  Velocity[X]                                      0.72289E+01 
c  Velocity[Y]                                      0.14707E+02 
c  Velocity[Z]                                      0.20016E+02 
c  Pressure     0.11932E+00     365   0.42346E-01   0.11499E+00 0.12880E+01 
c  k            0.53650E+00      21   0.58211E-04   0.45784E-02 0.14279E+02 
c  epsilon      0.53301E+04      21   0.26583E-03   0.53196E+07 0.74846E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028102                             2
a  epsilon                 -4.6188                             2
a  Local Time Step      2.5276e-08                        281231


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2929          17.496          1.8402         0.30186
v  Velocity[Y]             -32.897          30.196          1.0756         0.73122
v  Velocity[Z]             -53.727          32.077        -0.96304       -0.007467
v  ǁVelocityǁ             0.012252          58.739          6.2694          6.3009
v  Pressure                 -68368       2.331e+05      1.4463e+05      1.2286e+05
v  k                    2.4448e-06          11.089        0.078603        0.075351
v  epsilon               0.0072641      2.2892e+06          2847.9          53.661
v  TurbVisc             4.0355e-12         0.41838       0.0025118        0.037649
v  CourantNb              0.011459           39563           42.28           7.189
v  FourierNb              0.023006      2.3656e+05          21.914         0.32457
v  total_pressure       4.3163e+05       7.331e+05      6.4463e+05      6.2286e+05
v  Local Time Step           0.001        0.018164       0.0010014       0.0010111


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.37698      2.3771e+05          64.194          7.5136


 TIME FOR THE TIME STEP              547:        0.77711E+02

===============================================================


 INSTANT    0.548000000E+01   TIME STEP NUMBER             548
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.236541778E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271214124E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.79126E+02 0.80876E+01
   Friction velocity        uet   :  0.30313E-01 0.16955E+02
   Friction velocity        uk    :  0.30249E-01 0.16955E+02
   Dimensionless distance   yplus :  0.20365E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13476
   Nb of faces within the viscous sub-layer     :      10807
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13616E+02      50   0.89903E-01   0.38162E+02 0.29476E+02 
c  Velocity[X]                                      0.66785E+01 
c  Velocity[Y]                                      0.13706E+02 
c  Velocity[Z]                                      0.17777E+02 
c  Pressure     0.11182E+00     420   0.38851E-01   0.10732E+00 0.11846E+01 
c  k            0.53634E+00      18   0.48600E-04   0.40132E-02 0.13381E+02 
c  epsilon      0.53403E+04      11   0.19584E-03   0.30718E+07 0.56827E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.9532e-05                             1
a  epsilon                 -3.9246                             2
a  Local Time Step      2.5842e-08                        281222


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2936          15.197          1.8385         0.30202
v  Velocity[Y]             -31.054          34.829          1.0792          0.7318
v  Velocity[Z]             -46.093          32.709        -0.96463      -0.0070349
v  ǁVelocityǁ            0.0021255          49.335          6.2741          6.3019
v  Pressure                 -68426      2.3312e+05      1.4462e+05      1.2281e+05
v  k                    2.4777e-06          11.256        0.078601         0.07538
v  epsilon                0.016042      2.3193e+06          2844.8          53.693
v  TurbVisc             4.0449e-12         0.41838        0.002522        0.037656
v  CourantNb              0.027373           38697          42.304          7.1914
v  FourierNb              0.022985      2.3656e+05          21.915         0.32459
v  total_pressure       4.3157e+05      7.3312e+05      6.4462e+05      6.2281e+05
v  Local Time Step           0.001        0.015891       0.0010014       0.0010111


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64903      2.3791e+05          64.219           7.516


 TIME FOR THE TIME STEP              548:        0.74582E+02

===============================================================


 INSTANT    0.549000000E+01   TIME STEP NUMBER             549
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.787273018E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271161779E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72779E+02 0.78755E+01
   Friction velocity        uet   :  0.34940E-01 0.15001E+02
   Friction velocity        uk    :  0.41535E-01 0.15001E+02
   Dimensionless distance   yplus :  0.17948E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13486
   Nb of faces within the viscous sub-layer     :      10772
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13606E+02      49   0.88596E-01   0.38581E+02 0.29657E+02 
c  Velocity[X]                                      0.64504E+01 
c  Velocity[Y]                                      0.14037E+02 
c  Velocity[Z]                                      0.18093E+02 
c  Pressure     0.10474E+00     440   0.35870E-01   0.10034E+00 0.10632E+01 
c  k            0.53573E+00      21   0.17780E-03   0.95696E-02 0.20131E+02 
c  epsilon      0.53432E+04      14   0.28946E-03   0.45060E+07 0.68675E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.7526e-05                             1
a  epsilon                  -4.247                             3
a  Local Time Step      2.5437e-08                        281240


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3298          17.515          1.8384         0.30207
v  Velocity[Y]             -31.828          31.058          1.0827          0.7323
v  Velocity[Z]             -55.708          35.838        -0.96918      -0.0065432
v  ǁVelocityǁ            0.0087016          60.312          6.2798           6.302
v  Pressure                 -68549      2.3324e+05      1.4461e+05      1.2279e+05
v  k                    2.5451e-06          11.604        0.078895        0.075405
v  epsilon                0.016343      2.2839e+06            2857          53.766
v  TurbVisc             4.1047e-12         0.41838         0.00253        0.037661
v  CourantNb              0.082817           39313          42.341           7.194
v  FourierNb              0.022967      2.3656e+05          21.917         0.32476
v  total_pressure       4.3145e+05      7.3324e+05      6.4461e+05      6.2279e+05
v  Local Time Step           0.001        0.017428       0.0010014       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74435       2.379e+05          64.258          7.5188


 TIME FOR THE TIME STEP              549:        0.70281E+02

===============================================================


 INSTANT    0.550000000E+01   TIME STEP NUMBER             550
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.117294556E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271088060E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80912E+02 0.74377E+01
   Friction velocity        uet   :  0.35925E-01 0.18247E+02
   Friction velocity        uk    :  0.38477E-01 0.18247E+02
   Dimensionless distance   yplus :  0.17769E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13499
   Nb of faces within the viscous sub-layer     :      10767
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13602E+02      55   0.88313E-01   0.40876E+02 0.30538E+02 
c  Velocity[X]                                      0.66879E+01 
c  Velocity[Y]                                      0.14373E+02 
c  Velocity[Z]                                      0.19815E+02 
c  Pressure     0.10226E+00     300   0.34598E-01   0.97785E-01 0.96886E+00 
c  k            0.53445E+00      22   0.50893E-04   0.43421E-02 0.13975E+02 
c  epsilon      0.53607E+04      12   0.19795E-03   0.28074E+07 0.54094E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.7911e-06                             1
a  epsilon                 -4.1493                             2
a  Local Time Step      2.5254e-08                        281237


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3135          15.566          1.8357         0.30212
v  Velocity[Y]             -32.521          36.158          1.0893         0.73243
v  Velocity[Z]             -48.116          34.925        -0.97338      -0.0058707
v  ǁVelocityǁ             0.011531          51.097          6.2855          6.3025
v  Pressure                 -68381      2.3333e+05      1.4461e+05      1.2281e+05
v  k                    2.5835e-06          11.694        0.079023        0.075414
v  epsilon                0.016634      2.3263e+06          2863.1          53.793
v  TurbVisc             4.1756e-12         0.41838       0.0025353        0.037664
v  CourantNb               0.03176           39598          42.411          7.1943
v  FourierNb              0.022953      2.3655e+05          21.917         0.32472
v  total_pressure       4.3162e+05      7.3333e+05      6.4461e+05      6.2281e+05
v  Local Time Step           0.001        0.017356       0.0010014       0.0010111


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53289      2.3975e+05          64.328          7.5191


 TIME FOR THE TIME STEP              550:        0.67285E+02

===============================================================


 INSTANT    0.551000000E+01   TIME STEP NUMBER             551
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.292367494E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270995809E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68317E+02 0.68344E+01
   Friction velocity        uet   :  0.36121E-01 0.20005E+02
   Friction velocity        uk    :  0.42679E-01 0.20005E+02
   Dimensionless distance   yplus :  0.12011E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13530
   Nb of faces within the viscous sub-layer     :      10760
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13597E+02      54   0.90826E-01   0.40941E+02 0.30545E+02 
c  Velocity[X]                                      0.67162E+01 
c  Velocity[Y]                                      0.14513E+02 
c  Velocity[Z]                                      0.19711E+02 
c  Pressure     0.99193E-01     394   0.32876E-01   0.94614E-01 0.94856E+00 
c  k            0.53427E+00      23   0.10017E-03   0.47185E-02 0.14414E+02 
c  epsilon      0.53659E+04      12   0.24293E-03   0.24271E+07 0.50293E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -4.7515                             2
a  Local Time Step      2.5178e-08                        281222


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2806          16.978           1.835         0.30219
v  Velocity[Y]             -31.143          33.123          1.0924         0.73244
v  Velocity[Z]             -53.338          32.292        -0.97927      -0.0052011
v  ǁVelocityǁ            0.0017466          57.853          6.2907          6.3027
v  Pressure                 -68353      2.3341e+05      1.4461e+05      1.2282e+05
v  k                    2.2166e-07          11.604        0.079207         0.07543
v  epsilon               0.0086687      2.2973e+06          2865.9          53.846
v  TurbVisc              4.233e-12         0.41838       0.0025392        0.037666
v  CourantNb              0.012705           39717           42.46          7.1955
v  FourierNb              0.022944      2.3655e+05          21.917         0.32477
v  total_pressure       4.3165e+05      7.3341e+05      6.4461e+05      6.2282e+05
v  Local Time Step           0.001         0.01758       0.0010014       0.0010116


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.29908      2.3946e+05          64.377          7.5202


 TIME FOR THE TIME STEP              551:        0.69975E+02

===============================================================


 INSTANT    0.552000000E+01   TIME STEP NUMBER             552
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.701313172E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270907472E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74118E+02 0.79264E+01
   Friction velocity        uet   :  0.34509E-01 0.20306E+02
   Friction velocity        uk    :  0.40208E-01 0.20306E+02
   Dimensionless distance   yplus :  0.25910E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13533
   Nb of faces within the viscous sub-layer     :      10737
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13594E+02      48   0.90541E-01   0.39209E+02 0.29894E+02 
c  Velocity[X]                                      0.63942E+01 
c  Velocity[Y]                                      0.14735E+02 
c  Velocity[Z]                                      0.18079E+02 
c  Pressure     0.97374E-01     383   0.31718E-01   0.92761E-01 0.96503E+00 
c  k            0.53478E+00      21   0.10180E-03   0.55421E-02 0.15808E+02 
c  epsilon      0.53757E+04      12   0.26189E-03   0.56178E+07 0.76337E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.6447e-05                             1
a  epsilon                 -4.0497                             3
a  Local Time Step      2.5426e-08                        281220


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3311          15.306          1.8335         0.30246
v  Velocity[Y]             -31.042          33.181           1.094         0.73225
v  Velocity[Z]             -46.891          31.004        -0.98215      -0.0043705
v  ǁVelocityǁ             0.010049          50.645          6.2919          6.3025
v  Pressure                 -68228      2.3353e+05      1.4463e+05      1.2284e+05
v  k                    2.3758e-06          11.286        0.079322         0.07545
v  epsilon                0.017167      2.3351e+06          2875.9          53.893
v  TurbVisc             5.1542e-12         0.41838       0.0025432        0.037668
v  CourantNb             0.0026523           39330          42.533           7.196
v  FourierNb              0.022941      2.3655e+05          21.918         0.32483
v  total_pressure       4.3177e+05      7.3353e+05      6.4463e+05      6.2284e+05
v  Local Time Step           0.001        0.018791       0.0010014       0.0010114


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87772       2.384e+05          64.451          7.5208


 TIME FOR THE TIME STEP              552:        0.71273E+02

===============================================================


 INSTANT    0.553000000E+01   TIME STEP NUMBER             553
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.562285569E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270804824E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75040E+02 0.77749E+01
   Friction velocity        uet   :  0.33619E-01 0.23866E+02
   Friction velocity        uk    :  0.35914E-01 0.23866E+02
   Dimensionless distance   yplus :  0.17737E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13545
   Nb of faces within the viscous sub-layer     :      10714
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13587E+02      61   0.88743E-01   0.37605E+02 0.29268E+02 
c  Velocity[X]                                      0.60517E+01 
c  Velocity[Y]                                      0.13621E+02 
c  Velocity[Z]                                      0.17933E+02 
c  Pressure     0.94800E-01     596   0.31118E-01   0.90305E-01 0.11134E+01 
c  k            0.53562E+00      21   0.63882E-04   0.35300E-02 0.12566E+02 
c  epsilon      0.53801E+04      11   0.22990E-03   0.25005E+07 0.50976E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011785                             1
a  epsilon                 -4.5905                             4
a  Local Time Step      2.4851e-08                        281228


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3381          16.992          1.8343         0.30247
v  Velocity[Y]             -31.648          28.928          1.0923          0.7317
v  Velocity[Z]             -52.997          32.231        -0.98369      -0.0036922
v  ǁVelocityǁ             0.021566          57.488          6.2911          6.3024
v  Pressure                 -68050       2.336e+05      1.4471e+05      1.2293e+05
v  k                    2.6273e-06          11.431        0.079352         0.07548
v  epsilon                0.017381      2.3016e+06          2875.3          53.961
v  TurbVisc             3.9078e-12         0.41838       0.0025452         0.03767
v  CourantNb             0.0026833           40240           42.56          7.1956
v  FourierNb              0.022942      2.3655e+05          21.917         0.32482
v  total_pressure       4.3195e+05       7.336e+05      6.4471e+05      6.2293e+05
v  Local Time Step           0.001        0.016675       0.0010015       0.0010115


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75381      2.3804e+05          64.477          7.5204


 TIME FOR THE TIME STEP              553:        0.85267E+02

===============================================================


 INSTANT    0.554000000E+01   TIME STEP NUMBER             554
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.716159023E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270721438E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85384E+02 0.81323E+01
   Friction velocity        uet   :  0.33529E-01 0.20269E+02
   Friction velocity        uk    :  0.37547E-01 0.20269E+02
   Dimensionless distance   yplus :  0.11214E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13553
   Nb of faces within the viscous sub-layer     :      10718
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13585E+02      53   0.90059E-01   0.38114E+02 0.29494E+02 
c  Velocity[X]                                      0.60097E+01 
c  Velocity[Y]                                      0.12576E+02 
c  Velocity[Z]                                      0.19529E+02 
c  Pressure     0.95020E-01     538   0.30565E-01   0.90548E-01 0.10505E+01 
c  k            0.53583E+00      22   0.10599E-03   0.49299E-02 0.14896E+02 
c  epsilon      0.53879E+04      13   0.43266E-03   0.38359E+07 0.62983E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010026                             1
a  epsilon                 -3.9923                             4
a  Local Time Step      2.4559e-08                        281211


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3186          15.295          1.8342          0.3026
v  Velocity[Y]             -32.515          32.303          1.0911         0.73131
v  Velocity[Z]             -47.632          30.929        -0.98029      -0.0031885
v  ǁVelocityǁ            0.0070151          50.611          6.2878          6.3027
v  Pressure                 -67881      2.3369e+05      1.4478e+05        1.23e+05
v  k                      2.64e-06          11.231        0.079367        0.075497
v  epsilon                0.017546      2.3097e+06          2884.4          54.006
v  TurbVisc             4.3372e-12         0.41838       0.0025482        0.037672
v  CourantNb             0.0094745           40718          42.572          7.1955
v  FourierNb              0.022949      2.3655e+05          21.918         0.32489
v  total_pressure       4.3212e+05      7.3369e+05      6.4478e+05        6.23e+05
v  Local Time Step           0.001        0.018343       0.0010015       0.0010117


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.695      2.3883e+05           64.49          7.5204


 TIME FOR THE TIME STEP              554:        0.82928E+02

===============================================================


 INSTANT    0.555000000E+01   TIME STEP NUMBER             555
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.693957520E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270702940E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67834E+02 0.73908E+01
   Friction velocity        uet   :  0.34209E-01 0.19200E+02
   Friction velocity        uk    :  0.42386E-01 0.19200E+02
   Dimensionless distance   yplus :  0.14668E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13562
   Nb of faces within the viscous sub-layer     :      10705
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13589E+02      51   0.91164E-01   0.36483E+02 0.28847E+02 
c  Velocity[X]                                      0.58924E+01 
c  Velocity[Y]                                      0.12013E+02 
c  Velocity[Z]                                      0.18578E+02 
c  Pressure     0.94594E-01     567   0.30246E-01   0.90080E-01 0.10872E+01 
c  k            0.53590E+00      19   0.57599E-04   0.40884E-02 0.13467E+02 
c  epsilon      0.53841E+04      11   0.28750E-03   0.28555E+07 0.54481E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016456                             1
a  epsilon                 -4.2344                             5
a  Local Time Step      2.4472e-08                        281206


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3155          17.237          1.8342         0.30245
v  Velocity[Y]             -32.303          28.868          1.0883         0.73105
v  Velocity[Z]             -54.591           32.25         -0.9752      -0.0030841
v  ǁVelocityǁ             0.023776           59.15          6.2808          6.3028
v  Pressure                 -67857       2.338e+05      1.4485e+05      1.2308e+05
v  k                    2.7006e-06          11.268        0.079286        0.075506
v  epsilon                0.017565      2.2719e+06          2878.6          53.996
v  TurbVisc             4.3037e-12         0.41838       0.0025505        0.037673
v  CourantNb              0.018329           40864          42.545          7.1953
v  FourierNb               0.02296      2.3655e+05          21.916          0.3248
v  total_pressure       4.3214e+05       7.338e+05      6.4485e+05      6.2308e+05
v  Local Time Step           0.001        0.017189       0.0010015       0.0010116


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.655      2.3845e+05          64.461          7.5201


 TIME FOR THE TIME STEP              555:        0.81692E+02

===============================================================


 INSTANT    0.556000000E+01   TIME STEP NUMBER             556
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.220723793E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270692125E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76636E+02 0.77894E+01
   Friction velocity        uet   :  0.34110E-01 0.24456E+02
   Friction velocity        uk    :  0.45216E-01 0.24456E+02
   Dimensionless distance   yplus :  0.31205E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13555
   Nb of faces within the viscous sub-layer     :      10702
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13588E+02      49   0.88777E-01   0.34432E+02 0.27994E+02 
c  Velocity[X]                                      0.55290E+01 
c  Velocity[Y]                                      0.11959E+02 
c  Velocity[Z]                                      0.16945E+02 
c  Pressure     0.91889E-01     567   0.29016E-01   0.87497E-01 0.10855E+01 
c  k            0.53549E+00      22   0.98110E-04   0.49326E-02 0.14878E+02 
c  epsilon      0.53819E+04      12   0.23908E-03   0.37809E+07 0.62608E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019359                             1
a  epsilon                 -1.1897                             3
a  Local Time Step      2.3854e-08                        281182


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.283          15.187          1.8353         0.30206
v  Velocity[Y]              -33.63          32.039          1.0844           0.731
v  Velocity[Z]             -48.067          31.361         -0.9679      -0.0035385
v  ǁVelocityǁ            0.0058972          50.785          6.2728          6.3037
v  Pressure                 -67671      2.3385e+05       1.449e+05      1.2316e+05
v  k                    2.5197e-06          11.022        0.079283        0.075511
v  epsilon                0.017356      2.3158e+06          2882.2          53.975
v  TurbVisc             4.4048e-12         0.41838       0.0025509        0.037674
v  CourantNb              0.014416           41922          42.473          7.1933
v  FourierNb              0.022973      2.3655e+05          21.917         0.32486
v  total_pressure       4.3233e+05      7.3385e+05       6.449e+05      6.2316e+05
v  Local Time Step           0.001        0.016765       0.0010015       0.0010116


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74064      2.3794e+05          64.391          7.5182


 TIME FOR THE TIME STEP              556:        0.74434E+02

===============================================================


 INSTANT    0.557000000E+01   TIME STEP NUMBER             557
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.351605994E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270707142E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.78135E+02 0.76623E+01
   Friction velocity        uet   :  0.23399E-01 0.24384E+02
   Friction velocity        uk    :  0.23235E-01 0.24384E+02
   Dimensionless distance   yplus :  0.28026E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13556
   Nb of faces within the viscous sub-layer     :      10716
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13589E+02      47   0.90277E-01   0.33801E+02 0.27738E+02 
c  Velocity[X]                                      0.55490E+01 
c  Velocity[Y]                                      0.11722E+02 
c  Velocity[Z]                                      0.16530E+02 
c  Pressure     0.87842E-01     477   0.27941E-01   0.83806E-01 0.10191E+01 
c  k            0.53629E+00      19   0.90527E-04   0.43913E-02 0.13973E+02 
c  epsilon      0.53662E+04      12   0.20422E-03   0.22087E+07 0.47989E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015185                             1
a  epsilon                 -4.6164                             5
a  Local Time Step      2.3969e-08                        281229


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -7.27          17.478          1.8366         0.30189
v  Velocity[Y]             -29.511          31.745          1.0779         0.73094
v  Velocity[Z]             -55.432          32.131        -0.95864      -0.0042937
v  ǁVelocityǁ             0.018936           59.99          6.2629          6.3047
v  Pressure                 -67450      2.3383e+05      1.4492e+05      1.2324e+05
v  k                    2.6006e-06          10.948        0.079159        0.075526
v  epsilon                0.016938      2.2739e+06          2873.2           53.98
v  TurbVisc             4.0994e-12         0.41838        0.002552        0.037675
v  CourantNb             0.0016669           41721          42.366          7.1928
v  FourierNb              0.022985      2.3655e+05          21.918         0.32494
v  total_pressure       4.3255e+05      7.3383e+05      6.4492e+05      6.2324e+05
v  Local Time Step           0.001        0.017424       0.0010015       0.0010115


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61786      2.3885e+05          64.284          7.5177


 TIME FOR THE TIME STEP              557:        0.73082E+02

===============================================================


 INSTANT    0.558000000E+01   TIME STEP NUMBER             558
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.436501795E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270801666E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80093E+02 0.86759E+01
   Friction velocity        uet   :  0.36086E-01 0.22125E+02
   Friction velocity        uk    :  0.36433E-01 0.22125E+02
   Dimensionless distance   yplus :  0.19312E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13553
   Nb of faces within the viscous sub-layer     :      10748
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13595E+02      51   0.90979E-01   0.34785E+02 0.28160E+02 
c  Velocity[X]                                      0.56180E+01 
c  Velocity[Y]                                      0.11358E+02 
c  Velocity[Z]                                      0.17809E+02 
c  Pressure     0.86689E-01     386   0.27394E-01   0.82636E-01 0.87654E+00 
c  k            0.53726E+00      18   0.62805E-04   0.36820E-02 0.12861E+02 
c  epsilon      0.53452E+04      12   0.20953E-03   0.42871E+07 0.67088E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0023758                             2
a  epsilon                 -3.2533                             6
a  Local Time Step      2.4105e-08                        281223


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2508          15.378          1.8374          0.3021
v  Velocity[Y]             -29.749          32.054          1.0733         0.73119
v  Velocity[Z]             -46.389          32.822        -0.95013      -0.0052924
v  ǁVelocityǁ             0.014407          49.384          6.2542          6.3059
v  Pressure                 -67239      2.3382e+05      1.4491e+05      1.2327e+05
v  k                    2.5693e-06          10.989        0.078991        0.075538
v  epsilon                0.016509      2.3249e+06          2856.2          53.969
v  TurbVisc             4.2692e-12         0.41838       0.0025541        0.037676
v  CourantNb               0.05351           41486           42.27          7.1927
v  FourierNb              0.022998      2.3655e+05          21.919          0.3249
v  total_pressure       4.3276e+05      7.3382e+05      6.4491e+05      6.2327e+05
v  Local Time Step           0.001        0.016782       0.0010015       0.0010111


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68322      2.3966e+05          64.189          7.5176


 TIME FOR THE TIME STEP              558:        0.72000E+02

===============================================================


 INSTANT    0.559000000E+01   TIME STEP NUMBER             559
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.241057292E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270919342E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64255E+02 0.78114E+01
   Friction velocity        uet   :  0.35077E-01 0.20454E+02
   Friction velocity        uk    :  0.40244E-01 0.20454E+02
   Dimensionless distance   yplus :  0.17059E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13578
   Nb of faces within the viscous sub-layer     :      10746
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13592E+02      57   0.89680E-01   0.34812E+02 0.28132E+02 
c  Velocity[X]                                      0.53940E+01 
c  Velocity[Y]                                      0.11501E+02 
c  Velocity[Z]                                      0.17917E+02 
c  Pressure     0.86292E-01     386   0.27340E-01   0.82243E-01 0.93230E+00 
c  k            0.53707E+00      18   0.72200E-04   0.35026E-02 0.12526E+02 
c  epsilon      0.53348E+04      12   0.18162E-03   0.18166E+07 0.43726E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018653                             1
a  epsilon                 -4.8109                             5
a  Local Time Step      2.3486e-08                        281226


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2432          17.388          1.8383         0.30225
v  Velocity[Y]             -31.924          32.306          1.0677         0.73145
v  Velocity[Z]             -55.666          32.282        -0.94106      -0.0064578
v  ǁVelocityǁ            0.0084657          60.228          6.2447          6.3068
v  Pressure                 -67016      2.3375e+05      1.4489e+05      1.2331e+05
v  k                     2.527e-06          10.766        0.078898        0.075535
v  epsilon                0.016542      2.2959e+06          2851.2          53.938
v  TurbVisc             4.1765e-12         0.41838       0.0025578        0.037676
v  CourantNb              0.013598           42578          42.182          7.1928
v  FourierNb              0.023008      2.3655e+05          21.921         0.32492
v  total_pressure       4.3298e+05      7.3375e+05      6.4489e+05      6.2331e+05
v  Local Time Step           0.001        0.016472       0.0010015       0.0010114


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.758      2.4085e+05          64.103          7.5178


 TIME FOR THE TIME STEP              559:        0.76442E+02

===============================================================


 INSTANT    0.560000000E+01   TIME STEP NUMBER             560
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.755709347E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271060809E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88395E+02 0.74880E+01
   Friction velocity        uet   :  0.34587E-01 0.14522E+02
   Friction velocity        uk    :  0.35123E-01 0.14522E+02
   Dimensionless distance   yplus :  0.17962E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13555
   Nb of faces within the viscous sub-layer     :      10764
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13600E+02      57   0.87372E-01   0.33675E+02 0.27693E+02 
c  Velocity[X]                                      0.54518E+01 
c  Velocity[Y]                                      0.11253E+02 
c  Velocity[Z]                                      0.16971E+02 
c  Pressure     0.84621E-01     396   0.26947E-01   0.80718E-01 0.87798E+00 
c  k            0.53569E+00      21   0.93215E-04   0.36517E-02 0.12809E+02 
c  epsilon      0.53227E+04      11   0.21202E-03   0.25551E+07 0.51974E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00059545                             2
a  epsilon                 -3.6814                             6
a  Local Time Step      2.3317e-08                        281227


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2522          15.242          1.8393         0.30217
v  Velocity[Y]             -36.829          32.597          1.0621         0.73176
v  Velocity[Z]             -44.361          36.622        -0.93339        -0.00767
v  ǁVelocityǁ             0.016761          48.382          6.2393          6.3088
v  Pressure                 -66792      2.3362e+05      1.4485e+05      1.2334e+05
v  k                    2.5071e-06          11.036        0.078698        0.075514
v  epsilon                0.017032      2.3294e+06          2841.3          53.826
v  TurbVisc             4.1689e-12         0.41838       0.0025592        0.037676
v  CourantNb              0.025688           42887          42.069          7.1933
v  FourierNb              0.023015      2.3655e+05          21.922         0.32499
v  total_pressure       4.3321e+05      7.3362e+05      6.4485e+05      6.2334e+05
v  Local Time Step           0.001        0.016591       0.0010015       0.0010114


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75752      2.3847e+05          63.991          7.5182


 TIME FOR THE TIME STEP              560:        0.76990E+02

===============================================================


 INSTANT    0.561000000E+01   TIME STEP NUMBER             561
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.385227413E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271252462E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64599E+02 0.75189E+01
   Friction velocity        uet   :  0.31164E-01 0.19605E+02
   Friction velocity        uk    :  0.31284E-01 0.19605E+02
   Dimensionless distance   yplus :  0.15712E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13582
   Nb of faces within the viscous sub-layer     :      10764
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13606E+02      53   0.89946E-01   0.32670E+02 0.27261E+02 
c  Velocity[X]                                      0.52956E+01 
c  Velocity[Y]                                      0.11223E+02 
c  Velocity[Z]                                      0.16152E+02 
c  Pressure     0.84259E-01    1119   0.26992E-01   0.80242E-01 0.60427E+01 
c  k            0.53601E+00      18   0.45847E-04   0.27632E-02 0.11137E+02 
c  epsilon      0.53000E+04      12   0.23553E-03   0.56565E+07 0.77564E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -8.351e-05                             1
a  epsilon                 -3.8103                             5
a  Local Time Step      2.3243e-08                        281217


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2205          17.797            1.84         0.30198
v  Velocity[Y]             -33.661          29.623          1.0539         0.73202
v  Velocity[Z]             -53.633           32.23        -0.92537      -0.0063017
v  ǁVelocityǁ             0.010232          58.093          6.2324          6.3082
v  Pressure                 -67578      2.3237e+05      1.4366e+05      1.2244e+05
v  k                     2.474e-06          11.483        0.078516        0.075504
v  epsilon                0.017742        2.27e+06          2824.8          53.828
v  TurbVisc             4.1557e-12         0.41838       0.0025568        0.037676
v  CourantNb                     0           43023          42.009          7.1955
v  FourierNb               0.02302      2.3655e+05          21.923         0.32481
v  total_pressure       4.3242e+05      7.3237e+05      6.4366e+05      6.2244e+05
v  Local Time Step           0.001           0.014       0.0010015       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85826      2.4004e+05          63.932          7.5203


 TIME FOR THE TIME STEP              561:        0.11519E+03

===============================================================


 INSTANT    0.562000000E+01   TIME STEP NUMBER             562
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.333028826E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271063533E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84254E+02 0.83468E+01
   Friction velocity        uet   :  0.33526E-01 0.20567E+02
   Friction velocity        uk    :  0.36123E-01 0.20567E+02
   Dimensionless distance   yplus :  0.11023E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13569
   Nb of faces within the viscous sub-layer     :      10780
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13594E+02      49   0.89926E-01   0.33098E+02 0.27462E+02 
c  Velocity[X]                                      0.51958E+01 
c  Velocity[Y]                                      0.10987E+02 
c  Velocity[Z]                                      0.16915E+02 
c  Pressure     0.82710E-01     404   0.26230E-01   0.78654E-01 0.10138E+01 
c  k            0.53670E+00      17   0.91772E-04   0.45680E-02 0.14321E+02 
c  epsilon      0.53053E+04      13   0.47936E-03   0.20387E+08 0.14645E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.6422e-05                             1
a  epsilon                 -3.2089                             5
a  Local Time Step      2.2862e-08                        281190


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2108          15.048          1.8427         0.30192
v  Velocity[Y]             -32.491          32.687          1.0477         0.73229
v  Velocity[Z]             -43.356            37.3        -0.92095      -0.0057755
v  ǁVelocityǁ            0.0089114          46.227          6.2305          6.3085
v  Pressure                 -67403      2.3221e+05      1.4363e+05      1.2246e+05
v  k                    3.1489e-06          11.364        0.078338        0.075484
v  epsilon                0.018321      2.3261e+06            2827          53.729
v  TurbVisc             4.0535e-12         0.41838       0.0025512        0.037675
v  CourantNb             0.0081732           43741           41.92          7.1944
v  FourierNb              0.023024      2.3655e+05          21.921         0.32484
v  total_pressure        4.326e+05      7.3221e+05      6.4363e+05      6.2246e+05
v  Local Time Step           0.001          0.0154       0.0010015       0.0010112


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60119      2.3947e+05          63.841          7.5192


 TIME FOR THE TIME STEP              562:        0.77538E+02

===============================================================


 INSTANT    0.563000000E+01   TIME STEP NUMBER             563
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.296486892E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271159430E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58653E+02 0.80897E+01
   Friction velocity        uet   :  0.19853E-01 0.15482E+02
   Friction velocity        uk    :  0.19807E-01 0.15482E+02
   Dimensionless distance   yplus :  0.17735E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13563
   Nb of faces within the viscous sub-layer     :      10775
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13587E+02      59   0.89504E-01   0.32885E+02 0.27373E+02 
c  Velocity[X]                                      0.53817E+01 
c  Velocity[Y]                                      0.10868E+02 
c  Velocity[Z]                                      0.16635E+02 
c  Pressure     0.82461E-01     393   0.26298E-01   0.78410E-01 0.86126E+00 
c  k            0.53763E+00      20   0.10544E-03   0.40580E-02 0.13378E+02 
c  epsilon      0.52927E+04      11   0.32542E-03   0.12832E+08 0.11746E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -3.3214                             5
a  Local Time Step      2.3155e-08                        281217


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1462          18.607          1.8439         0.30178
v  Velocity[Y]             -33.373          30.171          1.0417         0.73262
v  Velocity[Z]             -54.193          32.177        -0.91877      -0.0057528
v  ǁVelocityǁ             0.007594          59.541          6.2292          6.3079
v  Pressure                 -68317       2.321e+05      1.4361e+05      1.2247e+05
v  k                    2.3409e-06          11.428        0.078055        0.075473
v  epsilon                0.019178      2.2644e+06            2795          53.719
v  TurbVisc             5.1521e-12         0.41838       0.0025425        0.037673
v  CourantNb             0.0053369           43187          41.871          7.1962
v  FourierNb              0.023024      2.3655e+05          21.917         0.32478
v  total_pressure       4.3168e+05       7.321e+05      6.4361e+05      6.2247e+05
v  Local Time Step           0.001         0.01694       0.0010015       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66466      2.3738e+05          63.788          7.5209


 TIME FOR THE TIME STEP              563:        0.66745E+02

===============================================================


 INSTANT    0.564000000E+01   TIME STEP NUMBER             564
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.283415412E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271132611E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87090E+02 0.83385E+01
   Friction velocity        uet   :  0.28475E-01 0.17818E+02
   Friction velocity        uk    :  0.29172E-01 0.17818E+02
   Dimensionless distance   yplus :  0.22735E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13550
   Nb of faces within the viscous sub-layer     :      10788
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13586E+02      53   0.88732E-01   0.33009E+02 0.27428E+02 
c  Velocity[X]                                      0.52818E+01 
c  Velocity[Y]                                      0.11412E+02 
c  Velocity[Z]                                      0.16314E+02 
c  Pressure     0.81335E-01     581   0.25897E-01   0.77376E-01 0.90141E+00 
c  k            0.53722E+00      20   0.54004E-04   0.30928E-02 0.11780E+02 
c  epsilon      0.52826E+04      11   0.22815E-03   0.55488E+07 0.77440E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -3.5325                             5
a  Local Time Step      2.2944e-08                        281243


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0388          15.118           1.844         0.30167
v  Velocity[Y]             -32.239          35.276          1.0366         0.73303
v  Velocity[Z]             -41.519          34.279        -0.91931      -0.0057172
v  ǁVelocityǁ             0.011495          44.402          6.2296           6.308
v  Pressure                 -69443      2.3211e+05      1.4356e+05      1.2245e+05
v  k                    1.8123e-06          11.334         0.07793        0.075452
v  epsilon                0.020193      2.2869e+06          2780.5          53.647
v  TurbVisc             3.7888e-12         0.41838       0.0025337        0.037672
v  CourantNb              0.021742           43585          41.842          7.1957
v  FourierNb              0.023026      2.3655e+05          21.912         0.32482
v  total_pressure       4.3056e+05      7.3211e+05      6.4356e+05      6.2245e+05
v  Local Time Step           0.001         0.01401       0.0010014       0.0010109


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68994      2.3876e+05          63.754          7.5205


 TIME FOR THE TIME STEP              564:        0.90946E+02

===============================================================


 INSTANT    0.565000000E+01   TIME STEP NUMBER             565
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.514334176E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271114760E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60535E+02 0.78756E+01
   Friction velocity        uet   :  0.32862E-01 0.16229E+02
   Friction velocity        uk    :  0.32805E-01 0.16229E+02
   Dimensionless distance   yplus :  0.14695E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13536
   Nb of faces within the viscous sub-layer     :      10787
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13579E+02      61   0.89280E-01   0.34572E+02 0.28017E+02 
c  Velocity[X]                                      0.53922E+01 
c  Velocity[Y]                                      0.11981E+02 
c  Velocity[Z]                                      0.17198E+02 
c  Pressure     0.82829E-01     529   0.26266E-01   0.78641E-01 0.10569E+01 
c  k            0.53705E+00      20   0.45674E-04   0.32647E-02 0.12047E+02 
c  epsilon      0.52778E+04      10   0.19525E-03   0.39946E+07 0.65806E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -2.4143                             6
a  Local Time Step      2.3593e-08                        281244


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1554          19.938           1.844         0.30154
v  Velocity[Y]             -29.321          30.809          1.0317         0.73352
v  Velocity[Z]             -57.827           32.14        -0.92107       -0.005619
v  ǁVelocityǁ            0.0058601          63.761          6.2318           6.308
v  Pressure                 -70722      2.3216e+05      1.4354e+05      1.2242e+05
v  k                    2.4532e-06          11.382        0.077818        0.075433
v  epsilon                0.021079      2.2834e+06          2768.9           53.62
v  TurbVisc             4.1637e-12         0.41838       0.0025284        0.037671
v  CourantNb              0.042156           42386          41.842          7.1969
v  FourierNb              0.023025      2.3655e+05          21.912         0.32474
v  total_pressure       4.2928e+05      7.3216e+05      6.4354e+05      6.2242e+05
v  Local Time Step           0.001        0.014542       0.0010014       0.0010112


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82354       2.385e+05          63.754          7.5217


 TIME FOR THE TIME STEP              565:        0.89131E+02

===============================================================


 INSTANT    0.566000000E+01   TIME STEP NUMBER             566
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.181706057E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271046500E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.90708E+02 0.82227E+01
   Friction velocity        uet   :  0.27174E-01 0.23912E+02
   Friction velocity        uk    :  0.28446E-01 0.23912E+02
   Dimensionless distance   yplus :  0.18537E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13537
   Nb of faces within the viscous sub-layer     :      10801
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13574E+02      54   0.88753E-01   0.36187E+02 0.28702E+02 
c  Velocity[X]                                      0.54460E+01 
c  Velocity[Y]                                      0.12134E+02 
c  Velocity[Z]                                      0.18607E+02 
c  Pressure     0.83673E-01     521   0.26615E-01   0.79451E-01 0.10712E+01 
c  k            0.53681E+00      19   0.38941E-04   0.29232E-02 0.11422E+02 
c  epsilon      0.52827E+04      10   0.36934E-03   0.45989E+07 0.70443E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -3.0061                             6
a  Local Time Step       2.386e-08                        281241


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1126          15.175          1.8422         0.30131
v  Velocity[Y]             -30.767          36.651          1.0297         0.73417
v  Velocity[Z]             -44.964          40.662         -0.9253      -0.0053662
v  ǁVelocityǁ             0.010928          47.812          6.2344          6.3079
v  Pressure                 -71536      2.3221e+05      1.4354e+05      1.2243e+05
v  k                    2.4611e-06          11.534          0.0779        0.075422
v  epsilon                0.021662       2.321e+06          2781.6          53.592
v  TurbVisc             4.0227e-12         0.41838       0.0025266        0.037669
v  CourantNb             0.0058986           41911          41.885          7.1978
v  FourierNb              0.023024      2.3655e+05          21.911         0.32478
v  total_pressure       4.2846e+05      7.3221e+05      6.4354e+05      6.2243e+05
v  Local Time Step           0.001        0.015996       0.0010014       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51571       2.413e+05          63.797          7.5226


 TIME FOR THE TIME STEP              566:        0.79903E+02

===============================================================


 INSTANT    0.567000000E+01   TIME STEP NUMBER             567
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.919711313E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271031514E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60671E+02 0.79999E+01
   Friction velocity        uet   :  0.27168E-01 0.21335E+02
   Friction velocity        uk    :  0.28128E-01 0.21335E+02
   Dimensionless distance   yplus :  0.27224E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13524
   Nb of faces within the viscous sub-layer     :      10807
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13572E+02      58   0.91798E-01   0.35609E+02 0.28434E+02 
c  Velocity[X]                                      0.55282E+01 
c  Velocity[Y]                                      0.12310E+02 
c  Velocity[Z]                                      0.17770E+02 
c  Pressure     0.84402E-01     504   0.27131E-01   0.80145E-01 0.12119E+01 
c  k            0.53700E+00      19   0.39495E-04   0.25718E-02 0.10700E+02 
c  epsilon      0.52797E+04      10   0.25058E-03   0.33217E+07 0.59971E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00025859                             1
a  epsilon                   -3.52                             6
a  Local Time Step      2.3511e-08                        281258


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1082          19.344          1.8415         0.30098
v  Velocity[Y]             -31.611          34.239          1.0279         0.73437
v  Velocity[Z]             -56.011          32.175        -0.93248      -0.0050893
v  ǁVelocityǁ             0.010011          61.791          6.2378          6.3078
v  Pressure                 -72007       2.323e+05      1.4356e+05       1.224e+05
v  k                    2.4442e-06          11.247        0.077911        0.075422
v  epsilon                0.021973      2.2525e+06          2774.8          53.612
v  TurbVisc             4.0795e-12         0.41838       0.0025278        0.037669
v  CourantNb              0.040791           42533          41.903          7.1984
v  FourierNb              0.023021      2.3655e+05          21.911         0.32479
v  total_pressure       4.2799e+05       7.323e+05      6.4356e+05       6.224e+05
v  Local Time Step           0.001        0.017183       0.0010014       0.0010114


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52016      2.4104e+05          63.815          7.5232


 TIME FOR THE TIME STEP              567:        0.91871E+02

===============================================================


 INSTANT    0.568000000E+01   TIME STEP NUMBER             568
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.506589953E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270958095E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84776E+02 0.83424E+01
   Friction velocity        uet   :  0.15375E-01 0.17607E+02
   Friction velocity        uk    :  0.18985E-01 0.17607E+02
   Dimensionless distance   yplus :  0.17112E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13498
   Nb of faces within the viscous sub-layer     :      10795
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13566E+02      59   0.91034E-01   0.35545E+02 0.28442E+02 
c  Velocity[X]                                      0.56347E+01 
c  Velocity[Y]                                      0.12851E+02 
c  Velocity[Z]                                      0.17059E+02 
c  Pressure     0.83366E-01     501   0.27251E-01   0.79039E-01 0.12308E+01 
c  k            0.53689E+00      18   0.47892E-04   0.32231E-02 0.11939E+02 
c  epsilon      0.53052E+04      14   0.27973E-03   0.48856E+07 0.72301E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -2.2912                             5
a  Local Time Step      2.3861e-08                        281260


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0718          15.153          1.8413         0.30086
v  Velocity[Y]             -33.052          37.329          1.0313         0.73453
v  Velocity[Z]             -40.954          31.698        -0.93874      -0.0046516
v  ǁVelocityǁ            0.0098872          43.812          6.2418          6.3078
v  Pressure                 -72548      2.3241e+05      1.4361e+05      1.2238e+05
v  k                    2.5059e-06          11.311        0.078151        0.075435
v  epsilon                0.021996       2.308e+06          2801.8          53.642
v  TurbVisc              4.042e-12         0.41838        0.002531        0.037669
v  CourantNb              0.008582           41909          41.943          7.1997
v  FourierNb              0.023018      2.3655e+05          21.912         0.32483
v  total_pressure       4.2745e+05      7.3241e+05      6.4361e+05      6.2238e+05
v  Local Time Step           0.001        0.016383       0.0010014       0.0010111


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.3288      2.3988e+05          63.855          7.5245


 TIME FOR THE TIME STEP              568:        0.78827E+02

===============================================================


 INSTANT    0.569000000E+01   TIME STEP NUMBER             569
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.907642621E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270843910E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59161E+02 0.79767E+01
   Friction velocity        uet   :  0.43296E-02 0.23021E+02
   Friction velocity        uk    :  0.11898E-01 0.23021E+02
   Dimensionless distance   yplus :  0.21711E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13468
   Nb of faces within the viscous sub-layer     :      10811
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13564E+02      57   0.90818E-01   0.36473E+02 0.28815E+02 
c  Velocity[X]                                      0.58003E+01 
c  Velocity[Y]                                      0.13363E+02 
c  Velocity[Z]                                      0.17310E+02 
c  Pressure     0.86278E-01     493   0.28326E-01   0.81691E-01 0.12044E+01 
c  k            0.53729E+00      22   0.42313E-04   0.29571E-02 0.11420E+02 
c  epsilon      0.53194E+04      11   0.58366E-03   0.56255E+07 0.77480E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018834                             1
a  epsilon                 -3.2432                             6
a  Local Time Step      2.3987e-08                        281273


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.0886          18.666          1.8414         0.30104
v  Velocity[Y]              -29.14          33.584          1.0334         0.73452
v  Velocity[Z]             -54.562          32.231        -0.94503      -0.0041284
v  ǁVelocityǁ            0.0094275           60.02          6.2458          6.3072
v  Pressure                 -72650       2.325e+05      1.4366e+05      1.2238e+05
v  k                     2.459e-06          11.295         0.07817        0.075452
v  epsilon                0.021822      2.2666e+06          2806.6          53.663
v  TurbVisc             4.1373e-12         0.41838       0.0025349        0.037669
v  CourantNb             0.0046925           41690          42.017          7.2003
v  FourierNb              0.023014      2.3655e+05          21.913         0.32466
v  total_pressure       4.2735e+05       7.325e+05      6.4366e+05      6.2238e+05
v  Local Time Step           0.001        0.018021       0.0010014       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.33331      2.4234e+05          63.929           7.525


 TIME FOR THE TIME STEP              569:        0.79865E+02

===============================================================


 INSTANT    0.570000000E+01   TIME STEP NUMBER             570
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.357112564E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270724041E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.82272E+02 0.86403E+01
   Friction velocity        uet   :  0.25522E-01 0.18760E+02
   Friction velocity        uk    :  0.26719E-01 0.18760E+02
   Dimensionless distance   yplus :  0.19052E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13448
   Nb of faces within the viscous sub-layer     :      10798
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13557E+02      51   0.91426E-01   0.37850E+02 0.29353E+02 
c  Velocity[X]                                      0.57558E+01 
c  Velocity[Y]                                      0.14462E+02 
c  Velocity[Z]                                      0.17632E+02 
c  Pressure     0.88296E-01     746   0.29456E-01   0.83661E-01 0.43091E+01 
c  k            0.53782E+00      20   0.10572E-03   0.42894E-02 0.13605E+02 
c  epsilon      0.53537E+04      12   0.32371E-03   0.55757E+07 0.76598E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -7.438e-05                             1
a  epsilon                 -3.3422                             6
a  Local Time Step      2.3486e-08                        281260


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1942          15.172          1.8425         0.30148
v  Velocity[Y]             -33.943          37.486          1.0356         0.73464
v  Velocity[Z]             -42.417          32.074        -0.95137      -0.0049366
v  ǁVelocityǁ             0.011577          45.251          6.2519          6.3084
v  Pressure                 -71103      2.3334e+05      1.4448e+05        1.23e+05
v  k                    2.5297e-06          11.179        0.078507        0.075482
v  epsilon                0.021555      2.3278e+06          2841.4          53.743
v  TurbVisc             4.1033e-12         0.41838       0.0025392        0.037671
v  CourantNb             0.0018761           42579          42.084          7.2001
v  FourierNb               0.02301      2.3655e+05          21.912         0.32486
v  total_pressure        4.289e+05      7.3334e+05      6.4448e+05        6.23e+05
v  Local Time Step           0.001         0.01592       0.0010014       0.0010112


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62213      2.4236e+05          63.996           7.525


 TIME FOR THE TIME STEP              570:        0.81195E+02

===============================================================


 INSTANT    0.571000000E+01   TIME STEP NUMBER             571
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.293386392E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270791340E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57444E+02 0.83878E+01
   Friction velocity        uet   :  0.28722E-01 0.19053E+02
   Friction velocity        uk    :  0.29312E-01 0.19053E+02
   Dimensionless distance   yplus :  0.12720E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13464
   Nb of faces within the viscous sub-layer     :      10787
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13559E+02      61   0.89161E-01   0.39451E+02 0.29982E+02 
c  Velocity[X]                                      0.59524E+01 
c  Velocity[Y]                                      0.15269E+02 
c  Velocity[Z]                                      0.18230E+02 
c  Pressure     0.92462E-01     401   0.31008E-01   0.87732E-01 0.12052E+01 
c  k            0.53757E+00      17   0.49319E-04   0.38904E-02 0.13143E+02 
c  epsilon      0.53721E+04      12   0.29544E-03   0.60344E+07 0.79531E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.9788e-05                             1
a  epsilon                 -3.0394                             7
a  Local Time Step      2.3958e-08                        281265


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.1471          18.578          1.8432         0.30175
v  Velocity[Y]             -29.773          31.503          1.0316         0.73385
v  Velocity[Z]             -54.083          31.855        -0.95539      -0.0050792
v  ǁVelocityǁ            0.0099721          59.448           6.254           6.309
v  Pressure                 -68977       2.334e+05      1.4453e+05      1.2297e+05
v  k                    2.5678e-06          11.162        0.078629        0.075512
v  epsilon                0.021277      2.2818e+06          2849.2           53.83
v  TurbVisc             4.1717e-12         0.41838       0.0025436        0.037673
v  CourantNb              0.012762           41739          42.161          7.2016
v  FourierNb              0.023005      2.3655e+05          21.914         0.32486
v  total_pressure       4.3102e+05       7.334e+05      6.4453e+05      6.2297e+05
v  Local Time Step           0.001        0.017512       0.0010014       0.0010112


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67295      2.4009e+05          64.076          7.5265


 TIME FOR THE TIME STEP              571:        0.73596E+02

===============================================================


 INSTANT    0.572000000E+01   TIME STEP NUMBER             572
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.264833882E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270795927E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80460E+02 0.83555E+01
   Friction velocity        uet   :  0.28537E-01 0.18495E+02
   Friction velocity        uk    :  0.29191E-01 0.18495E+02
   Dimensionless distance   yplus :  0.21868E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13452
   Nb of faces within the viscous sub-layer     :      10771
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13564E+02      66   0.89112E-01   0.40207E+02 0.30218E+02 
c  Velocity[X]                                      0.64169E+01 
c  Velocity[Y]                                      0.16135E+02 
c  Velocity[Z]                                      0.17655E+02 
c  Pressure     0.95846E-01     404   0.32542E-01   0.90993E-01 0.12018E+01 
c  k            0.53837E+00      21   0.13367E-03   0.64079E-02 0.16258E+02 
c  epsilon      0.54203E+04      13   0.37989E-03   0.13251E+08 0.11649E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.2995e-05                             1
a  epsilon                -0.84521                             3
a  Local Time Step      2.3921e-08                        281246


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2307          15.373          1.8427         0.30188
v  Velocity[Y]             -32.795          38.915          1.0282         0.73343
v  Velocity[Z]             -42.606           32.61        -0.95675      -0.0044195
v  ǁVelocityǁ             0.013548          46.473          6.2524          6.3102
v  Pressure                 -66713      2.3344e+05      1.4458e+05      1.2294e+05
v  k                    2.5043e-06          10.806        0.079029        0.075563
v  epsilon                0.021064      2.3053e+06          2907.3          53.968
v  TurbVisc             4.2814e-12         0.41838       0.0025476        0.037675
v  CourantNb            0.00087193           41804          42.228          7.2023
v  FourierNb              0.023001      2.3655e+05          21.913         0.32492
v  total_pressure       4.3329e+05      7.3344e+05      6.4458e+05      6.2294e+05
v  Local Time Step           0.001        0.018659       0.0010014       0.0010112


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68442      2.4225e+05          64.142          7.5272


 TIME FOR THE TIME STEP              572:        0.78166E+02

===============================================================


 INSTANT    0.573000000E+01   TIME STEP NUMBER             573
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.231316721E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270759672E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63539E+02 0.88324E+01
   Friction velocity        uet   :  0.33740E-01 0.20887E+02
   Friction velocity        uk    :  0.39930E-01 0.20887E+02
   Dimensionless distance   yplus :  0.26442E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13450
   Nb of faces within the viscous sub-layer     :      10770
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13565E+02      63   0.91829E-01   0.41727E+02 0.30817E+02 
c  Velocity[X]                                      0.67541E+01 
c  Velocity[Y]                                      0.17371E+02 
c  Velocity[Z]                                      0.17602E+02 
c  Pressure     0.10178E+00     402   0.34654E-01   0.96618E-01 0.12836E+01 
c  k            0.54013E+00      21   0.24792E-03   0.92425E-02 0.18504E+02 
c  epsilon      0.54774E+04      14   0.11825E-02   0.41815E+08 0.20286E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -4.732e-05                             1
a  epsilon                 -2.0394                             4
a  Local Time Step      2.4214e-08                        281259


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2847          18.529          1.8394         0.30213
v  Velocity[Y]             -30.563           32.16          1.0224         0.73313
v  Velocity[Z]             -53.651          31.975        -0.95431      -0.0032265
v  ǁVelocityǁ            0.0065334              59          6.2445          6.3102
v  Pressure                 -67392      2.3349e+05      1.4464e+05      1.2289e+05
v  k                    2.5571e-06          10.794        0.079284        0.075618
v  epsilon                0.020831      4.2133e+06            2947          54.085
v  TurbVisc             4.1479e-12         0.41838       0.0025528        0.037679
v  CourantNb              0.019834           41298          42.252          7.2025
v  FourierNb              0.022997      2.3655e+05          21.915         0.32495
v  total_pressure       4.3261e+05      7.3349e+05      6.4464e+05      6.2289e+05
v  Local Time Step           0.001        0.020363       0.0010014       0.0010114


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54515      2.4096e+05          64.166          7.5274


 TIME FOR THE TIME STEP              573:        0.85133E+02

===============================================================


 INSTANT    0.574000000E+01   TIME STEP NUMBER             574
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.165074372E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270648327E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.79648E+02 0.93824E+01
   Friction velocity        uet   :  0.33590E-01 0.23368E+02
   Friction velocity        uk    :  0.40602E-01 0.23368E+02
   Dimensionless distance   yplus :  0.11436E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13419
   Nb of faces within the viscous sub-layer     :      10811
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13562E+02      55   0.89406E-01   0.44905E+02 0.31954E+02 
c  Velocity[X]                                      0.73218E+01 
c  Velocity[Y]                                      0.19174E+02 
c  Velocity[Z]                                      0.18410E+02 
c  Pressure     0.10486E+00     686   0.35942E-01   0.99587E-01 0.42259E+01 
c  k            0.54122E+00      20   0.21973E-03   0.75598E-02 0.16961E+02 
c  epsilon      0.55051E+04      14   0.86911E-03   0.21652E+08 0.14753E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.2787e-05                             1
a  epsilon                 -4.6453                             5
a  Local Time Step      2.4703e-08                        281248


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.2869          15.255          1.8378         0.30214
v  Velocity[Y]             -32.593          41.366          1.0216         0.73302
v  Velocity[Z]             -43.237          33.735        -0.95312      -0.0031952
v  ǁVelocityǁ             0.011223          46.409          6.2383          6.3105
v  Pressure                 -67113      2.3433e+05      1.4547e+05      1.2349e+05
v  k                    2.7307e-06          10.786         0.07937        0.075676
v  epsilon                0.020588      2.3066e+06          2930.7          54.156
v  TurbVisc             4.2442e-12         0.41838       0.0025599        0.037683
v  CourantNb              0.010971           40481          42.206          7.2006
v  FourierNb              0.022993      2.3655e+05          21.916         0.32509
v  total_pressure       4.3289e+05      7.3433e+05      6.4547e+05      6.2349e+05
v  Local Time Step           0.001        0.018183       0.0010015       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77395       2.418e+05          64.122          7.5257


 TIME FOR THE TIME STEP              574:        0.83213E+02

===============================================================


 INSTANT    0.575000000E+01   TIME STEP NUMBER             575
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.252951385E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270659604E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61539E+02 0.93083E+01
   Friction velocity        uet   :  0.15989E-01 0.22918E+02
   Friction velocity        uk    :  0.17899E-01 0.22918E+02
   Dimensionless distance   yplus :  0.23147E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13440
   Nb of faces within the viscous sub-layer     :      10820
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13567E+02      59   0.88363E-01   0.44229E+02 0.31718E+02 
c  Velocity[X]                                      0.73625E+01 
c  Velocity[Y]                                      0.18523E+02 
c  Velocity[Z]                                      0.18344E+02 
c  Pressure     0.10494E+00     575   0.36646E-01   0.99852E-01 0.13151E+01 
c  k            0.54159E+00      18   0.73011E-04   0.45874E-02 0.14095E+02 
c  epsilon      0.55328E+04      14   0.27963E-03   0.26865E+07 0.51753E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012209                             1
a  epsilon                 -1.3013                             3
a  Local Time Step        2.45e-08                        281232


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -7.38          18.099          1.8373         0.30193
v  Velocity[Y]              -31.51          30.464          1.0237         0.73283
v  Velocity[Z]             -54.199          31.639         -0.9478      -0.0026583
v  ǁVelocityǁ            0.0037791          58.823          6.2317           6.311
v  Pressure                 -67641      2.3442e+05      1.4556e+05       1.235e+05
v  k                     2.365e-06          11.086        0.079603        0.075727
v  epsilon                 0.02056      2.2999e+06          2943.3           54.26
v  TurbVisc             4.4716e-12         0.41838       0.0025699        0.037688
v  CourantNb             0.0054799           40816          42.169          7.1982
v  FourierNb               0.02299      2.3655e+05          21.918         0.32511
v  total_pressure       4.3236e+05      7.3442e+05      6.4556e+05       6.235e+05
v  Local Time Step           0.001        0.020002       0.0010015       0.0010114


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7547      2.4002e+05          64.087          7.5233


 TIME FOR THE TIME STEP              575:        0.92536E+02

===============================================================


 INSTANT    0.576000000E+01   TIME STEP NUMBER             576
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.202233467E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270590237E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.77433E+02 0.97566E+01
   Friction velocity        uet   :  0.35433E-01 0.22541E+02
   Friction velocity        uk    :  0.47988E-01 0.22541E+02
   Dimensionless distance   yplus :  0.12040E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13424
   Nb of faces within the viscous sub-layer     :      10858
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13577E+02      54   0.93785E-01   0.42563E+02 0.31120E+02 
c  Velocity[X]                                      0.72799E+01 
c  Velocity[Y]                                      0.17543E+02 
c  Velocity[Z]                                      0.17740E+02 
c  Pressure     0.10600E+00     780   0.37517E-01   0.10087E+00 0.51927E+01 
c  k            0.54221E+00      20   0.96055E-04   0.65628E-02 0.16983E+02 
c  epsilon      0.55366E+04      13   0.15875E-03   0.18000E+07 0.42397E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001229                             1
a  epsilon                 -1.5328                             4
a  Local Time Step      2.4337e-08                        281243


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4263          15.441          1.8367         0.30215
v  Velocity[Y]             -30.963          38.516          1.0313         0.73298
v  Velocity[Z]             -43.545          38.973        -0.94112      -0.0033924
v  ǁVelocityǁ            0.0077827          47.115          6.2295          6.3127
v  Pressure                 -67100      2.3537e+05       1.465e+05      1.2425e+05
v  k                    3.1514e-06          11.219        0.079551        0.075783
v  epsilon                0.020494      2.3398e+06          2934.2          54.285
v  TurbVisc             3.9362e-12         0.41838       0.0025817        0.037692
v  CourantNb                     0           41089          42.127          7.1973
v  FourierNb              0.022988      2.3655e+05           21.92         0.32513
v  total_pressure        4.329e+05      7.3537e+05       6.465e+05      6.2425e+05
v  Local Time Step           0.001         0.01903       0.0010015       0.0010111


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63605      2.4107e+05          64.047          7.5224


 TIME FOR THE TIME STEP              576:        0.82996E+02

===============================================================


 INSTANT    0.577000000E+01   TIME STEP NUMBER             577
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.972927276E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270719042E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65864E+02 0.95547E+01
   Friction velocity        uet   :  0.15915E-01 0.19918E+02
   Friction velocity        uk    :  0.22226E-01 0.19918E+02
   Dimensionless distance   yplus :  0.25415E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13428
   Nb of faces within the viscous sub-layer     :      10858
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13585E+02      51   0.92378E-01   0.41393E+02 0.30688E+02 
c  Velocity[X]                                      0.71106E+01 
c  Velocity[Y]                                      0.16556E+02 
c  Velocity[Z]                                      0.17725E+02 
c  Pressure     0.10594E+00     449   0.37256E-01   0.10084E+00 0.12868E+01 
c  k            0.54270E+00      19   0.19866E-03   0.80548E-02 0.18078E+02 
c  epsilon      0.55352E+04      12   0.18451E-03   0.21989E+07 0.46794E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021488                             2
a  epsilon                 -1.3515                             3
a  Local Time Step      2.4074e-08                        281209


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4562          18.734          1.8379         0.30227
v  Velocity[Y]             -30.709           39.77          1.0412         0.73272
v  Velocity[Z]             -54.588          31.561        -0.93567      -0.0039034
v  ǁVelocityǁ            0.0070621          59.991          6.2304          6.3136
v  Pressure                 -67441      2.3542e+05      1.4652e+05      1.2425e+05
v  k                    2.3598e-06          11.084        0.079679        0.075831
v  epsilon                0.020036      2.3019e+06          2935.3          54.365
v  TurbVisc             5.1197e-12         0.41838       0.0025897        0.037697
v  CourantNb              0.011509           41539          42.107          7.1975
v  FourierNb              0.022987      2.3655e+05          21.925         0.32525
v  total_pressure       4.3256e+05      7.3542e+05      6.4652e+05      6.2425e+05
v  Local Time Step           0.001        0.016407       0.0010015       0.0010111


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67247      2.4028e+05          64.032          7.5227


 TIME FOR THE TIME STEP              577:        0.76770E+02

===============================================================


 INSTANT    0.578000000E+01   TIME STEP NUMBER             578
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.352104377E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270780453E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83144E+02 0.93574E+01
   Friction velocity        uet   :  0.21139E-01 0.17930E+02
   Friction velocity        uk    :  0.40936E-01 0.17930E+02
   Dimensionless distance   yplus :  0.22879E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13434
   Nb of faces within the viscous sub-layer     :      10870
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13589E+02      50   0.90757E-01   0.43242E+02 0.31354E+02 
c  Velocity[X]                                      0.71948E+01 
c  Velocity[Y]                                      0.16387E+02 
c  Velocity[Z]                                      0.19660E+02 
c  Pressure     0.10468E+00     571   0.35929E-01   0.99609E-01 0.12221E+01 
c  k            0.54216E+00      20   0.30285E-03   0.95028E-02 0.18568E+02 
c  epsilon      0.55190E+04      12   0.21726E-03   0.26253E+07 0.51262E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020406                             1
a  epsilon                 -1.5246                             4
a  Local Time Step      2.3399e-08                        281223


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5017          15.313          1.8421         0.30247
v  Velocity[Y]             -32.603           40.62          1.0521          0.7326
v  Velocity[Z]             -46.946          35.216        -0.93236      -0.0042824
v  ǁVelocityǁ             0.011036          49.949          6.2358          6.3144
v  Pressure                 -67706      2.3542e+05      1.4654e+05      1.2429e+05
v  k                    2.4787e-06          10.405        0.079629        0.075882
v  epsilon                0.019391      2.3234e+06          2924.7          54.409
v  TurbVisc             3.8804e-12         0.41838        0.002593        0.037702
v  CourantNb              0.021461           42737          42.074          7.1981
v  FourierNb              0.022989      2.3655e+05          21.922         0.32528
v  total_pressure       4.3229e+05      7.3542e+05      6.4654e+05      6.2429e+05
v  Local Time Step           0.001        0.018048       0.0010015       0.0010112


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64587       2.411e+05          63.996          7.5234


 TIME FOR THE TIME STEP              578:        0.84333E+02

===============================================================


 INSTANT    0.579000000E+01   TIME STEP NUMBER             579
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.433998247E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270841178E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65452E+02 0.94561E+01
   Friction velocity        uet   :  0.25516E-01 0.25380E+02
   Friction velocity        uk    :  0.37429E-01 0.25380E+02
   Dimensionless distance   yplus :  0.32386E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13433
   Nb of faces within the viscous sub-layer     :      10888
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13593E+02      50   0.90120E-01   0.43636E+02 0.31485E+02 
c  Velocity[X]                                      0.67726E+01 
c  Velocity[Y]                                      0.17120E+02 
c  Velocity[Z]                                      0.19743E+02 
c  Pressure     0.10322E+00     443   0.34859E-01   0.98329E-01 0.10784E+01 
c  k            0.54220E+00      20   0.70210E-04   0.57850E-02 0.15968E+02 
c  epsilon      0.55067E+04      14   0.17561E-03   0.25534E+07 0.50776E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.3297e-05                             1
a  epsilon                 -1.5545                             4
a  Local Time Step      2.4108e-08                        281200


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4897          18.746          1.8434         0.30231
v  Velocity[Y]             -32.398          38.978          1.0644         0.73256
v  Velocity[Z]             -54.841          31.694        -0.93313      -0.0046144
v  ǁVelocityǁ             0.015431          59.937          6.2422          6.3152
v  Pressure                 -68002      2.3542e+05      1.4655e+05      1.2429e+05
v  k                    2.3219e-06          10.147        0.079578        0.075928
v  epsilon                0.018698      2.2773e+06          2918.8          54.408
v  TurbVisc             4.0816e-12         0.41838       0.0025943        0.037708
v  CourantNb              0.021121           41481          42.105          7.1989
v  FourierNb              0.022993      2.3655e+05          21.922         0.32532
v  total_pressure         4.32e+05      7.3542e+05      6.4655e+05      6.2429e+05
v  Local Time Step           0.001        0.019853       0.0010015       0.0010112


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63136      2.4117e+05          64.026          7.5242


 TIME FOR THE TIME STEP              579:        0.74384E+02

===============================================================


 INSTANT    0.580000000E+01   TIME STEP NUMBER             580
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.134791386E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270828954E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.81517E+02 0.90503E+01
   Friction velocity        uet   :  0.36438E-01 0.17515E+02
   Friction velocity        uk    :  0.41136E-01 0.17515E+02
   Dimensionless distance   yplus :  0.22349E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13452
   Nb of faces within the viscous sub-layer     :      10882
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13602E+02      59   0.90014E-01   0.40933E+02 0.30491E+02 
c  Velocity[X]                                      0.67467E+01 
c  Velocity[Y]                                      0.15878E+02 
c  Velocity[Z]                                      0.18308E+02 
c  Pressure     0.10060E+00     530   0.34135E-01   0.95734E-01 0.10690E+01 
c  k            0.54123E+00      19   0.70518E-04   0.47699E-02 0.14416E+02 
c  epsilon      0.55114E+04      13   0.50307E-03   0.60395E+07 0.77837E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.9994e-06                             1
a  epsilon                 -1.1353                             3
a  Local Time Step      2.3941e-08                        281198


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4611          15.384          1.8415         0.30215
v  Velocity[Y]             -31.544          29.018          1.0781         0.73229
v  Velocity[Z]             -42.848          39.849        -0.93204      -0.0047659
v  ǁVelocityǁ             0.018644          46.447          6.2484          6.3167
v  Pressure                 -68176      2.3535e+05      1.4654e+05      1.2434e+05
v  k                    2.4444e-06          10.316        0.079696        0.075983
v  epsilon                0.018074      2.3247e+06          2931.3          54.488
v  TurbVisc             3.8873e-12         0.41838       0.0025945        0.037714
v  CourantNb              0.032025           41770          42.162          7.2011
v  FourierNb              0.022997      2.3655e+05          21.919         0.32536
v  total_pressure       4.3182e+05      7.3535e+05      6.4654e+05      6.2434e+05
v  Local Time Step           0.001        0.020234       0.0010015       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56474      2.4157e+05           64.08          7.5265


 TIME FOR THE TIME STEP              580:        0.78603E+02

===============================================================


 INSTANT    0.581000000E+01   TIME STEP NUMBER             581
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.313386055E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270842683E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64219E+02 0.90125E+01
   Friction velocity        uet   :  0.36250E-01 0.18264E+02
   Friction velocity        uk    :  0.45290E-01 0.18264E+02
   Dimensionless distance   yplus :  0.23305E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13490
   Nb of faces within the viscous sub-layer     :      10845
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13606E+02      49   0.93014E-01   0.40013E+02 0.30155E+02 
c  Velocity[X]                                      0.67570E+01 
c  Velocity[Y]                                      0.15606E+02 
c  Velocity[Z]                                      0.17649E+02 
c  Pressure     0.99801E-01     475   0.33228E-01   0.94992E-01 0.99903E+00 
c  k            0.54111E+00      22   0.67943E-04   0.40547E-02 0.13299E+02 
c  epsilon      0.55055E+04      16   0.69610E-03   0.62185E+07 0.79012E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.2047e-05                             1
a  epsilon                  -1.625                             5
a  Local Time Step      2.4213e-08                        281228


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5243           19.19           1.839         0.30225
v  Velocity[Y]             -30.293          34.553           1.091         0.73204
v  Velocity[Z]             -55.325          31.954        -0.93198      -0.0051933
v  ǁVelocityǁ             0.015665          60.927          6.2568          6.3172
v  Pressure                 -68410      2.3534e+05      1.4654e+05      1.2437e+05
v  k                     2.371e-06           10.33        0.079744        0.076042
v  epsilon                0.017363      2.2833e+06          2935.9          54.605
v  TurbVisc               4.05e-12         0.41838       0.0025933        0.037719
v  CourantNb              0.041781           41300          42.157          7.2033
v  FourierNb              0.023003      2.3655e+05          21.918         0.32538
v  total_pressure       4.3159e+05      7.3534e+05      6.4654e+05      6.2437e+05
v  Local Time Step           0.001        0.022159       0.0010014        0.001011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81827      2.3992e+05          64.074          7.5287


 TIME FOR THE TIME STEP              581:        0.76380E+02

===============================================================


 INSTANT    0.582000000E+01   TIME STEP NUMBER             582
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.110059628E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270871353E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84371E+02 0.93105E+01
   Friction velocity        uet   :  0.36430E-01 0.17796E+02
   Friction velocity        uk    :  0.43940E-01 0.17796E+02
   Dimensionless distance   yplus :  0.22708E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13498
   Nb of faces within the viscous sub-layer     :      10843
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13609E+02      57   0.91834E-01   0.42854E+02 0.31183E+02 
c  Velocity[X]                                      0.71934E+01 
c  Velocity[Y]                                      0.17069E+02 
c  Velocity[Z]                                      0.18591E+02 
c  Pressure     0.10393E+00     346   0.33954E-01   0.98843E-01 0.91448E+00 
c  k            0.54167E+00      18   0.72452E-04   0.40834E-02 0.13390E+02 
c  epsilon      0.55065E+04      14   0.40860E-03   0.30861E+07 0.55669E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -7.2831                             4
a  Local Time Step      2.3909e-08                        281209


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4307          15.408          1.8348         0.30237
v  Velocity[Y]             -30.869          35.597          1.1059         0.73202
v  Velocity[Z]             -46.876          32.819        -0.93438      -0.0057513
v  ǁVelocityǁ            0.0043852          49.856          6.2659          6.3187
v  Pressure                 -68499      2.3528e+05      1.4652e+05       1.244e+05
v  k                    2.4039e-06          10.808        0.079741        0.076093
v  epsilon                0.016815      2.3296e+06          2931.2          54.699
v  TurbVisc             3.9455e-12         0.41838       0.0025896        0.037725
v  CourantNb                     0           41825          42.205          7.2046
v  FourierNb              0.023011      2.3655e+05          21.915         0.32538
v  total_pressure        4.315e+05      7.3528e+05      6.4652e+05       6.244e+05
v  Local Time Step           0.001        0.021519       0.0010014       0.0010107


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71044      2.3891e+05           64.12            7.53


 TIME FOR THE TIME STEP              582:        0.71398E+02

===============================================================


 INSTANT    0.583000000E+01   TIME STEP NUMBER             583
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.499587573E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270918754E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65058E+02 0.96158E+01
   Friction velocity        uet   :  0.36630E-01 0.15003E+02
   Friction velocity        uk    :  0.50981E-01 0.15003E+02
   Dimensionless distance   yplus :  0.11569E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13536
   Nb of faces within the viscous sub-layer     :      10813
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13620E+02      50   0.92510E-01   0.45583E+02 0.32170E+02 
c  Velocity[X]                                      0.70362E+01 
c  Velocity[Y]                                      0.18702E+02 
c  Velocity[Z]                                      0.19844E+02 
c  Pressure     0.10475E+00     295   0.34585E-01   0.99741E-01 0.96888E+00 
c  k            0.54281E+00      19   0.15962E-03   0.79989E-02 0.17769E+02 
c  epsilon      0.55022E+04      12   0.25382E-03   0.31172E+07 0.55825E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023661                             1
a  epsilon                 -2.1348                             4
a  Local Time Step      2.4024e-08                        281208


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4724          18.639          1.8306         0.30261
v  Velocity[Y]             -32.319          27.422          1.1182         0.73198
v  Velocity[Z]             -54.154          31.901         -0.9376      -0.0062644
v  ǁVelocityǁ             0.020484          59.537          6.2747          6.3199
v  Pressure                 -68533      2.3527e+05       1.465e+05      1.2441e+05
v  k                    2.5641e-06           11.18        0.079821        0.076152
v  epsilon                0.016443      2.2828e+06          2933.1          54.858
v  TurbVisc             3.9951e-12         0.41838       0.0025887         0.03773
v  CourantNb              0.026294           41624          42.278          7.2074
v  FourierNb               0.02302      2.3655e+05          21.914         0.32533
v  total_pressure       4.3147e+05      7.3527e+05       6.465e+05      6.2441e+05
v  Local Time Step           0.001        0.019702       0.0010014       0.0010107


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62551       2.382e+05          64.193          7.5327


 TIME FOR THE TIME STEP              583:        0.69719E+02

===============================================================


 INSTANT    0.584000000E+01   TIME STEP NUMBER             584
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.187782053E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270951664E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80718E+02 0.94485E+01
   Friction velocity        uet   :  0.34203E-01 0.18023E+02
   Friction velocity        uk    :  0.34166E-01 0.18023E+02
   Dimensionless distance   yplus :  0.22723E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13548
   Nb of faces within the viscous sub-layer     :      10793
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13620E+02      49   0.90728E-01   0.44255E+02 0.31658E+02 
c  Velocity[X]                                      0.70238E+01 
c  Velocity[Y]                                      0.18213E+02 
c  Velocity[Z]                                      0.19019E+02 
c  Pressure     0.10656E+00     310   0.36008E-01   0.10148E+00 0.10308E+01 
c  k            0.54189E+00      20   0.35631E-03   0.10970E-01 0.19389E+02 
c  epsilon      0.55080E+04      13   0.19797E-03   0.33965E+07 0.58181E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00026494                             2
a  epsilon                 -1.8371                             6
a  Local Time Step      2.3788e-08                        281215


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4494          15.251          1.8279          0.3032
v  Velocity[Y]             -34.666          30.964          1.1279         0.73173
v  Velocity[Z]             -44.532           37.68         -0.9403      -0.0066762
v  ǁVelocityǁ              0.01788          47.417          6.2836          6.3208
v  Pressure                 -68343      2.3526e+05      1.4647e+05      1.2442e+05
v  k                    2.3827e-06          11.496        0.079815        0.076196
v  epsilon                0.016203      2.3512e+06          2926.6          54.903
v  TurbVisc             4.2552e-12         0.41838       0.0025909        0.037735
v  CourantNb             0.0015271           42037          42.356          7.2109
v  FourierNb               0.02303      2.3655e+05          21.914         0.32536
v  total_pressure       4.3166e+05      7.3526e+05      6.4647e+05      6.2442e+05
v  Local Time Step           0.001        0.021672       0.0010014       0.0010109


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.79206       2.386e+05           64.27          7.5362


 TIME FOR THE TIME STEP              584:        0.64467E+02

===============================================================


 INSTANT    0.585000000E+01   TIME STEP NUMBER             585
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.305062083E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271013534E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68373E+02 0.91235E+01
   Friction velocity        uet   :  0.35415E-01 0.16998E+02
   Friction velocity        uk    :  0.48655E-01 0.16998E+02
   Dimensionless distance   yplus :  0.80932E-03 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13569
   Nb of faces within the viscous sub-layer     :      10774
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13627E+02      50   0.92362E-01   0.43455E+02 0.31396E+02 
c  Velocity[X]                                      0.67178E+01 
c  Velocity[Y]                                      0.18310E+02 
c  Velocity[Z]                                      0.18427E+02 
c  Pressure     0.11072E+00     298   0.38046E-01   0.10557E+00 0.10769E+01 
c  k            0.54084E+00      22   0.16660E-03   0.12686E-01 0.23193E+02 
c  epsilon      0.54931E+04      12   0.29576E-03   0.52174E+07 0.72376E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021063                             1
a  epsilon                 -1.4076                             6
a  Local Time Step       2.414e-08                        281211


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4716          18.934          1.8258         0.30343
v  Velocity[Y]             -33.508          30.983          1.1338         0.73198
v  Velocity[Z]             -55.335            32.2        -0.94025      -0.0068922
v  ǁVelocityǁ            0.0087236           60.84          6.2887          6.3208
v  Pressure                 -68262      2.3529e+05      1.4645e+05      1.2442e+05
v  k                    2.4078e-06           11.49        0.079918        0.076239
v  epsilon                0.010485      2.2759e+06          2924.3           54.98
v  TurbVisc             3.9833e-12         0.41838       0.0025954         0.03774
v  CourantNb             0.0065615           41426          42.438          7.2142
v  FourierNb              0.023041      2.3655e+05          21.915          0.3254
v  total_pressure       4.3174e+05      7.3529e+05      6.4645e+05      6.2442e+05
v  Local Time Step           0.001        0.019791       0.0010014        0.001011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73788      2.4071e+05          64.353          7.5396


 TIME FOR THE TIME STEP              585:        0.67491E+02

===============================================================


 INSTANT    0.586000000E+01   TIME STEP NUMBER             586
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.875329792E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271058467E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84343E+02 0.84296E+01
   Friction velocity        uet   :  0.36335E-01 0.21339E+02
   Friction velocity        uk    :  0.45343E-01 0.21339E+02
   Dimensionless distance   yplus :  0.24306E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13576
   Nb of faces within the viscous sub-layer     :      10757
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13625E+02      51   0.92483E-01   0.43362E+02 0.31357E+02 
c  Velocity[X]                                      0.67882E+01 
c  Velocity[Y]                                      0.17788E+02 
c  Velocity[Z]                                      0.18786E+02 
c  Pressure     0.11235E+00     333   0.38611E-01   0.10726E+00 0.10472E+01 
c  k            0.53851E+00      21   0.28372E-03   0.14585E-01 0.23695E+02 
c  epsilon      0.54905E+04      13   0.29734E-03   0.42287E+07 0.64960E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001577                             2
a  epsilon                 -1.6159                             4
a  Local Time Step        2.48e-08                        281214


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3856          15.235          1.8238         0.30356
v  Velocity[Y]             -32.341           31.73          1.1378         0.73184
v  Velocity[Z]              -47.12          33.629        -0.94111      -0.0070838
v  ǁVelocityǁ            0.0083068          50.112          6.2931           6.321
v  Pressure                 -68120      2.3533e+05      1.4643e+05      1.2443e+05
v  k                    2.4494e-06          11.048        0.079977        0.076282
v  epsilon               0.0096314      2.3291e+06            2928          55.013
v  TurbVisc             4.0237e-12         0.41838       0.0026014        0.037745
v  CourantNb                     0           40323          42.487           7.215
v  FourierNb               0.02305      2.3655e+05          21.917         0.32547
v  total_pressure       4.3188e+05      7.3533e+05      6.4643e+05      6.2443e+05
v  Local Time Step           0.001         0.02177       0.0010015       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73035       2.405e+05          64.404          7.5405


 TIME FOR THE TIME STEP              586:        0.69400E+02

===============================================================


 INSTANT    0.587000000E+01   TIME STEP NUMBER             587
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.514347612E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271131642E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65821E+02 0.77493E+01
   Friction velocity        uet   :  0.36372E-01 0.20027E+02
   Friction velocity        uk    :  0.43953E-01 0.20027E+02
   Dimensionless distance   yplus :  0.13133E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13604
   Nb of faces within the viscous sub-layer     :      10780
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13625E+02      48   0.90959E-01   0.43045E+02 0.31212E+02 
c  Velocity[X]                                      0.65145E+01 
c  Velocity[Y]                                      0.17273E+02 
c  Velocity[Z]                                      0.19257E+02 
c  Pressure     0.11245E+00     405   0.38465E-01   0.10748E+00 0.10927E+01 
c  k            0.53729E+00      20   0.14239E-03   0.10264E-01 0.21333E+02 
c  epsilon      0.54686E+04      12   0.20806E-03   0.23803E+07 0.49131E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00029585                             2
a  epsilon                 -3.2379                             7
a  Local Time Step      2.4186e-08                        281180


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3973          18.447          1.8214         0.30393
v  Velocity[Y]             -32.651          31.685          1.1393         0.73189
v  Velocity[Z]             -54.506          32.192        -0.94015      -0.0077812
v  ǁVelocityǁ             0.014019          59.811          6.2958          6.3212
v  Pressure                 -68088      2.3531e+05      1.4639e+05      1.2441e+05
v  k                    2.5234e-06          11.001        0.079832        0.076318
v  epsilon               0.0030451      2.2743e+06          2915.6          55.014
v  TurbVisc             4.1147e-12         0.41838       0.0026063        0.037751
v  CourantNb              0.062543           41347          42.476          7.2167
v  FourierNb              0.023061      2.3655e+05          21.918         0.32545
v  total_pressure       4.3191e+05      7.3531e+05      6.4639e+05      6.2441e+05
v  Local Time Step           0.001        0.023219       0.0010015       0.0010109


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55846      2.4007e+05          64.394          7.5421


 TIME FOR THE TIME STEP              587:        0.80098E+02

===============================================================


 INSTANT    0.588000000E+01   TIME STEP NUMBER             588
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.139405780E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271224822E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.81032E+02 0.70467E+01
   Friction velocity        uet   :  0.36031E-01 0.17984E+02
   Friction velocity        uk    :  0.40105E-01 0.17984E+02
   Dimensionless distance   yplus :  0.22692E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13589
   Nb of faces within the viscous sub-layer     :      10773
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13626E+02      48   0.91779E-01   0.41179E+02 0.30552E+02 
c  Velocity[X]                                      0.66504E+01 
c  Velocity[Y]                                      0.16338E+02 
c  Velocity[Z]                                      0.18191E+02 
c  Pressure     0.10750E+00     848   0.36519E-01   0.10256E+00 0.20691E+01 
c  k            0.53590E+00      20   0.15720E-03   0.10727E-01 0.21850E+02 
c  epsilon      0.54301E+04      13   0.18711E-03   0.78063E+07 0.89239E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0464e-05                             1
a  epsilon                 -1.5364                             5
a  Local Time Step      2.4124e-08                        281206


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3885           15.31          1.8193         0.30414
v  Velocity[Y]              -30.18          31.908          1.1384         0.73215
v  Velocity[Z]             -43.738          38.618        -0.93646      -0.0081967
v  ǁVelocityǁ            0.0074615          47.759          6.2945          6.3209
v  Pressure                 -68069      2.3501e+05      1.4605e+05      1.2416e+05
v  k                    2.4136e-06          10.946        0.079736        0.076353
v  epsilon                 0.01606      2.3382e+06          2904.7          55.012
v  TurbVisc             4.1501e-12         0.41838       0.0026076        0.037756
v  CourantNb              0.019171           41453          42.462          7.2174
v  FourierNb              0.023069      2.3655e+05          21.919         0.32541
v  total_pressure       4.3193e+05      7.3501e+05      6.4605e+05      6.2416e+05
v  Local Time Step           0.001        0.021523       0.0010014        0.001011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64517      2.3916e+05          64.381          7.5429


 TIME FOR THE TIME STEP              588:        0.96225E+02

===============================================================


 INSTANT    0.589000000E+01   TIME STEP NUMBER             589
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.594173442E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271236056E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63578E+02 0.69562E+01
   Friction velocity        uet   :  0.35689E-01 0.18532E+02
   Friction velocity        uk    :  0.36588E-01 0.18532E+02
   Dimensionless distance   yplus :  0.13473E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13591
   Nb of faces within the viscous sub-layer     :      10797
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13625E+02      53   0.92432E-01   0.38806E+02 0.29679E+02 
c  Velocity[X]                                      0.65916E+01 
c  Velocity[Y]                                      0.15196E+02 
c  Velocity[Z]                                      0.17018E+02 
c  Pressure     0.10302E+00     844   0.35016E-01   0.98396E-01 0.56360E+01 
c  k            0.53596E+00      19   0.86888E-04   0.72655E-02 0.17925E+02 
c  epsilon      0.54210E+04      13   0.17525E-03   0.29764E+07 0.55238E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                -0.82204                             4
a  Local Time Step      2.4248e-08                        281179


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.3787          18.518           1.818         0.30365
v  Velocity[Y]              -32.56           32.25          1.1342          0.7323
v  Velocity[Z]             -55.266          32.311        -0.93132      -0.0072696
v  ǁVelocityǁ            0.0062773          60.591          6.2899          6.3175
v  Pressure                 -68783      2.3396e+05      1.4501e+05      1.2335e+05
v  k                    2.5345e-06           11.33        0.079536        0.076377
v  epsilon                0.016052      2.3014e+06          2892.8          54.965
v  TurbVisc             4.0058e-12         0.41838       0.0026067        0.037761
v  CourantNb              0.067251           41240          42.399           7.216
v  FourierNb              0.023077      2.3655e+05          21.921         0.32555
v  total_pressure       4.3122e+05      7.3396e+05      6.4501e+05      6.2335e+05
v  Local Time Step           0.001        0.023675       0.0010015       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52584       2.397e+05           64.32          7.5415


 TIME FOR THE TIME STEP              589:        0.99506E+02

===============================================================


 INSTANT    0.590000000E+01   TIME STEP NUMBER             590
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.323105558E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271193424E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83681E+02 0.75885E+01
   Friction velocity        uet   :  0.34398E-01 0.18959E+02
   Friction velocity        uk    :  0.34057E-01 0.18959E+02
   Dimensionless distance   yplus :  0.81422E-03 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13581
   Nb of faces within the viscous sub-layer     :      10816
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13606E+02      52   0.89426E-01   0.38028E+02 0.29383E+02 
c  Velocity[X]                                      0.62357E+01 
c  Velocity[Y]                                      0.14788E+02 
c  Velocity[Z]                                      0.17004E+02 
c  Pressure     0.10389E+00     467   0.35151E-01   0.99343E-01 0.14386E+01 
c  k            0.53635E+00      21   0.70495E-04   0.65206E-02 0.16881E+02 
c  epsilon      0.54062E+04      11   0.15292E-03   0.21665E+07 0.47215E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -1.2349                             4
a  Local Time Step       2.445e-08                        281179


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4117          15.284          1.8157         0.30352
v  Velocity[Y]             -36.079          32.588          1.1264         0.73297
v  Velocity[Z]             -43.646          35.316        -0.92484       -0.006748
v  ǁVelocityǁ             0.012925          46.913          6.2813          6.3155
v  Pressure                 -68435      2.3388e+05      1.4496e+05      1.2339e+05
v  k                    2.5523e-06          11.582        0.079242        0.076387
v  epsilon                0.016024      2.3142e+06          2881.8          54.883
v  TurbVisc             4.2286e-12         0.41838       0.0026048        0.037766
v  CourantNb              0.010374           40900          42.331          7.2133
v  FourierNb              0.023083      2.3655e+05           21.92         0.32555
v  total_pressure       4.3156e+05      7.3388e+05      6.4496e+05      6.2339e+05
v  Local Time Step           0.001        0.026043       0.0010015       0.0010113


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44156      2.3778e+05          64.251          7.5389


 TIME FOR THE TIME STEP              590:        0.83227E+02

===============================================================


 INSTANT    0.591000000E+01   TIME STEP NUMBER             591
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.637353558E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271200774E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62039E+02 0.79567E+01
   Friction velocity        uet   :  0.32651E-01 0.16203E+02
   Friction velocity        uk    :  0.34876E-01 0.16203E+02
   Dimensionless distance   yplus :  0.11891E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13576
   Nb of faces within the viscous sub-layer     :      10836
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13607E+02      51   0.89641E-01   0.36971E+02 0.28996E+02 
c  Velocity[X]                                      0.60295E+01 
c  Velocity[Y]                                      0.13134E+02 
c  Velocity[Z]                                      0.17807E+02 
c  Pressure     0.96888E-01     877   0.32806E-01   0.92856E-01 0.31743E+01 
c  k            0.53749E+00      24   0.16740E-03   0.91402E-02 0.19590E+02 
c  epsilon      0.53999E+04      11   0.14387E-03   0.10140E+07 0.32253E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.1141e-05                             1
a  epsilon               -0.060623                             1
a  Local Time Step      2.4434e-08                        281165


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.356          18.879           1.814         0.30331
v  Velocity[Y]             -33.694          33.297          1.1161         0.73347
v  Velocity[Z]             -56.275          32.092        -0.91747      -0.0059593
v  ǁVelocityǁ            0.0057489          61.765            6.27          6.3124
v  Pressure                 -68727      2.3332e+05       1.444e+05      1.2299e+05
v  k                    2.9319e-06          11.527        0.079011        0.076395
v  epsilon                0.015991      2.2779e+06          2875.9          54.801
v  TurbVisc             4.2475e-12         0.41838       0.0026017        0.037771
v  CourantNb             0.0034604           40927          42.229          7.2098
v  FourierNb              0.023088      2.3655e+05          21.918          0.3255
v  total_pressure       4.3127e+05      7.3332e+05       6.444e+05      6.2299e+05
v  Local Time Step           0.001        0.027747       0.0010015       0.0010114


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55334       2.397e+05          64.148          7.5353


 TIME FOR THE TIME STEP              591:        0.10060E+03

===============================================================


 INSTANT    0.592000000E+01   TIME STEP NUMBER             592
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.596307431E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271130604E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85955E+02 0.83241E+01
   Friction velocity        uet   :  0.21903E-01 0.20117E+02
   Friction velocity        uk    :  0.50571E-01 0.20117E+02
   Dimensionless distance   yplus :  0.22843E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13565
   Nb of faces within the viscous sub-layer     :      10855
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13603E+02      49   0.89076E-01   0.35155E+02 0.28271E+02 
c  Velocity[X]                                      0.58144E+01 
c  Velocity[Y]                                      0.12498E+02 
c  Velocity[Z]                                      0.16843E+02 
c  Pressure     0.96259E-01     573   0.32526E-01   0.92316E-01 0.14882E+01 
c  k            0.53795E+00      20   0.64580E-04   0.57088E-02 0.15840E+02 
c  epsilon      0.53934E+04      11   0.15561E-03   0.13203E+07 0.36938E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon               -0.015497                             1
a  Local Time Step      2.4055e-08                        281155


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4236          15.246          1.8139         0.30293
v  Velocity[Y]              -31.49          32.438          1.1055         0.73352
v  Velocity[Z]             -41.678           40.04        -0.91149      -0.0062098
v  ǁVelocityǁ             0.013953           45.46          6.2598          6.3099
v  Pressure                 -68364      2.3324e+05      1.4435e+05      1.2298e+05
v  k                    2.3735e-06          11.461        0.078822        0.076404
v  epsilon                0.015497      2.3303e+06          2871.3          54.738
v  TurbVisc             4.7547e-12         0.41838       0.0025981        0.037775
v  CourantNb              0.030235           41571           42.13          7.2055
v  FourierNb               0.02309      2.3655e+05          21.918         0.32551
v  total_pressure       4.3164e+05      7.3324e+05      6.4435e+05      6.2298e+05
v  Local Time Step           0.001        0.028508       0.0010016       0.0010115


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55749      2.4014e+05          64.048           7.531


 TIME FOR THE TIME STEP              592:        0.76876E+02

===============================================================


 INSTANT    0.593000000E+01   TIME STEP NUMBER             593
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.188352214E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271189449E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59555E+02 0.79678E+01
   Friction velocity        uet   :  0.20533E-01 0.20788E+02
   Friction velocity        uk    :  0.59011E-01 0.20788E+02
   Dimensionless distance   yplus :  0.23208E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13578
   Nb of faces within the viscous sub-layer     :      10884
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13600E+02      59   0.87902E-01   0.33209E+02 0.27498E+02 
c  Velocity[X]                                      0.56121E+01 
c  Velocity[Y]                                      0.11107E+02 
c  Velocity[Z]                                      0.16490E+02 
c  Pressure     0.92856E-01     768   0.31214E-01   0.89190E-01 0.29314E+01 
c  k            0.53842E+00      24   0.15068E-03   0.90292E-02 0.19957E+02 
c  epsilon      0.53655E+04      11   0.18317E-03   0.33311E+07 0.58987E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017452                             1
a  epsilon                 -1.1653                             2
a  Local Time Step      2.4105e-08                        281124


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4943          18.839          1.8156          0.3024
v  Velocity[Y]             -31.528          33.546          1.0929         0.73313
v  Velocity[Z]              -56.05          32.294        -0.90772      -0.0063543
v  ǁVelocityǁ              0.01125          61.566          6.2495          6.3076
v  Pressure                 -68697      2.3272e+05      1.4387e+05      1.2261e+05
v  k                    2.5498e-06          11.149         0.07862        0.076393
v  epsilon                0.016114      2.2728e+06          2851.7          54.655
v  TurbVisc             3.8799e-12         0.41838       0.0025949        0.037779
v  CourantNb                     0           41486          42.046          7.2018
v  FourierNb              0.023095      2.3655e+05          21.919         0.32552
v  total_pressure        4.313e+05      7.3272e+05      6.4387e+05      6.2261e+05
v  Local Time Step           0.001        0.027762       0.0010016       0.0010114


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59923      2.3849e+05          63.965          7.5273


 TIME FOR THE TIME STEP              593:        0.94531E+02

===============================================================


 INSTANT    0.594000000E+01   TIME STEP NUMBER             594
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.555872723E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271196500E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85759E+02 0.80793E+01
   Friction velocity        uet   :  0.30230E-01 0.18775E+02
   Friction velocity        uk    :  0.55155E-01 0.18775E+02
   Dimensionless distance   yplus :  0.12955E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13587
   Nb of faces within the viscous sub-layer     :      10892
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13600E+02      57   0.88972E-01   0.33056E+02 0.27424E+02 
c  Velocity[X]                                      0.51627E+01 
c  Velocity[Y]                                      0.11339E+02 
c  Velocity[Z]                                      0.16554E+02 
c  Pressure     0.89076E-01     485   0.29800E-01   0.85584E-01 0.11229E+01 
c  k            0.53952E+00      19   0.19754E-03   0.13731E-01 0.24299E+02 
c  epsilon      0.53663E+04      14   0.24113E-03   0.23729E+07 0.49671E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                -0.20193                             1
a  Local Time Step      2.4633e-08                        281122


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4196          15.267          1.8179         0.30215
v  Velocity[Y]             -34.636          32.068          1.0809         0.73314
v  Velocity[Z]             -41.581          33.426        -0.90483      -0.0070386
v  ǁVelocityǁ            0.0055111          45.079          6.2415          6.3062
v  Pressure                 -71939      2.3264e+05      1.4383e+05      1.2262e+05
v  k                    2.6325e-06          11.141        0.078498        0.076367
v  epsilon                0.016289      2.3334e+06          2854.7          54.549
v  TurbVisc             4.3349e-12         0.41838       0.0025916        0.037781
v  CourantNb              0.038585           40596          41.975          7.1985
v  FourierNb              0.023098      2.3656e+05          21.917         0.32549
v  total_pressure       4.2806e+05      7.3264e+05      6.4383e+05      6.2262e+05
v  Local Time Step           0.001        0.028167       0.0010016       0.0010114


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73248       2.395e+05          63.892          7.5239


 TIME FOR THE TIME STEP              594:        0.75737E+02

===============================================================


 INSTANT    0.595000000E+01   TIME STEP NUMBER             595
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.413344832E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271295706E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58142E+02 0.86686E+01
   Friction velocity        uet   :  0.33373E-01 0.21544E+02
   Friction velocity        uk    :  0.47809E-01 0.21544E+02
   Dimensionless distance   yplus :  0.11814E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13592
   Nb of faces within the viscous sub-layer     :      10924
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13599E+02      47   0.88699E-01   0.33161E+02 0.27483E+02 
c  Velocity[X]                                      0.50790E+01 
c  Velocity[Y]                                      0.11565E+02 
c  Velocity[Z]                                      0.16518E+02 
c  Pressure     0.87770E-01     868   0.29275E-01   0.84509E-01 0.40535E+01 
c  k            0.53993E+00      20   0.13371E-03   0.10860E-01 0.21702E+02 
c  epsilon      0.53788E+04      11   0.18453E-03   0.25470E+07 0.51468E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00077257                             1
a  epsilon               -0.060467                             1
a  Local Time Step      2.4045e-08                        281077


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5572          18.774          1.8204         0.30188
v  Velocity[Y]             -33.214          31.332          1.0675         0.73288
v  Velocity[Z]             -55.967           32.25        -0.90428      -0.0069977
v  ǁVelocityǁ              0.01164          61.454          6.2358          6.3042
v  Pressure                 -75136      2.3194e+05      1.4314e+05      1.2204e+05
v  k                    2.6729e-06          11.147        0.078347        0.076334
v  epsilon                0.016463      2.3055e+06          2846.2          54.467
v  TurbVisc              4.279e-12         0.41838        0.002589        0.037783
v  CourantNb               0.11518           41589          41.912          7.1955
v  FourierNb              0.023104      2.3656e+05          21.916         0.32561
v  total_pressure       4.2486e+05      7.3194e+05      6.4314e+05      6.2204e+05
v  Local Time Step           0.001        0.023835       0.0010017       0.0010115


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73815      2.3923e+05          63.829          7.5211


 TIME FOR THE TIME STEP              595:        0.86788E+02

===============================================================


 INSTANT    0.596000000E+01   TIME STEP NUMBER             596
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.239779897E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271213169E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84913E+02 0.87061E+01
   Friction velocity        uet   :  0.35043E-01 0.20027E+02
   Friction velocity        uk    :  0.59703E-01 0.20027E+02
   Dimensionless distance   yplus :  0.19450E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13582
   Nb of faces within the viscous sub-layer     :      10912
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13598E+02      47   0.86401E-01   0.32450E+02 0.27180E+02 
c  Velocity[X]                                      0.51830E+01 
c  Velocity[Y]                                      0.11280E+02 
c  Velocity[Z]                                      0.15988E+02 
c  Pressure     0.84690E-01     324   0.28119E-01   0.81520E-01 0.85974E+00 
c  k            0.54056E+00      21   0.17540E-03   0.11025E-01 0.21505E+02 
c  epsilon      0.53731E+04      11   0.16518E-03   0.21488E+07 0.47235E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                -0.11125                             1
a  Local Time Step      2.3337e-08                        281079


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.4551           15.19           1.823         0.30205
v  Velocity[Y]             -30.021          32.579          1.0556         0.73302
v  Velocity[Z]             -41.953          40.225        -0.90259      -0.0070891
v  ǁVelocityǁ            0.0060822          45.778          6.2313          6.3028
v  Pressure                 -76849      2.3192e+05      1.4312e+05      1.2205e+05
v  k                    2.4012e-06          11.498        0.078428        0.076304
v  epsilon                0.016637      2.3059e+06          2847.6          54.417
v  TurbVisc             4.4164e-12         0.41838       0.0025885        0.037784
v  CourantNb              0.013612           42850          41.866          7.1934
v  FourierNb               0.02311      2.3655e+05          21.914         0.32552
v  total_pressure       4.2315e+05      7.3192e+05      6.4312e+05      6.2205e+05
v  Local Time Step           0.001        0.023823       0.0010017       0.0010114


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54755      2.3938e+05           63.78          7.5189


 TIME FOR THE TIME STEP              596:        0.62152E+02

===============================================================


 INSTANT    0.597000000E+01   TIME STEP NUMBER             597
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.247210997E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271216084E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59256E+02 0.87600E+01
   Friction velocity        uet   :  0.34945E-01 0.17327E+02
   Friction velocity        uk    :  0.41694E-01 0.17327E+02
   Dimensionless distance   yplus :  0.72799E-03 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13587
   Nb of faces within the viscous sub-layer     :      10927
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13602E+02      48   0.88505E-01   0.32381E+02 0.27162E+02 
c  Velocity[X]                                      0.51959E+01 
c  Velocity[Y]                                      0.10821E+02 
c  Velocity[Z]                                      0.16364E+02 
c  Pressure     0.83375E-01     318   0.27402E-01   0.80254E-01 0.80716E+00 
c  k            0.54042E+00      22   0.68333E-04   0.78370E-02 0.18596E+02 
c  epsilon      0.53804E+04      12   0.33263E-03   0.71322E+07 0.85935E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon               -0.050056                             1
a  Local Time Step        2.37e-08                        281063


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6005          18.954          1.8236         0.30184
v  Velocity[Y]             -30.909          30.793           1.046         0.73343
v  Velocity[Z]             -56.601          32.551         -0.9072      -0.0072905
v  ǁVelocityǁ             0.010906           62.17          6.2277           6.302
v  Pressure                 -77796      2.3189e+05       1.431e+05      1.2204e+05
v  k                    3.1144e-06          11.597        0.078509        0.076259
v  epsilon                 0.01679      2.2979e+06          2859.5          54.346
v  TurbVisc             4.0491e-12         0.41838       0.0025897        0.037786
v  CourantNb              0.062053           42194          41.848          7.1912
v  FourierNb               0.02312      2.3655e+05          21.915          0.3257
v  total_pressure        4.222e+05      7.3189e+05       6.431e+05      6.2204e+05
v  Local Time Step           0.001        0.021337       0.0010017       0.0010115


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82536      2.4002e+05          63.763          7.5169


 TIME FOR THE TIME STEP              597:        0.70411E+02

===============================================================


 INSTANT    0.598000000E+01   TIME STEP NUMBER             598
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.390834108E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271229769E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87074E+02 0.91068E+01
   Friction velocity        uet   :  0.32035E-01 0.19091E+02
   Friction velocity        uk    :  0.34799E-01 0.19091E+02
   Dimensionless distance   yplus :  0.24360E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13570
   Nb of faces within the viscous sub-layer     :      10928
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13603E+02      54   0.89721E-01   0.34132E+02 0.27874E+02 
c  Velocity[X]                                      0.53422E+01 
c  Velocity[Y]                                      0.11938E+02 
c  Velocity[Z]                                      0.16852E+02 
c  Pressure     0.85611E-01     507   0.27998E-01   0.82267E-01 0.95281E+00 
c  k            0.54089E+00      23   0.10250E-03   0.80326E-02 0.18632E+02 
c  epsilon      0.53847E+04      13   0.22054E-03   0.39671E+07 0.64242E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011102                             1
a  epsilon                -0.68528                             2
a  Local Time Step      2.3738e-08                        281075


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5665          15.267          1.8241         0.30183
v  Velocity[Y]             -35.066          34.631           1.039         0.73404
v  Velocity[Z]             -41.887          32.643        -0.91244       -0.007501
v  ǁVelocityǁ             0.014267          44.709          6.2292          6.3017
v  Pressure                 -78405      2.3184e+05      1.4306e+05      1.2201e+05
v  k                    2.2673e-06          11.128        0.078394        0.076228
v  epsilon                0.016968      2.3819e+06          2853.4          54.239
v  TurbVisc             5.0376e-12         0.41838       0.0025905        0.037786
v  CourantNb              0.020076           42126          41.834          7.1897
v  FourierNb              0.023132      2.3655e+05          21.915         0.32567
v  total_pressure       4.2159e+05      7.3184e+05      6.4306e+05      6.2201e+05
v  Local Time Step           0.001        0.022626       0.0010017       0.0010116


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96606      2.3895e+05          63.749          7.5153


 TIME FOR THE TIME STEP              598:        0.88383E+02

===============================================================


 INSTANT    0.599000000E+01   TIME STEP NUMBER             599
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.238638729E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271272547E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56836E+02 0.92475E+01
   Friction velocity        uet   :  0.32801E-01 0.18971E+02
   Friction velocity        uk    :  0.41449E-01 0.18971E+02
   Dimensionless distance   yplus :  0.23797E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13562
   Nb of faces within the viscous sub-layer     :      10907
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13601E+02      53   0.89511E-01   0.34090E+02 0.27824E+02 
c  Velocity[X]                                      0.54237E+01 
c  Velocity[Y]                                      0.11990E+02 
c  Velocity[Z]                                      0.16676E+02 
c  Pressure     0.84899E-01     642   0.27960E-01   0.81514E-01 0.18308E+01 
c  k            0.54142E+00      19   0.14078E-03   0.66259E-02 0.16369E+02 
c  epsilon      0.53633E+04      12   0.19905E-03   0.21650E+07 0.47512E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.1389e-05                             1
a  epsilon                -0.14094                             1
a  Local Time Step      2.3143e-08                        281075


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5439          19.086          1.8253         0.30167
v  Velocity[Y]             -33.615          30.709          1.0348         0.73442
v  Velocity[Z]             -57.178          32.189        -0.91905       -0.007183
v  ǁVelocityǁ            0.0044249           62.83          6.2339          6.3007
v  Pressure                 -78915      2.3155e+05       1.428e+05      1.2177e+05
v  k                     2.395e-06          10.999        0.078466        0.076206
v  epsilon                0.017237      2.2591e+06          2846.6          54.218
v  TurbVisc             3.7736e-12         0.41838       0.0025916        0.037787
v  CourantNb             0.0018555           43209          41.863          7.1893
v  FourierNb              0.023147      2.3655e+05          21.913         0.32562
v  total_pressure       4.2109e+05      7.3155e+05       6.428e+05      6.2177e+05
v  Local Time Step           0.001        0.022052       0.0010017       0.0010117


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.49381      2.3852e+05          63.776          7.5149


 TIME FOR THE TIME STEP              599:        0.92217E+02

===============================================================


 INSTANT    0.600000000E+01   TIME STEP NUMBER             600
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.365778830E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271205279E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87947E+02 0.96213E+01
   Friction velocity        uet   :  0.33464E-01 0.13653E+02
   Friction velocity        uk    :  0.55401E-01 0.13653E+02
   Dimensionless distance   yplus :  0.54291E-03 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13557
   Nb of faces within the viscous sub-layer     :      10932
   Total number of wall faces                   :      41000
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        600, Physical time    0.60000E+01


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint/main
 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                            
  Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary
 End writing


 Time for restart files:    0.15606E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13602E+02      57   0.88978E-01   0.33984E+02 0.27811E+02 
c  Velocity[X]                                      0.54266E+01 
c  Velocity[Y]                                      0.12193E+02 
c  Velocity[Z]                                      0.16364E+02 
c  Pressure     0.85852E-01     551   0.28337E-01   0.82295E-01 0.11748E+01 
c  k            0.54276E+00      18   0.13740E-03   0.54876E-02 0.14942E+02 
c  epsilon      0.54024E+04      11   0.20479E-03   0.21496E+07 0.46989E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                -0.19468                             1
a  Local Time Step      2.3618e-08                        281075


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5266          15.149          1.8249         0.30139
v  Velocity[Y]             -32.039          36.925           1.038         0.73495
v  Velocity[Z]             -41.391          33.616        -0.92687      -0.0066407
v  ǁVelocityǁ            0.0043347          44.421          6.2393          6.2996
v  Pressure                 -79274      2.3149e+05      1.4279e+05      1.2171e+05
v  k                    2.6975e-06          10.835        0.078602        0.076191
v  epsilon                0.017635      2.3874e+06          2864.8          54.198
v  TurbVisc             4.0102e-12         0.41838       0.0025931        0.037789
v  CourantNb              0.038424           42341          41.921          7.1887
v  FourierNb              0.023165      2.3655e+05          21.913          0.3257
v  total_pressure       4.2073e+05      7.3149e+05      6.4279e+05      6.2171e+05
v  Local Time Step           0.001        0.022777       0.0010017        0.001012


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69316      2.3817e+05          63.834          7.5144


 TIME FOR THE TIME STEP              600:        0.90742E+02

===============================================================


 INSTANT    0.601000000E+01   TIME STEP NUMBER             601
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.266169228E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.271102885E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60306E+02 0.99055E+01
   Friction velocity        uet   :  0.33441E-01 0.20437E+02
   Friction velocity        uk    :  0.44307E-01 0.20437E+02
   Dimensionless distance   yplus :  0.26077E-02 0.20255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13542
   Nb of faces within the viscous sub-layer     :      10895
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13716E+02      50   0.88534E-01   0.45586E+03 0.93783E+02 
c  Velocity[X]                                      0.22365E+02 
c  Velocity[Y]                                      0.46338E+02 
c  Velocity[Z]                                      0.38715E+03 
c  Pressure     0.91268E-01    1471   0.19249E+00   0.87406E-01 0.48888E+03 
c  k            0.68054E+00      24   0.13237E-02   0.46334E+00 0.12907E+03 
c  epsilon      0.53923E+04      17   0.40393E-03   0.37726E+07 0.62909E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon        
a  Local Time Step      2.3482e-08                        281097


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.468          22.275          1.9428         0.33826
v  Velocity[Y]             -33.137          34.677          1.1856         0.81624
v  Velocity[Z]             -59.381          33.332         -0.9627     -0.00074298
v  ǁVelocityǁ             0.033894          66.525          6.4824          6.8611
v  Pressure                -139.68      4.7911e+05      2.7707e+05      2.5362e+05
v  k                     2.319e-06          10.931        0.079351         0.08073
v  epsilon                 0.01803      2.2516e+06          2876.7          55.398
v  TurbVisc             4.4626e-12         0.41838       0.0025942        0.037791
v  CourantNb             0.0046518           42586          42.021          7.1873
v  FourierNb              0.023183      2.3655e+05          21.914         0.32575
v  total_pressure       4.9986e+05      9.7911e+05      7.7707e+05      7.5362e+05
v  Local Time Step           0.001        0.022236       0.0010017       0.0010121


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.92412       2.413e+05          63.935           7.513


 TIME FOR THE TIME STEP              601:        0.12761E+03

===============================================================


 INSTANT    0.602000000E+01   TIME STEP NUMBER             602
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.260573653E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312857781E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98242E+02 0.10102E+02
   Friction velocity        uet   :  0.34573E-01 0.23759E+02
   Friction velocity        uk    :  0.39421E-01 0.23759E+02
   Dimensionless distance   yplus :  0.30316E-02 0.21590E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14109
   Nb of faces within the viscous sub-layer     :      10722
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16502E+02      85   0.85393E-01   0.22076E+03 0.62606E+02 
c  Velocity[X]                                      0.25586E+02 
c  Velocity[Y]                                      0.46809E+02 
c  Velocity[Z]                                      0.14837E+03 
c  Pressure     0.23576E+00    1534   0.75801E-01   0.22007E+00 0.17155E+03 
c  k            0.72694E+00      23   0.42362E-03   0.20608E+00 0.80006E+02 
c  epsilon      0.62675E+04      18   0.20257E-02   0.17444E+09 0.36646E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon               -0.090513                             1
a  Local Time Step      2.5752e-08                        281148


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.0227          16.292          2.0075         0.35391
v  Velocity[Y]             -31.657          40.317          1.2814         0.86007
v  Velocity[Z]             -49.528          33.499        -0.94874        0.010976
v  ǁVelocityǁ              0.01594          52.789          6.6203          7.1719
v  Pressure                -4250.9      3.9636e+05      2.4155e+05      2.1334e+05
v  k                    2.4141e-06          11.219        0.083265        0.085075
v  epsilon                0.018297      4.6072e+06            3372          59.378
v  TurbVisc             3.8351e-12         0.48035       0.0026665        0.039424
v  CourantNb              0.035331           38832          44.078          7.8842
v  FourierNb              0.023209      2.3655e+05          21.915         0.32783
v  total_pressure       4.9575e+05      8.9636e+05      7.4155e+05      7.1334e+05
v  Local Time Step           0.001         0.02446       0.0010011       0.0010077


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4985      2.4007e+05          65.993          8.2121


 TIME FOR THE TIME STEP              602:        0.15728E+03

===============================================================


 INSTANT    0.603000000E+01   TIME STEP NUMBER             603
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.353420074E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313121840E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.82114E+02 0.99360E+01
   Friction velocity        uet   :  0.39417E-01 0.36366E+02
   Friction velocity        uk    :  0.38969E-01 0.36366E+02
   Dimensionless distance   yplus :  0.46403E-02 0.22864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14247
   Nb of faces within the viscous sub-layer     :      10576
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16679E+02      75   0.85337E-01   0.80120E+02 0.37466E+02 
c  Velocity[X]                                      0.16137E+02 
c  Velocity[Y]                                      0.32729E+02 
c  Velocity[Z]                                      0.31254E+02 
c  Pressure     0.15804E+00    1576   0.11882E+00   0.14414E+00 0.31201E+03 
c  k            0.74915E+00      23   0.30645E-03   0.99204E-01 0.52643E+02 
c  epsilon      0.61620E+04      17   0.97535E-03   0.13190E+09 0.34363E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -9.9207                             5
a  Local Time Step      2.0488e-08                        281174


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.2526          17.697          2.0369         0.35351
v  Velocity[Y]             -32.086          38.329          1.2933         0.86356
v  Velocity[Z]             -50.071          38.394        -0.97001       0.0034509
v  ǁVelocityǁ            0.0090309          55.864           6.704          7.2145
v  Pressure                 -63860      2.9187e+05      1.8708e+05      1.5645e+05
v  k                    2.2886e-06          11.327        0.082963        0.088214
v  epsilon                0.018367      2.4242e+06          3154.1          60.261
v  TurbVisc             4.1453e-12         0.49311       0.0027001         0.04035
v  CourantNb               0.10532           48809          44.519          7.9391
v  FourierNb              0.023231      2.3655e+05          21.916         0.32892
v  total_pressure       4.3614e+05      7.9187e+05      6.8708e+05      6.5645e+05
v  Local Time Step           0.001        0.015022       0.0010011       0.0010077


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.53867      2.4477e+05          66.435          8.2681


 TIME FOR THE TIME STEP              603:        0.16907E+03

===============================================================


 INSTANT    0.604000000E+01   TIME STEP NUMBER             604
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.729809233E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312983535E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.81539E+02 0.10671E+02
   Friction velocity        uet   :  0.28049E-01 0.35617E+02
   Friction velocity        uk    :  0.28001E-01 0.35617E+02
   Dimensionless distance   yplus :  0.45447E-02 0.23331E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14338
   Nb of faces within the viscous sub-layer     :      10457
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16101E+02      75   0.88552E-01   0.75799E+02 0.36653E+02 
c  Velocity[X]                                      0.13078E+02 
c  Velocity[Y]                                      0.30248E+02 
c  Velocity[Z]                                      0.32474E+02 
c  Pressure     0.18389E+00    1783   0.84806E-01   0.16421E+00 0.11715E+03 
c  k            0.76611E+00      22   0.14358E-03   0.56960E-01 0.39099E+02 
c  epsilon      0.64441E+04      18   0.14943E-02   0.13463E+09 0.32116E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -7.7432                             3
a  Local Time Step      2.0824e-08                        281208


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7805          19.007          2.0483         0.35035
v  Velocity[Y]             -33.154          41.867           1.254         0.85342
v  Velocity[Z]             -53.867          37.718        -0.99796      -0.0080976
v  ǁVelocityǁ             0.011116          58.719          6.7489          7.1699
v  Pressure                 -85475      2.7317e+05      1.6787e+05      1.3715e+05
v  k                    2.2858e-06          11.079         0.08455        0.090657
v  epsilon                0.018561      4.7371e+06          3432.6          61.551
v  TurbVisc             3.8309e-12         0.49459       0.0027244        0.041048
v  CourantNb              0.013856           48021          44.923          7.9785
v  FourierNb              0.023248      2.3655e+05          21.916         0.32957
v  total_pressure       4.1453e+05      7.7317e+05      6.6787e+05      6.3715e+05
v  Local Time Step           0.001        0.016524       0.0010011       0.0010076


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40532      2.4161e+05          66.839          8.3081


 TIME FOR THE TIME STEP              604:        0.16748E+03

===============================================================


 INSTANT    0.605000000E+01   TIME STEP NUMBER             605
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.234298292E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313155040E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87488E+02 0.11218E+02
   Friction velocity        uet   :  0.31420E-01 0.33620E+02
   Friction velocity        uk    :  0.41479E-01 0.33620E+02
   Dimensionless distance   yplus :  0.42899E-02 0.23467E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14361
   Nb of faces within the viscous sub-layer     :      10345
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15747E+02      76   0.92232E-01   0.69158E+02 0.35099E+02 
c  Velocity[X]                                      0.11930E+02 
c  Velocity[Y]                                      0.28135E+02 
c  Velocity[Z]                                      0.29093E+02 
c  Pressure     0.16073E+00    1309   0.57967E-01   0.14113E+00 0.25572E+02 
c  k            0.77701E+00      27   0.17858E-03   0.41920E-01 0.32692E+02 
c  epsilon      0.65286E+04      14   0.91071E-03   0.74729E+08 0.24791E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.0384e-06                             1
a  epsilon                 -15.498                             9
a  Local Time Step      2.1305e-08                        281239


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8329          18.218          2.0479         0.34843
v  Velocity[Y]             -33.518          33.279          1.2139         0.84638
v  Velocity[Z]             -55.202          38.226         -1.0082      -0.0093962
v  ǁVelocityǁ              0.01571          60.748          6.7777          7.1402
v  Pressure                 -83671      2.7741e+05      1.7097e+05      1.4114e+05
v  k                    2.3425e-06          11.627        0.084975        0.092601
v  epsilon                0.018701       2.737e+06          3339.7          62.357
v  TurbVisc             3.9191e-12         0.49479       0.0027517        0.041686
v  CourantNb              0.012563           46937          45.319          8.0094
v  FourierNb              0.023263      2.3655e+05          21.917         0.33026
v  total_pressure       4.1633e+05      7.7741e+05      6.7097e+05      6.4114e+05
v  Local Time Step           0.001        0.018176       0.0010011       0.0010076


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.2401      2.4572e+05          67.237          8.3397


 TIME FOR THE TIME STEP              605:        0.13210E+03

===============================================================


 INSTANT    0.606000000E+01   TIME STEP NUMBER             606
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.678951719E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312621011E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93688E+02 0.98572E+01
   Friction velocity        uet   :  0.37035E-01 0.33898E+02
   Friction velocity        uk    :  0.46471E-01 0.33898E+02
   Dimensionless distance   yplus :  0.43254E-02 0.23590E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14387
   Nb of faces within the viscous sub-layer     :      10291
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15694E+02      82   0.93220E-01   0.68061E+02 0.34735E+02 
c  Velocity[X]                                      0.12133E+02 
c  Velocity[Y]                                      0.27877E+02 
c  Velocity[Z]                                      0.28052E+02 
c  Pressure     0.14608E+00    1434   0.53503E-01   0.12606E+00 0.59054E+02 
c  k            0.78049E+00      26   0.44441E-03   0.67817E-01 0.41552E+02 
c  epsilon      0.67106E+04      15   0.10412E-02   0.61995E+08 0.21648E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0015135                             3
a  epsilon                 -7.8059                             4
a  Local Time Step      2.1859e-08                        281269


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.0373          19.858          2.0526           0.349
v  Velocity[Y]             -37.511          44.834          1.1911         0.84528
v  Velocity[Z]             -56.086          32.594         -1.0134       -0.008725
v  ǁVelocityǁ             0.019213          60.621          6.8106          7.1483
v  Pressure                 -73240      2.8908e+05      1.8144e+05       1.516e+05
v  k                    2.3855e-06          12.541        0.086566        0.094217
v  epsilon                 0.01901      3.4776e+06          3551.2          63.105
v  TurbVisc             3.9866e-12         0.49483       0.0027858        0.042293
v  CourantNb              0.042178           45748          45.575          8.0289
v  FourierNb              0.023277      2.3655e+05          21.921         0.33115
v  total_pressure       4.2676e+05      7.8908e+05      6.8144e+05       6.516e+05
v  Local Time Step           0.001        0.019994       0.0010011       0.0010078


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51075      2.4483e+05          67.497          8.3601


 TIME FOR THE TIME STEP              606:        0.14263E+03

===============================================================


 INSTANT    0.607000000E+01   TIME STEP NUMBER             607
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.996971320E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313130464E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10210E+03 0.82559E+01
   Friction velocity        uet   :  0.35579E-01 0.32620E+02
   Friction velocity        uk    :  0.50588E-01 0.32620E+02
   Dimensionless distance   yplus :  0.36689E-02 0.23749E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14423
   Nb of faces within the viscous sub-layer     :      10260
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15790E+02      79   0.97905E-01   0.66431E+02 0.34290E+02 
c  Velocity[X]                                      0.11647E+02 
c  Velocity[Y]                                      0.26322E+02 
c  Velocity[Z]                                      0.28462E+02 
c  Pressure     0.14200E+00    1251   0.49799E-01   0.12079E+00 0.26158E+02 
c  k            0.77911E+00      22   0.37632E-03   0.64657E-01 0.40296E+02 
c  epsilon      0.69208E+04      16   0.14522E-02   0.83715E+08 0.24462E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                -0.70058                             2
a  Local Time Step      2.2491e-08                        281301


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.941          18.991          2.0561         0.34882
v  Velocity[Y]             -35.051          46.759          1.1801         0.84624
v  Velocity[Z]             -61.778          33.997         -1.0173      -0.0055037
v  ǁVelocityǁ             0.019158           67.67          6.8412          7.1676
v  Pressure                 -70596      2.9479e+05      1.8612e+05      1.5614e+05
v  k                    2.4328e-06          13.421        0.087518        0.095615
v  epsilon               0.0027738      4.3911e+06          3630.2          63.799
v  TurbVisc             4.0502e-12         0.49485       0.0028191        0.042863
v  CourantNb              0.026689           44463           45.86           8.058
v  FourierNb              0.023291      2.3655e+05          21.926         0.33197
v  total_pressure        4.294e+05      7.9479e+05      6.8612e+05      6.5614e+05
v  Local Time Step           0.001        0.019504       0.0010011       0.0010078


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65937      2.4235e+05          67.786            8.39


 TIME FOR THE TIME STEP              607:        0.11845E+03

===============================================================


 INSTANT    0.608000000E+01   TIME STEP NUMBER             608
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.847860865E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312890339E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11297E+03 0.68490E+01
   Friction velocity        uet   :  0.33768E-01 0.27843E+02
   Friction velocity        uk    :  0.52031E-01 0.27843E+02
   Dimensionless distance   yplus :  0.35528E-02 0.23819E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14490
   Nb of faces within the viscous sub-layer     :      10197
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15851E+02      82   0.94269E-01   0.65784E+02 0.33907E+02 
c  Velocity[X]                                      0.10543E+02 
c  Velocity[Y]                                      0.26067E+02 
c  Velocity[Z]                                      0.29175E+02 
c  Pressure     0.13860E+00    1292   0.46331E-01   0.11609E+00 0.93305E+01 
c  k            0.77980E+00      24   0.22701E-03   0.42019E-01 0.32293E+02 
c  epsilon      0.71200E+04      16   0.12223E-02   0.66394E+08 0.21382E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                  -5.562                             2
a  Local Time Step      2.2598e-08                        281307


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.0517          20.181          2.0598         0.34837
v  Velocity[Y]             -38.648           43.53          1.1743         0.84798
v  Velocity[Z]             -60.221          33.209           -1.03      -0.0046789
v  ǁVelocityǁ             0.019441          64.068           6.872          7.1865
v  Pressure                 -71715      2.9748e+05      1.8791e+05      1.5757e+05
v  k                    2.9043e-06          13.341         0.08871        0.096833
v  epsilon                0.020001      3.7703e+06          3738.4          64.464
v  TurbVisc             4.2616e-12         0.49486       0.0028514        0.043388
v  CourantNb              0.005771           44252          46.061          8.0794
v  FourierNb              0.023305      2.3655e+05          21.933         0.33273
v  total_pressure       4.2828e+05      7.9748e+05      6.8791e+05      6.5757e+05
v  Local Time Step           0.001        0.021455       0.0010011       0.0010079


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67588      2.3807e+05          67.994          8.4121


 TIME FOR THE TIME STEP              608:        0.13315E+03

===============================================================


 INSTANT    0.609000000E+01   TIME STEP NUMBER             609
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.390342014E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312944754E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11512E+03 0.67686E+01
   Friction velocity        uet   :  0.34644E-01 0.28636E+02
   Friction velocity        uk    :  0.52434E-01 0.28636E+02
   Dimensionless distance   yplus :  0.36540E-02 0.23848E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14532
   Nb of faces within the viscous sub-layer     :      10197
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15875E+02      82   0.94762E-01   0.65141E+02 0.33798E+02 
c  Velocity[X]                                      0.10249E+02 
c  Velocity[Y]                                      0.25022E+02 
c  Velocity[Z]                                      0.29869E+02 
c  Pressure     0.13681E+00     786   0.44503E-01   0.11317E+00 0.32501E+01 
c  k            0.78127E+00      21   0.13872E-03   0.27979E-01 0.26211E+02 
c  epsilon      0.72077E+04      13   0.20440E-02   0.47716E+08 0.17976E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0012596                             5
a  epsilon                 -29.984                            14
a  Local Time Step      2.2916e-08                        281333


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.982          18.852          2.0607         0.34762
v  Velocity[Y]             -37.606          34.116          1.1682         0.84891
v  Velocity[Z]             -61.926          38.234         -1.0423      -0.0055052
v  ǁVelocityǁ             0.023073          67.665          6.8985          7.1994
v  Pressure                 -74622      2.9816e+05      1.8785e+05      1.5737e+05
v  k                    2.1637e-06          13.212        0.089292        0.097874
v  epsilon                0.020132      3.0082e+06          3780.1           64.99
v  TurbVisc             4.1773e-12         0.49486       0.0028804        0.043868
v  CourantNb              0.011253           43637          46.284          8.1025
v  FourierNb              0.023321      2.3655e+05          21.937         0.33338
v  total_pressure       4.2538e+05      7.9816e+05      6.8785e+05      6.5737e+05
v  Local Time Step           0.001         0.02123        0.001001       0.0010078


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.33236      2.4003e+05          68.222          8.4359


 TIME FOR THE TIME STEP              609:        0.11444E+03

===============================================================


 INSTANT    0.610000000E+01   TIME STEP NUMBER             610
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.599426202E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312954217E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11409E+03 0.67867E+01
   Friction velocity        uet   :  0.33031E-01 0.23357E+02
   Friction velocity        uk    :  0.34975E-01 0.23357E+02
   Dimensionless distance   yplus :  0.29803E-02 0.23859E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14588
   Nb of faces within the viscous sub-layer     :      10184
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15887E+02      82   0.96931E-01   0.58902E+02 0.32062E+02 
c  Velocity[X]                                      0.95242E+01 
c  Velocity[Y]                                      0.23188E+02 
c  Velocity[Z]                                      0.26190E+02 
c  Pressure     0.13077E+00    1067   0.41564E-01   0.10663E+00 0.25707E+01 
c  k            0.78247E+00      23   0.12793E-03   0.31039E-01 0.27498E+02 
c  epsilon      0.72256E+04      15   0.12507E-02   0.24072E+08 0.12841E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                -0.19135                             2
a  Local Time Step      2.3299e-08                        281357


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.0812           18.71          2.0619         0.34712
v  Velocity[Y]             -31.285          43.031          1.1606         0.84935
v  Velocity[Z]             -55.468          36.045         -1.0563      -0.0061169
v  ǁVelocityǁ            0.0094994           60.26          6.9247          7.2095
v  Pressure                 -77349      2.9841e+05      1.8753e+05      1.5718e+05
v  k                    2.8361e-06           13.23        0.089802        0.098771
v  epsilon                0.021136      2.9697e+06          3768.2           65.44
v  TurbVisc             4.0038e-12         0.49487       0.0029041        0.044304
v  CourantNb              0.045271           42920           46.39          8.1216
v  FourierNb               0.02334      2.3655e+05          21.939         0.33405
v  total_pressure       4.2265e+05      7.9841e+05      6.8753e+05      6.5718e+05
v  Local Time Step           0.001        0.016098        0.001001       0.0010077


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7936      2.3991e+05          68.329          8.4557


 TIME FOR THE TIME STEP              610:        0.11243E+03

===============================================================


 INSTANT    0.611000000E+01   TIME STEP NUMBER             611
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.864800188E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312949035E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97381E+02 0.67907E+01
   Friction velocity        uet   :  0.15422E-01 0.26278E+02
   Friction velocity        uk    :  0.30003E-01 0.26278E+02
   Dimensionless distance   yplus :  0.33531E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14599
   Nb of faces within the viscous sub-layer     :      10135
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15884E+02      81   0.10093E+00   0.56890E+02 0.31446E+02 
c  Velocity[X]                                      0.92305E+01 
c  Velocity[Y]                                      0.22067E+02 
c  Velocity[Z]                                      0.25592E+02 
c  Pressure     0.13065E+00     602   0.40402E-01   0.10552E+00 0.20112E+01 
c  k            0.78378E+00      22   0.16919E-03   0.42184E-01 0.31895E+02 
c  epsilon      0.72458E+04      15   0.43327E-03   0.13989E+08 0.97266E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -6.2865                             3
a  Local Time Step      2.3007e-08                        281365


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.0377          19.926          2.0623         0.34676
v  Velocity[Y]             -32.208          34.796          1.1523         0.84926
v  Velocity[Z]             -65.354           35.69         -1.0631      -0.0062338
v  ǁVelocityǁ             0.017935           71.26           6.948          7.2176
v  Pressure                 -79234      2.9871e+05      1.8747e+05      1.5726e+05
v  k                    2.6613e-06          13.022         0.09044        0.099578
v  epsilon                0.013647      2.9652e+06          3806.3          65.932
v  TurbVisc             4.1486e-12         0.49487       0.0029241        0.044698
v  CourantNb              0.022595           43465          46.563          8.1406
v  FourierNb              0.023362      2.3655e+05           21.94          0.3346
v  total_pressure       4.2077e+05      7.9871e+05      6.8747e+05      6.5726e+05
v  Local Time Step           0.001        0.016761        0.001001       0.0010079


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88016       2.414e+05          68.502          8.4752


 TIME FOR THE TIME STEP              611:        0.93649E+02

===============================================================


 INSTANT    0.612000000E+01   TIME STEP NUMBER             612
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.765831270E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312896666E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12474E+03 0.68265E+01
   Friction velocity        uet   :  0.39170E-01 0.20271E+02
   Friction velocity        uk    :  0.49431E-01 0.20271E+02
   Dimensionless distance   yplus :  0.20553E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14642
   Nb of faces within the viscous sub-layer     :      10100
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15882E+02      83   0.98972E-01   0.58534E+02 0.31909E+02 
c  Velocity[X]                                      0.92536E+01 
c  Velocity[Y]                                      0.21386E+02 
c  Velocity[Z]                                      0.27895E+02 
c  Pressure     0.12737E+00     630   0.38583E-01   0.10175E+00 0.21110E+01 
c  k            0.78555E+00      30   0.27660E-03   0.70734E-01 0.41044E+02 
c  epsilon      0.72614E+04      13   0.27033E-03   0.87897E+07 0.76967E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon               -0.036939                             1
a  Local Time Step      2.2947e-08                        281335


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.0789          19.951          2.0667          0.3468
v  Velocity[Y]             -36.206          41.709           1.149           0.849
v  Velocity[Z]             -56.629          34.263         -1.0709      -0.0050986
v  ǁVelocityǁ             0.015474          61.629          6.9748          7.2245
v  Pressure                 -80499      2.9899e+05      1.8746e+05       1.574e+05
v  k                     3.211e-06           13.15        0.090981         0.10033
v  epsilon                0.021717       3.006e+06          3816.5          66.492
v  TurbVisc             4.4481e-12         0.49488       0.0029455        0.045057
v  CourantNb              0.027642           43580          46.715          8.1566
v  FourierNb              0.023383      2.3655e+05          21.941         0.33506
v  total_pressure        4.195e+05      7.9899e+05      6.8746e+05       6.574e+05
v  Local Time Step           0.001        0.012891       0.0010011       0.0010079


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58474      2.4199e+05          68.656          8.4916


 TIME FOR THE TIME STEP              612:        0.85361E+02

===============================================================


 INSTANT    0.613000000E+01   TIME STEP NUMBER             613
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.123589898E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312754546E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10327E+03 0.68260E+01
   Friction velocity        uet   :  0.39709E-01 0.26493E+02
   Friction velocity        uk    :  0.55308E-01 0.26493E+02
   Dimensionless distance   yplus :  0.16872E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14639
   Nb of faces within the viscous sub-layer     :      10084
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15872E+02      69   0.10109E+00   0.58968E+02 0.31942E+02 
c  Velocity[X]                                      0.90395E+01 
c  Velocity[Y]                                      0.21270E+02 
c  Velocity[Z]                                      0.28659E+02 
c  Pressure     0.12679E+00     861   0.37970E-01   0.10066E+00 0.50767E+01 
c  k            0.78781E+00      22   0.47219E-03   0.12715E+00 0.54506E+02 
c  epsilon      0.72847E+04      14   0.65597E-03   0.16104E+08 0.10344E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -6.3436                             4
a  Local Time Step       2.343e-08                        281337


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.9634          19.238          2.0691         0.34673
v  Velocity[Y]             -34.901          38.065          1.1485         0.84876
v  Velocity[Z]             -66.051          44.664          -1.077      -0.0050506
v  ǁVelocityǁ             0.015649           71.95          6.9998          7.2317
v  Pressure                 -80532      3.0009e+05      1.8846e+05      1.5829e+05
v  k                    3.8907e-06           13.56        0.091727         0.10105
v  epsilon               0.0042041      2.9894e+06          3864.4          67.127
v  TurbVisc             4.7203e-12         0.49488       0.0029686        0.045384
v  CourantNb              0.029439           42680          46.923          8.1717
v  FourierNb                0.0234      2.3656e+05          21.943         0.33585
v  total_pressure       4.1947e+05      8.0009e+05      6.8846e+05      6.5829e+05
v  Local Time Step           0.001        0.013383       0.0010011       0.0010082


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54949      2.3989e+05          68.866          8.5075


 TIME FOR THE TIME STEP              613:        0.10206E+03

===============================================================


 INSTANT    0.614000000E+01   TIME STEP NUMBER             614
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.206421540E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312744126E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12787E+03 0.68130E+01
   Friction velocity        uet   :  0.36822E-01 0.28276E+02
   Friction velocity        uk    :  0.58173E-01 0.28276E+02
   Dimensionless distance   yplus :  0.23637E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14656
   Nb of faces within the viscous sub-layer     :      10074
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15876E+02      63   0.99577E-01   0.58607E+02 0.31844E+02 
c  Velocity[X]                                      0.93385E+01 
c  Velocity[Y]                                      0.21382E+02 
c  Velocity[Z]                                      0.27886E+02 
c  Pressure     0.12615E+00     596   0.37103E-01   0.99368E-01 0.16097E+01 
c  k            0.79173E+00      28   0.86635E-03   0.22502E+00 0.71155E+02 
c  epsilon      0.73281E+04      13   0.51145E-03   0.89501E+07 0.76636E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0020557                             5
a  epsilon                 -43.661                             5
a  Local Time Step      2.3527e-08                        281352


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.9881          18.631          2.0758         0.34694
v  Velocity[Y]             -40.375          41.198          1.1538         0.84822
v  Velocity[Z]             -59.248          36.139         -1.0829      -0.0044544
v  ǁVelocityǁ             0.014811          64.172          7.0245          7.2373
v  Pressure                 -81237      3.0011e+05      1.8851e+05      1.5835e+05
v  k                    1.2386e-06          13.889        0.092139         0.10179
v  epsilon                0.016947      2.9754e+06          3851.9           67.93
v  TurbVisc             5.3392e-12         0.49488       0.0029948        0.045681
v  CourantNb             0.0040035           42504          47.106          8.1864
v  FourierNb              0.023402      2.3656e+05          21.946         0.33632
v  total_pressure       4.1876e+05      8.0011e+05      6.8851e+05      6.5835e+05
v  Local Time Step           0.001        0.012339       0.0010011       0.0010082


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57857      2.3872e+05          69.052          8.5227


 TIME FOR THE TIME STEP              614:        0.90665E+02

===============================================================


 INSTANT    0.615000000E+01   TIME STEP NUMBER             615
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.479748937E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312657731E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10878E+03 0.67767E+01
   Friction velocity        uet   :  0.32777E-01 0.33258E+02
   Friction velocity        uk    :  0.39279E-01 0.33258E+02
   Dimensionless distance   yplus :  0.33036E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14677
   Nb of faces within the viscous sub-layer     :      10008
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15868E+02      66   0.99301E-01   0.57501E+02 0.31556E+02 
c  Velocity[X]                                      0.92819E+01 
c  Velocity[Y]                                      0.22150E+02 
c  Velocity[Z]                                      0.26069E+02 
c  Pressure     0.12395E+00     934   0.36261E-01   0.97229E-01 0.34223E+01 
c  k            0.79735E+00      30   0.14243E-02   0.30969E+00 0.81938E+02 
c  epsilon      0.74007E+04      14   0.88875E-03   0.31261E+08 0.14039E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -5.2975                             4
a  Local Time Step      2.2988e-08                        281352


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8176          19.285          2.0828         0.34708
v  Velocity[Y]             -36.947          32.956          1.1612         0.84765
v  Velocity[Z]             -64.837          35.577         -1.0894      -0.0044284
v  ǁVelocityǁ             0.011322          70.889          7.0468          7.2439
v  Pressure                 -81406      3.0088e+05      1.8915e+05      1.5891e+05
v  k                    2.9466e-06          14.182        0.093359         0.10251
v  epsilon                0.010036      3.3334e+06            3938          68.968
v  TurbVisc             1.6733e-12         0.49488       0.0030236        0.045952
v  CourantNb              0.025487           43501          47.345           8.198
v  FourierNb              0.023404      2.3656e+05          21.947         0.33688
v  total_pressure       4.1859e+05      8.0088e+05      6.8915e+05      6.5891e+05
v  Local Time Step           0.001        0.012339       0.0010011       0.0010084


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73535      2.3773e+05          69.292          8.5349


 TIME FOR THE TIME STEP              615:        0.10189E+03

===============================================================


 INSTANT    0.616000000E+01   TIME STEP NUMBER             616
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.598940017E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312782948E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12408E+03 0.68011E+01
   Friction velocity        uet   :  0.20633E-01 0.38562E+02
   Friction velocity        uk    :  0.37045E-01 0.38562E+02
   Dimensionless distance   yplus :  0.22101E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14687
   Nb of faces within the viscous sub-layer     :       9992
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15873E+02      65   0.98695E-01   0.62283E+02 0.32658E+02 
c  Velocity[X]                                      0.94734E+01 
c  Velocity[Y]                                      0.23840E+02 
c  Velocity[Z]                                      0.28970E+02 
c  Pressure     0.12981E+00     839   0.37767E-01   0.10126E+00 0.17893E+01 
c  k            0.80537E+00      27   0.17265E-02   0.32126E+00 0.81307E+02 
c  epsilon      0.74852E+04      15   0.10125E-02   0.20665E+08 0.11279E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -7.1049                             6
a  Local Time Step      2.2868e-08                        281351


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8161          19.256          2.0862         0.34729
v  Velocity[Y]             -37.595          47.863          1.1701         0.84679
v  Velocity[Z]             -61.534          37.931         -1.0941      -0.0037993
v  ǁVelocityǁ             0.017083          65.397           7.066           7.249
v  Pressure                 -81894      3.0109e+05      1.8936e+05      1.5904e+05
v  k                    2.7387e-06           17.08        0.094122         0.10324
v  epsilon                0.014609      3.2051e+06          3958.5          70.061
v  TurbVisc             5.2011e-12         0.49488       0.0030575        0.046197
v  CourantNb              0.044208           43729          47.545          8.2123
v  FourierNb              0.023405      2.3656e+05          21.949         0.33744
v  total_pressure       4.1811e+05      8.0109e+05      6.8936e+05      6.5904e+05
v  Local Time Step           0.001        0.013572       0.0010011       0.0010085


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55397      2.3755e+05          69.494          8.5497


 TIME FOR THE TIME STEP              616:        0.98583E+02

===============================================================


 INSTANT    0.617000000E+01   TIME STEP NUMBER             617
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.315972259E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312567187E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11858E+03 0.73486E+01
   Friction velocity        uet   :  0.83992E-02 0.36816E+02
   Friction velocity        uk    :  0.20178E-01 0.36816E+02
   Dimensionless distance   yplus :  0.20828E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14687
   Nb of faces within the viscous sub-layer     :       9968
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15870E+02      61   0.10108E+00   0.61326E+02 0.32526E+02 
c  Velocity[X]                                      0.92666E+01 
c  Velocity[Y]                                      0.23672E+02 
c  Velocity[Z]                                      0.28387E+02 
c  Pressure     0.13072E+00     840   0.38312E-01   0.10153E+00 0.84652E+01 
c  k            0.81312E+00      23   0.14537E-02   0.20864E+00 0.64122E+02 
c  epsilon      0.75559E+04      14   0.87662E-03   0.10554E+08 0.79492E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00034979                             2
a  epsilon                 -103.14                             9
a  Local Time Step      2.2423e-08                        281340


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6883          18.194          2.0902         0.34799
v  Velocity[Y]             -38.203          43.007          1.1785         0.84632
v  Velocity[Z]             -64.223          43.388         -1.0971      -0.0060733
v  ǁVelocityǁ             0.020094          69.971          7.0795          7.2573
v  Pressure                 -80758      3.0314e+05      1.9133e+05      1.6063e+05
v  k                    2.7895e-06           18.75        0.094962         0.10389
v  epsilon              0.00029461        3.29e+06          3982.6          71.102
v  TurbVisc             3.8341e-12         0.49488       0.0030937        0.046418
v  CourantNb             0.0026709           44597          47.729          8.2207
v  FourierNb              0.023407      2.3656e+05          21.949         0.33802
v  total_pressure       4.1924e+05      8.0314e+05      6.9133e+05      6.6063e+05
v  Local Time Step           0.001        0.010779       0.0010011       0.0010086


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72676      2.3812e+05          69.678          8.5587


 TIME FOR THE TIME STEP              617:        0.97932E+02

===============================================================


 INSTANT    0.618000000E+01   TIME STEP NUMBER             618
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.498758359E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312833040E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12208E+03 0.81983E+01
   Friction velocity        uet   :  0.16393E-01 0.40144E+02
   Friction velocity        uk    :  0.44001E-01 0.40144E+02
   Dimensionless distance   yplus :  0.31660E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14679
   Nb of faces within the viscous sub-layer     :       9951
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15889E+02      62   0.99858E-01   0.62552E+02 0.32784E+02 
c  Velocity[X]                                      0.93226E+01 
c  Velocity[Y]                                      0.26749E+02 
c  Velocity[Z]                                      0.26480E+02 
c  Pressure     0.13873E+00     423   0.39601E-01   0.10709E+00 0.15262E+01 
c  k            0.82159E+00      23   0.94070E-03   0.15915E+00 0.54965E+02 
c  epsilon      0.76329E+04      14   0.55876E-03   0.13481E+08 0.88599E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014188                             1
a  epsilon                 -38.874                             8
a  Local Time Step      2.2483e-08                        281337


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5383          18.334          2.0948         0.34833
v  Velocity[Y]             -35.391          48.707          1.1825         0.84589
v  Velocity[Z]             -56.393          39.671         -1.0952      -0.0071018
v  ǁVelocityǁ            0.0036682          60.731          7.0893          7.2638
v  Pressure                 -81504      3.0318e+05      1.9132e+05      1.6058e+05
v  k                    2.7209e-06          20.039        0.095702         0.10453
v  epsilon              0.00020088      3.3457e+06          4022.3          72.043
v  TurbVisc             4.1193e-12         0.49488       0.0031298        0.046616
v  CourantNb              0.051587           44477           47.85          8.2313
v  FourierNb              0.023409      2.3656e+05          21.948         0.33868
v  total_pressure        4.185e+05      8.0318e+05      6.9132e+05      6.6058e+05
v  Local Time Step           0.001        0.011586       0.0010011       0.0010088


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67861      2.4051e+05          69.798            8.57


 TIME FOR THE TIME STEP              618:        0.62907E+02

===============================================================


 INSTANT    0.619000000E+01   TIME STEP NUMBER             619
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.128405035E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312955273E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85042E+02 0.86353E+01
   Friction velocity        uet   :  0.31214E-01 0.34891E+02
   Friction velocity        uk    :  0.42312E-01 0.34891E+02
   Dimensionless distance   yplus :  0.29506E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14689
   Nb of faces within the viscous sub-layer     :       9935
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15888E+02      80   0.99343E-01   0.71117E+02 0.34960E+02 
c  Velocity[X]                                      0.10084E+02 
c  Velocity[Y]                                      0.32145E+02 
c  Velocity[Z]                                      0.28888E+02 
c  Pressure     0.14897E+00     449   0.41960E-01   0.11467E+00 0.14012E+01 
c  k            0.82681E+00      25   0.80726E-03   0.11523E+00 0.46441E+02 
c  epsilon      0.76815E+04      16   0.34475E-03   0.71918E+07 0.64345E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.000178                             2
a  epsilon                 -17.537                             6
a  Local Time Step       2.168e-08                        281384


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6015           18.72          2.0981         0.34878
v  Velocity[Y]              -32.18           34.97          1.1854         0.84579
v  Velocity[Z]             -64.641          38.718          -1.091      -0.0074788
v  ǁVelocityǁ             0.015087          70.353          7.0956          7.2688
v  Pressure                 -82089      3.0314e+05       1.913e+05      1.6054e+05
v  k                    2.7837e-06          19.864        0.096418         0.10512
v  epsilon                0.012375      3.3336e+06            4029          72.845
v  TurbVisc             4.2343e-12         0.49488       0.0031706        0.046795
v  CourantNb             0.0003406           46126          47.926           8.239
v  FourierNb               0.02341      2.3656e+05          21.949         0.33924
v  total_pressure       4.1791e+05      8.0314e+05       6.913e+05      6.6054e+05
v  Local Time Step           0.001        0.010651       0.0010011       0.0010087


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69252      2.3998e+05          69.875          8.5783


 TIME FOR THE TIME STEP              619:        0.75303E+02

===============================================================


 INSTANT    0.620000000E+01   TIME STEP NUMBER             620
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.134590512E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313002007E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12323E+03 0.90061E+01
   Friction velocity        uet   :  0.24387E-01 0.37520E+02
   Friction velocity        uk    :  0.44930E-01 0.37520E+02
   Dimensionless distance   yplus :  0.39074E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14704
   Nb of faces within the viscous sub-layer     :       9923
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15897E+02      61   0.10047E+00   0.74828E+02 0.35746E+02 
c  Velocity[X]                                      0.10598E+02 
c  Velocity[Y]                                      0.34967E+02 
c  Velocity[Z]                                      0.29263E+02 
c  Pressure     0.15850E+00     382   0.44890E-01   0.12167E+00 0.13108E+01 
c  k            0.82220E+00      27   0.18767E-02   0.32792E+00 0.80021E+02 
c  epsilon      0.77016E+04      16   0.62342E-03   0.14728E+08 0.92157E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.6256e-05                             1
a  epsilon                -0.45261                             4
a  Local Time Step      2.1798e-08                        281379


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.484          18.788          2.0975         0.34974
v  Velocity[Y]             -33.785          33.366          1.1867         0.84644
v  Velocity[Z]             -61.923          37.001         -1.0845      -0.0073297
v  ǁVelocityǁ             0.015486          65.509           7.098          7.2724
v  Pressure                 -82410      3.0323e+05      1.9128e+05      1.6053e+05
v  k                      2.76e-06          16.387        0.096857         0.10553
v  epsilon                0.012519      3.3689e+06          4064.9          73.141
v  TurbVisc             4.0106e-12         0.49488        0.003214        0.046956
v  CourantNb              0.060563           45875          47.922          8.2461
v  FourierNb              0.023412      2.3656e+05          21.951         0.33962
v  total_pressure       4.1759e+05      8.0323e+05      6.9128e+05      6.6053e+05
v  Local Time Step           0.001        0.011716       0.0010011       0.0010087


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45013      2.3729e+05          69.874          8.5858


 TIME FOR THE TIME STEP              620:        0.79828E+02

===============================================================


 INSTANT    0.621000000E+01   TIME STEP NUMBER             621
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.173062839E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312968899E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11945E+03 0.94242E+01
   Friction velocity        uet   :  0.33341E-01 0.36823E+02
   Friction velocity        uk    :  0.53376E-01 0.36823E+02
   Dimensionless distance   yplus :  0.17125E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14720
   Nb of faces within the viscous sub-layer     :       9894
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15899E+02      61   0.10110E+00   0.74169E+02 0.35666E+02 
c  Velocity[X]                                      0.11041E+02 
c  Velocity[Y]                                      0.34438E+02 
c  Velocity[Z]                                      0.28691E+02 
c  Pressure     0.16525E+00     388   0.47689E-01   0.12654E+00 0.14066E+01 
c  k            0.81635E+00      24   0.16349E-02   0.37757E+00 0.87773E+02 
c  epsilon      0.77018E+04      14   0.82317E-03   0.11008E+08 0.80577E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                 -3.1743                             7
a  Local Time Step      2.1497e-08                        281377


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.5906          17.778          2.0996         0.35088
v  Velocity[Y]              -36.07          46.133          1.1853         0.84782
v  Velocity[Z]             -63.499          43.158         -1.0776      -0.0069245
v  ǁVelocityǁ             0.022947          69.126          7.0995           7.275
v  Pressure                 -82952      3.0339e+05      1.9126e+05      1.6051e+05
v  k                    2.8004e-06          12.677        0.096933         0.10583
v  epsilon               0.0003693      3.3527e+06          4059.7          72.983
v  TurbVisc             4.2241e-12         0.49488       0.0032517        0.047097
v  CourantNb              0.083395           46518          47.945          8.2519
v  FourierNb              0.023414      2.3656e+05          21.951         0.34034
v  total_pressure       4.1705e+05      8.0339e+05      6.9126e+05      6.6051e+05
v  Local Time Step           0.001        0.012283       0.0010011       0.0010089


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69907      2.3831e+05          69.896          8.5923


 TIME FOR THE TIME STEP              621:        0.75798E+02

===============================================================


 INSTANT    0.622000000E+01   TIME STEP NUMBER             622
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.665554508E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312933195E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12016E+03 0.96460E+01
   Friction velocity        uet   :  0.33744E-01 0.38788E+02
   Friction velocity        uk    :  0.51182E-01 0.38788E+02
   Dimensionless distance   yplus :  0.32355E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14724
   Nb of faces within the viscous sub-layer     :       9871
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15898E+02      64   0.10043E+00   0.69492E+02 0.34493E+02 
c  Velocity[X]                                      0.11640E+02 
c  Velocity[Y]                                      0.30252E+02 
c  Velocity[Z]                                      0.27600E+02 
c  Pressure     0.16573E+00     540   0.48194E-01   0.12646E+00 0.14329E+01 
c  k            0.81450E+00      25   0.11041E-02   0.28352E+00 0.77014E+02 
c  epsilon      0.76303E+04      14   0.81890E-03   0.21381E+08 0.11318E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.4324e-05                             1
a  epsilon                -0.30341                             3
a  Local Time Step      2.1429e-08                        281388


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7521          17.887          2.1041         0.35142
v  Velocity[Y]             -36.888          45.551          1.1813         0.84951
v  Velocity[Z]             -55.057          34.751         -1.0705      -0.0067957
v  ǁVelocityǁ             0.025118          58.519          7.1036          7.2785
v  Pressure                 -83357      3.0352e+05      1.9121e+05      1.6056e+05
v  k                     2.617e-06          12.811        0.097177          0.1061
v  epsilon               0.0039575      3.3506e+06          4061.4          72.857
v  TurbVisc             4.0873e-12         0.49488       0.0032882        0.047221
v  CourantNb             0.0092705           46666          47.935          8.2554
v  FourierNb              0.023415      2.3656e+05          21.951          0.3407
v  total_pressure       4.1664e+05      8.0352e+05      6.9121e+05      6.6056e+05
v  Local Time Step           0.001        0.012223       0.0010011       0.0010088


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66138      2.3668e+05          69.886          8.5961


 TIME FOR THE TIME STEP              622:        0.81986E+02

===============================================================


 INSTANT    0.623000000E+01   TIME STEP NUMBER             623
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.115746019E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312887266E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98940E+02 0.99318E+01
   Friction velocity        uet   :  0.24144E-01 0.33444E+02
   Friction velocity        uk    :  0.51766E-01 0.33444E+02
   Dimensionless distance   yplus :  0.42675E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14750
   Nb of faces within the viscous sub-layer     :       9870
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15901E+02      66   0.99959E-01   0.66215E+02 0.33650E+02 
c  Velocity[X]                                      0.10729E+02 
c  Velocity[Y]                                      0.25962E+02 
c  Velocity[Z]                                      0.29524E+02 
c  Pressure     0.15694E+00     524   0.44711E-01   0.11909E+00 0.13306E+01 
c  k            0.81211E+00      31   0.85921E-03   0.27635E+00 0.77089E+02 
c  epsilon      0.76344E+04      15   0.50242E-03   0.21799E+08 0.11457E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00030158                             1
a  epsilon                 -2.3853                             4
a  Local Time Step      2.1173e-08                        281389


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7605          17.787          2.1076         0.35063
v  Velocity[Y]             -36.788          39.509          1.1818         0.85078
v  Velocity[Z]              -62.92          44.387         -1.0626      -0.0064535
v  ǁVelocityǁ             0.028671           68.44          7.1053          7.2823
v  Pressure                 -83564      3.0362e+05      1.9118e+05       1.606e+05
v  k                    2.6679e-06          12.824        0.097244         0.10628
v  epsilon                0.010368      3.3214e+06          4062.8          72.657
v  TurbVisc             4.0466e-12         0.49488       0.0033238        0.047329
v  CourantNb              0.067513           47230          47.957          8.2602
v  FourierNb              0.023417      2.3656e+05          21.954         0.34126
v  total_pressure       4.1644e+05      8.0362e+05      6.9118e+05       6.606e+05
v  Local Time Step           0.001        0.012382       0.0010011       0.0010087


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5895      2.3693e+05           69.91          8.6014


 TIME FOR THE TIME STEP              623:        0.86222E+02

===============================================================


 INSTANT    0.624000000E+01   TIME STEP NUMBER             624
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.610101480E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312874556E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11801E+03 0.10149E+02
   Friction velocity        uet   :  0.32365E-01 0.32893E+02
   Friction velocity        uk    :  0.44672E-01 0.32893E+02
   Dimensionless distance   yplus :  0.41972E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14795
   Nb of faces within the viscous sub-layer     :       9836
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15908E+02      61   0.99254E-01   0.62879E+02 0.32673E+02 
c  Velocity[X]                                      0.10601E+02 
c  Velocity[Y]                                      0.23201E+02 
c  Velocity[Z]                                      0.29077E+02 
c  Pressure     0.14736E+00     541   0.41094E-01   0.11117E+00 0.12567E+01 
c  k            0.80982E+00      26   0.50030E-03   0.16349E+00 0.59713E+02 
c  epsilon      0.76219E+04      15   0.37623E-03   0.18218E+08 0.10520E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  epsilon                -0.11782                             1
a  Local Time Step      2.1348e-08                        281400


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.765          17.637          2.1097         0.35011
v  Velocity[Y]             -38.554          43.219          1.1847         0.85206
v  Velocity[Z]             -61.008          34.585         -1.0534      -0.0063812
v  ǁVelocityǁ             0.025867          64.288          7.1146          7.2863
v  Pressure                 -83634      3.0372e+05      1.9114e+05      1.6063e+05
v  k                    1.6971e-06          13.414        0.097447         0.10643
v  epsilon                0.012949      3.3101e+06          4060.6          72.518
v  TurbVisc             3.8693e-12         0.49488       0.0033576         0.04742
v  CourantNb             0.0091347           46842          47.954          8.2645
v  FourierNb              0.023419      2.3655e+05          21.956         0.34155
v  total_pressure       4.1637e+05      8.0372e+05      6.9114e+05      6.6063e+05
v  Local Time Step           0.001        0.013444        0.001001       0.0010085


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.33753      2.4044e+05           69.91           8.606


 TIME FOR THE TIME STEP              624:        0.82758E+02

===============================================================


 INSTANT    0.625000000E+01   TIME STEP NUMBER             625
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.541636681E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312900968E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11636E+03 0.94696E+01
   Friction velocity        uet   :  0.35661E-01 0.32091E+02
   Friction velocity        uk    :  0.43098E-01 0.32091E+02
   Dimensionless distance   yplus :  0.40948E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14802
   Nb of faces within the viscous sub-layer     :       9833
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15907E+02      62   0.97278E-01   0.61691E+02 0.32466E+02 
c  Velocity[X]                                      0.10071E+02 
c  Velocity[Y]                                      0.22356E+02 
c  Velocity[Z]                                      0.29264E+02 
c  Pressure     0.13911E+00     471   0.38240E-01   0.10445E+00 0.12681E+01 
c  k            0.80776E+00      26   0.35680E-03   0.13365E+00 0.54346E+02 
c  epsilon      0.76163E+04      15   0.37362E-03   0.17762E+08 0.10395E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022102                             6
a  epsilon                 -3.5304                            13
a  Local Time Step      2.1372e-08                        281396


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7841          18.339          2.1145         0.34941
v  Velocity[Y]             -39.127          29.763          1.1913         0.85282
v  Velocity[Z]             -65.325          44.038         -1.0446        -0.00669
v  ǁVelocityǁ             0.018974          70.887           7.125          7.2888
v  Pressure                 -83546      3.0378e+05       1.911e+05      1.6067e+05
v  k                    2.7379e-06          13.606        0.097816         0.10657
v  epsilon                0.022027      3.2748e+06            4081          72.395
v  TurbVisc             4.1312e-12         0.49488       0.0033883        0.047497
v  CourantNb               0.07516           46790          48.045          8.2701
v  FourierNb               0.02342      2.3655e+05          21.956         0.34196
v  total_pressure       4.1645e+05      8.0378e+05       6.911e+05      6.6067e+05
v  Local Time Step           0.001        0.014517        0.001001       0.0010083


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63942      2.4161e+05          70.002           8.612


 TIME FOR THE TIME STEP              625:        0.84329E+02

===============================================================


 INSTANT    0.626000000E+01   TIME STEP NUMBER             626
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.236510895E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312954706E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12539E+03 0.10215E+02
   Friction velocity        uet   :  0.32651E-01 0.34518E+02
   Friction velocity        uk    :  0.35578E-01 0.34518E+02
   Dimensionless distance   yplus :  0.33523E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14827
   Nb of faces within the viscous sub-layer     :       9822
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15918E+02      64   0.99960E-01   0.58494E+02 0.31523E+02 
c  Velocity[X]                                      0.95705E+01 
c  Velocity[Y]                                      0.20682E+02 
c  Velocity[Z]                                      0.28241E+02 
c  Pressure     0.13346E+00     416   0.36470E-01   0.99714E-01 0.12275E+01 
c  k            0.80663E+00      25   0.23685E-03   0.93072E-01 0.45545E+02 
c  epsilon      0.75753E+04      16   0.21667E-03   0.87111E+07 0.73310E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.4661e-05                             2
a  epsilon        
a  Local Time Step      2.0589e-08                        281398


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.9164          17.244          2.1158         0.34925
v  Velocity[Y]             -39.419          34.508          1.1959         0.85315
v  Velocity[Z]             -56.666          33.916          -1.038      -0.0075155
v  ǁVelocityǁ             0.026098          60.017          7.1338          7.2923
v  Pressure                 -83421      3.0388e+05      1.9105e+05      1.6069e+05
v  k                    2.1478e-06          13.908        0.097813         0.10671
v  epsilon                0.022418       3.249e+06          4048.8          72.276
v  TurbVisc             4.0239e-12         0.49488        0.003417        0.047566
v  CourantNb              0.003835           48570          48.116          8.2736
v  FourierNb              0.023421      2.3655e+05          21.961         0.34222
v  total_pressure       4.1658e+05      8.0388e+05      6.9105e+05      6.6069e+05
v  Local Time Step           0.001        0.015829        0.001001       0.0010081


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7472      2.4226e+05          70.077          8.6159


 TIME FOR THE TIME STEP              626:        0.83360E+02

===============================================================


 INSTANT    0.627000000E+01   TIME STEP NUMBER             627
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.290062823E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313039528E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10321E+03 0.96856E+01
   Friction velocity        uet   :  0.27229E-01 0.32807E+02
   Friction velocity        uk    :  0.40745E-01 0.32807E+02
   Dimensionless distance   yplus :  0.41862E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14851
   Nb of faces within the viscous sub-layer     :       9822
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15916E+02      60   0.98301E-01   0.60055E+02 0.31997E+02 
c  Velocity[X]                                      0.99645E+01 
c  Velocity[Y]                                      0.21063E+02 
c  Velocity[Z]                                      0.29028E+02 
c  Pressure     0.13209E+00     454   0.35856E-01   0.98413E-01 0.11803E+01 
c  k            0.80486E+00      25   0.16597E-03   0.67097E-01 0.38779E+02 
c  epsilon      0.75228E+04      17   0.44070E-03   0.16215E+08 0.10019E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0012795                             4
a  epsilon                 -32.696                             1
a  Local Time Step      1.9596e-08                        281376


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.9063          17.924          2.1191         0.34983
v  Velocity[Y]             -39.171          35.279          1.1983         0.85372
v  Velocity[Z]             -62.773          44.692         -1.0332      -0.0086507
v  ǁVelocityǁ             0.025406          68.166          7.1423          7.2951
v  Pressure                 -83541      3.0398e+05      1.9099e+05       1.607e+05
v  k                    1.0442e-06           13.96        0.098127         0.10683
v  epsilon                0.022924      3.2084e+06          4066.3          72.203
v  TurbVisc              4.134e-12         0.49488       0.0034404        0.047627
v  CourantNb              0.027311           51032          48.178          8.2789
v  FourierNb              0.023423      2.3655e+05          21.961          0.3425
v  total_pressure       4.1646e+05      8.0398e+05      6.9099e+05       6.607e+05
v  Local Time Step           0.001        0.017411        0.001001       0.0010081


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55643      2.4259e+05          70.139          8.6214


 TIME FOR THE TIME STEP              627:        0.89965E+02

===============================================================


 INSTANT    0.628000000E+01   TIME STEP NUMBER             628
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.449754353E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313145798E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11764E+03 0.97735E+01
   Friction velocity        uet   :  0.38897E-01 0.35272E+02
   Friction velocity        uk    :  0.41355E-01 0.35272E+02
   Dimensionless distance   yplus :  0.45008E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14857
   Nb of faces within the viscous sub-layer     :       9823
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15923E+02      60   0.96668E-01   0.57317E+02 0.31207E+02 
c  Velocity[X]                                      0.10180E+02 
c  Velocity[Y]                                      0.20851E+02 
c  Velocity[Z]                                      0.26286E+02 
c  Pressure     0.12796E+00     390   0.35158E-01   0.95089E-01 0.11611E+01 
c  k            0.80250E+00      25   0.19081E-03   0.53974E-01 0.34722E+02 
c  epsilon      0.75227E+04      17   0.28573E-03   0.15220E+08 0.97134E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.8075e-05                             2
a  epsilon                -0.11416                             1
a  Local Time Step      1.9511e-08                        281384


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.958          17.372          2.1196         0.35032
v  Velocity[Y]             -32.777          37.579          1.2007         0.85407
v  Velocity[Z]             -56.178          33.909          -1.032       -0.010052
v  ǁVelocityǁ             0.023956          59.451          7.1509          7.2984
v  Pressure                 -83509      3.0417e+05      1.9092e+05      1.6071e+05
v  k                    2.7086e-06          13.189        0.098135         0.10695
v  epsilon                0.026042      3.2014e+06          4061.6          72.077
v  TurbVisc             4.1967e-12         0.49488       0.0034602        0.047682
v  CourantNb              0.023054           51253          48.219          8.2841
v  FourierNb              0.023424      2.3655e+05          21.963         0.34285
v  total_pressure       4.1649e+05      8.0417e+05      6.9092e+05      6.6071e+05
v  Local Time Step           0.001        0.016984        0.001001       0.0010078


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46562      2.4277e+05          70.182           8.627


 TIME FOR THE TIME STEP              628:        0.75948E+02

===============================================================


 INSTANT    0.629000000E+01   TIME STEP NUMBER             629
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.773952671E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313307725E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10151E+03 0.10112E+02
   Friction velocity        uet   :  0.25295E-01 0.29879E+02
   Friction velocity        uk    :  0.40494E-01 0.29879E+02
   Dimensionless distance   yplus :  0.27497E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14894
   Nb of faces within the viscous sub-layer     :       9805
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15938E+02      61   0.98657E-01   0.58746E+02 0.31594E+02 
c  Velocity[X]                                      0.10402E+02 
c  Velocity[Y]                                      0.22032E+02 
c  Velocity[Z]                                      0.26312E+02 
c  Pressure     0.13040E+00     924   0.35882E-01   0.96847E-01 0.40692E+01 
c  k            0.80324E+00      25   0.16866E-03   0.39528E-01 0.29367E+02 
c  epsilon      0.75267E+04      14   0.47829E-03   0.22130E+08 0.11667E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.0458e-05                             1
a  epsilon              -0.0033586                             1
a  Local Time Step      1.9381e-08                        281385


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.9446          18.594          2.1229         0.35078
v  Velocity[Y]             -35.786          38.904          1.2008         0.85446
v  Velocity[Z]             -65.121          41.224         -1.0305      -0.0086182
v  ǁVelocityǁ             0.014676          70.622          7.1594          7.2992
v  Pressure                 -84467      3.0334e+05      1.8987e+05      1.5993e+05
v  k                    1.5752e-06          13.107        0.098313         0.10709
v  epsilon               0.0033586      3.1894e+06          4086.6          72.069
v  TurbVisc             4.0632e-12         0.49488       0.0034788        0.047733
v  CourantNb              0.028546           51596           48.26          8.2899
v  FourierNb              0.023425      2.3655e+05          21.964         0.34301
v  total_pressure       4.1553e+05      8.0334e+05      6.8987e+05      6.5993e+05
v  Local Time Step           0.001        0.017046        0.001001       0.0010077


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55748      2.4312e+05          70.224          8.6329


 TIME FOR THE TIME STEP              629:        0.10842E+03

===============================================================


 INSTANT    0.630000000E+01   TIME STEP NUMBER             630
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.697492391E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313155409E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12459E+03 0.10954E+02
   Friction velocity        uet   :  0.27431E-01 0.30748E+02
   Friction velocity        uk    :  0.57012E-01 0.30748E+02
   Dimensionless distance   yplus :  0.37121E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14908
   Nb of faces within the viscous sub-layer     :       9795
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15936E+02      57   0.10089E+00   0.61838E+02 0.32409E+02 
c  Velocity[X]                                      0.11262E+02 
c  Velocity[Y]                                      0.22618E+02 
c  Velocity[Z]                                      0.27958E+02 
c  Pressure     0.13163E+00     546   0.36051E-01   0.97665E-01 0.11242E+01 
c  k            0.80534E+00      26   0.11046E-03   0.26191E-01 0.24046E+02 
c  epsilon      0.75368E+04      14   0.36420E-03   0.90632E+07 0.74711E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.4673e-06                             1
a  epsilon                -0.10328                             1
a  Local Time Step      1.9301e-08                        281399


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.9498           17.16          2.1257         0.35085
v  Velocity[Y]             -38.287          33.757          1.2055         0.85473
v  Velocity[Z]             -55.031          34.283         -1.0304      -0.0075106
v  ǁVelocityǁ             0.010694          58.399          7.1707          7.3003
v  Pressure                 -84322      3.0334e+05      1.8979e+05       1.599e+05
v  k                    4.1395e-07          12.905        0.098289         0.10722
v  epsilon                0.023267      3.1634e+06            4080          72.068
v  TurbVisc             2.2513e-12         0.49488       0.0034974         0.04778
v  CourantNb              0.094286           51810          48.286          8.2936
v  FourierNb              0.023425      2.3655e+05          21.963          0.3432
v  total_pressure       4.1568e+05      8.0334e+05      6.8979e+05       6.599e+05
v  Local Time Step           0.001        0.017989        0.001001       0.0010077


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57088      2.4027e+05          70.249          8.6368


 TIME FOR THE TIME STEP              630:        0.81629E+02

===============================================================


 INSTANT    0.631000000E+01   TIME STEP NUMBER             631
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.546393941E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313101516E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85414E+02 0.11252E+02
   Friction velocity        uet   :  0.42092E-01 0.31608E+02
   Friction velocity        uk    :  0.46517E-01 0.31608E+02
   Dimensionless distance   yplus :  0.33455E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14957
   Nb of faces within the viscous sub-layer     :       9798
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15938E+02      62   0.99148E-01   0.64741E+02 0.33118E+02 
c  Velocity[X]                                      0.11162E+02 
c  Velocity[Y]                                      0.24380E+02 
c  Velocity[Z]                                      0.29199E+02 
c  Pressure     0.12970E+00     385   0.35533E-01   0.96349E-01 0.10740E+01 
c  k            0.80700E+00      24   0.93680E-04   0.22820E-01 0.22552E+02 
c  epsilon      0.75336E+04      13   0.33040E-03   0.13421E+08 0.90977E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.1134e-05                             1
a  epsilon        
a  Local Time Step      1.8831e-08                        281396


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8291          18.251          2.1259         0.35084
v  Velocity[Y]             -36.406           33.02          1.2092         0.85455
v  Velocity[Z]             -65.619          43.427         -1.0288      -0.0068887
v  ǁVelocityǁ             0.016704           71.12          7.1784          7.3005
v  Pressure                 -84090      3.0357e+05      1.8977e+05       1.599e+05
v  k                    2.6178e-06           13.25        0.098483         0.10737
v  epsilon                0.020785       3.129e+06          4079.1           72.21
v  TurbVisc             1.6666e-12         0.49488       0.0035147        0.047822
v  CourantNb              0.010965           53104          48.373          8.2973
v  FourierNb              0.023426      2.3655e+05          21.964         0.34349
v  total_pressure       4.1591e+05      8.0357e+05      6.8977e+05       6.599e+05
v  Local Time Step           0.001        0.017509        0.001001       0.0010076


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46366      2.3969e+05          70.337          8.6408


 TIME FOR THE TIME STEP              631:        0.75188E+02

===============================================================


 INSTANT    0.632000000E+01   TIME STEP NUMBER             632
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.349826936E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313010836E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12713E+03 0.10749E+02
   Friction velocity        uet   :  0.22352E-01 0.31649E+02
   Friction velocity        uk    :  0.25829E-01 0.31649E+02
   Dimensionless distance   yplus :  0.32992E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14972
   Nb of faces within the viscous sub-layer     :       9787
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15942E+02      61   0.97867E-01   0.63787E+02 0.32919E+02 
c  Velocity[X]                                      0.11543E+02 
c  Velocity[Y]                                      0.25035E+02 
c  Velocity[Z]                                      0.27209E+02 
c  Pressure     0.12752E+00     517   0.35249E-01   0.94741E-01 0.11546E+01 
c  k            0.80686E+00      24   0.11447E-03   0.20556E-01 0.21308E+02 
c  epsilon      0.75423E+04      12   0.44978E-03   0.10372E+08 0.79757E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.7392e-05                             1
a  epsilon        
a  Local Time Step      1.8721e-08                        281411


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.9622          17.401          2.1229         0.35118
v  Velocity[Y]             -34.844          32.885          1.2158         0.85445
v  Velocity[Z]             -51.684          34.493         -1.0258       -0.006384
v  ǁVelocityǁ             0.010188          54.805          7.1827          7.3015
v  Pressure                 -83623      3.0381e+05      1.8973e+05      1.5994e+05
v  k                    2.7147e-06          13.897        0.098693          0.1075
v  epsilon                0.024124      3.1265e+06          4100.9          72.276
v  TurbVisc             3.8954e-12         0.49488       0.0035341        0.047861
v  CourantNb              0.082947           53416          48.425          8.2998
v  FourierNb              0.023427      2.3656e+05          21.967         0.34381
v  total_pressure       4.1638e+05      8.0381e+05      6.8973e+05      6.5994e+05
v  Local Time Step           0.001        0.017921        0.001001       0.0010075


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57819        2.38e+05          70.392          8.6436


 TIME FOR THE TIME STEP              632:        0.82629E+02

===============================================================


 INSTANT    0.633000000E+01   TIME STEP NUMBER             633
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.688006726E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312956175E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88157E+02 0.10066E+02
   Friction velocity        uet   :  0.19537E-01 0.32841E+02
   Friction velocity        uk    :  0.23842E-01 0.32841E+02
   Dimensionless distance   yplus :  0.32917E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14993
   Nb of faces within the viscous sub-layer     :       9789
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15953E+02      60   0.10059E+00   0.65153E+02 0.33223E+02 
c  Velocity[X]                                      0.12078E+02 
c  Velocity[Y]                                      0.26272E+02 
c  Velocity[Z]                                      0.26803E+02 
c  Pressure     0.13042E+00     506   0.36641E-01   0.97134E-01 0.12080E+01 
c  k            0.80443E+00      25   0.11370E-03   0.20489E-01 0.21281E+02 
c  epsilon      0.74983E+04      12   0.21674E-03   0.79086E+07 0.69953E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.2752e-05                             1
a  epsilon        
a  Local Time Step      1.8465e-08                        281410


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.9278          18.583          2.1203         0.35111
v  Velocity[Y]             -36.182          31.426          1.2237         0.85448
v  Velocity[Z]             -61.889          40.503         -1.0282      -0.0058648
v  ǁVelocityǁ             0.014378           66.83          7.1894          7.3014
v  Pressure                 -83192       3.041e+05      1.8971e+05      1.5997e+05
v  k                    2.7084e-06          13.954        0.098815         0.10762
v  epsilon                 0.02567      3.1009e+06          4083.5          72.301
v  TurbVisc             4.0144e-12         0.49488       0.0035506        0.047896
v  CourantNb              0.070472           54157          48.432          8.3031
v  FourierNb              0.023427      2.3655e+05          21.968         0.34391
v  total_pressure       4.1681e+05       8.041e+05      6.8971e+05      6.5997e+05
v  Local Time Step           0.001        0.015022        0.001001       0.0010073


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74972      2.4217e+05            70.4           8.647


 TIME FOR THE TIME STEP              633:        0.80703E+02

===============================================================


 INSTANT    0.634000000E+01   TIME STEP NUMBER             634
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.438412323E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312883624E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11257E+03 0.98055E+01
   Friction velocity        uet   :  0.38877E-01 0.28670E+02
   Friction velocity        uk    :  0.40190E-01 0.28670E+02
   Dimensionless distance   yplus :  0.30390E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15020
   Nb of faces within the viscous sub-layer     :       9763
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15956E+02      58   0.10164E+00   0.70944E+02 0.34688E+02 
c  Velocity[X]                                      0.11951E+02 
c  Velocity[Y]                                      0.29927E+02 
c  Velocity[Z]                                      0.29065E+02 
c  Pressure     0.13699E+00     427   0.38855E-01   0.10220E+00 0.12301E+01 
c  k            0.80421E+00      21   0.10721E-03   0.18752E-01 0.20384E+02 
c  epsilon      0.74800E+04      12   0.21892E-03   0.73953E+07 0.67760E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.7445e-05                             1
a  epsilon        
a  Local Time Step      1.8693e-08                        281386


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.9138          17.307          2.1218         0.35165
v  Velocity[Y]             -33.979          35.173          1.2391         0.85386
v  Velocity[Z]             -55.186          34.335         -1.0323      -0.0055987
v  ǁVelocityǁ             0.021134          58.489          7.2038          7.3024
v  Pressure                 -82785      3.0436e+05      1.8968e+05      1.6003e+05
v  k                    2.2122e-06          13.697        0.099162         0.10774
v  epsilon                0.027138      3.0691e+06          4084.7          72.402
v  TurbVisc             3.9784e-12         0.49488       0.0035649        0.047928
v  CourantNb                     0           53497          48.482          8.3052
v  FourierNb              0.023428      2.3655e+05          21.967         0.34413
v  total_pressure       4.1721e+05      8.0436e+05      6.8968e+05      6.6003e+05
v  Local Time Step           0.001        0.014532       0.0010009       0.0010071


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54657      2.4358e+05          70.449          8.6494


 TIME FOR THE TIME STEP              634:        0.75579E+02

===============================================================


 INSTANT    0.635000000E+01   TIME STEP NUMBER             635
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.564613341E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312866051E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89651E+02 0.10696E+02
   Friction velocity        uet   :  0.20158E-01 0.29011E+02
   Friction velocity        uk    :  0.58049E-01 0.29011E+02
   Dimensionless distance   yplus :  0.27212E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15059
   Nb of faces within the viscous sub-layer     :       9740
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15954E+02      65   0.10092E+00   0.72314E+02 0.35006E+02 
c  Velocity[X]                                      0.12569E+02 
c  Velocity[Y]                                      0.29980E+02 
c  Velocity[Z]                                      0.29765E+02 
c  Pressure     0.14185E+00     512   0.41161E-01   0.10622E+00 0.12887E+01 
c  k            0.80672E+00      21   0.12994E-03   0.21910E-01 0.21815E+02 
c  epsilon      0.74847E+04      12   0.21348E-03   0.53637E+07 0.57600E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.0599e-05                             1
a  epsilon        
a  Local Time Step      1.8589e-08                        281382


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7381           18.42          2.1195         0.35227
v  Velocity[Y]             -35.049          35.712          1.2516         0.85284
v  Velocity[Z]             -61.985          41.675         -1.0343      -0.0053147
v  ǁVelocityǁ             0.031241          66.941          7.2147           7.302
v  Pressure                 -82570      3.0459e+05      1.8967e+05      1.6005e+05
v  k                    2.6941e-06          13.478         0.09951          0.1079
v  epsilon                  0.0284      3.0578e+06          4095.2          72.634
v  TurbVisc             4.0951e-12         0.49488       0.0035761        0.047957
v  CourantNb              0.010687           53795          48.618          8.3092
v  FourierNb              0.023429      2.3655e+05          21.969         0.34417
v  total_pressure       4.1743e+05      8.0459e+05      6.8967e+05      6.6005e+05
v  Local Time Step           0.001         0.01326       0.0010009       0.0010068


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58199      2.4428e+05          70.587          8.6533


 TIME FOR THE TIME STEP              635:        0.81198E+02

===============================================================


 INSTANT    0.636000000E+01   TIME STEP NUMBER             636
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.523907976E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312847379E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10494E+03 0.10832E+02
   Friction velocity        uet   :  0.18266E-01 0.26304E+02
   Friction velocity        uk    :  0.51950E-01 0.26304E+02
   Dimensionless distance   yplus :  0.22620E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15062
   Nb of faces within the viscous sub-layer     :       9749
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15964E+02      60   0.10152E+00   0.70721E+02 0.34665E+02 
c  Velocity[X]                                      0.12538E+02 
c  Velocity[Y]                                      0.30809E+02 
c  Velocity[Z]                                      0.27374E+02 
c  Pressure     0.15034E+00     508   0.44277E-01   0.11314E+00 0.13810E+01 
c  k            0.80794E+00      23   0.16396E-03   0.22185E-01 0.22216E+02 
c  epsilon      0.74706E+04      12   0.15519E-03   0.29589E+07 0.42933E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010254                             1
a  epsilon        
a  Local Time Step      1.8565e-08                        281417


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6628          17.335          2.1179         0.35221
v  Velocity[Y]             -34.301          41.248          1.2597         0.85193
v  Velocity[Z]             -60.471           34.98          -1.035      -0.0052333
v  ǁVelocityǁ             0.011485          63.892          7.2258          7.3016
v  Pressure                 -82305      3.0472e+05      1.8965e+05      1.6008e+05
v  k                    2.8128e-06          13.062        0.099702         0.10805
v  epsilon                0.029253      3.0465e+06          4089.9          72.742
v  TurbVisc             3.9449e-12         0.49488        0.003591        0.047988
v  CourantNb              0.009396           53866          48.686          8.3124
v  FourierNb              0.023431      2.3655e+05          21.968         0.34427
v  total_pressure       4.1769e+05      8.0472e+05      6.8965e+05      6.6008e+05
v  Local Time Step           0.001        0.013082       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67016      2.4156e+05          70.654          8.6567


 TIME FOR THE TIME STEP              636:        0.82428E+02

===============================================================


 INSTANT    0.637000000E+01   TIME STEP NUMBER             637
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.679136519E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312850696E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10549E+03 0.96118E+01
   Friction velocity        uet   :  0.23465E-01 0.24715E+02
   Friction velocity        uk    :  0.42183E-01 0.24715E+02
   Dimensionless distance   yplus :  0.25767E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15047
   Nb of faces within the viscous sub-layer     :       9731
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15963E+02      57   0.10034E+00   0.70867E+02 0.34644E+02 
c  Velocity[X]                                      0.12373E+02 
c  Velocity[Y]                                      0.30995E+02 
c  Velocity[Z]                                      0.27498E+02 
c  Pressure     0.15133E+00     484   0.45823E-01   0.11453E+00 0.14747E+01 
c  k            0.80614E+00      22   0.10545E-03   0.21968E-01 0.22080E+02 
c  epsilon      0.74737E+04      13   0.24263E-03   0.74014E+07 0.67779E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -6.791e-05                             1
a  epsilon        
a  Local Time Step      1.8468e-08                        281421


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6164          18.542          2.1141         0.35191
v  Velocity[Y]             -33.809          37.709          1.2639         0.85097
v  Velocity[Z]             -62.817          42.918         -1.0373      -0.0050734
v  ǁVelocityǁ             0.024799          68.302          7.2375          7.3005
v  Pressure                 -82181      3.0483e+05      1.8965e+05       1.601e+05
v  k                     2.888e-06          13.297         0.10013         0.10823
v  epsilon                 0.02956      3.0364e+06          4097.3          72.965
v  TurbVisc             4.2119e-12         0.49488       0.0036107        0.048017
v  CourantNb              0.046599           54149          48.819          8.3138
v  FourierNb              0.023433      2.3655e+05           21.97         0.34452
v  total_pressure       4.1782e+05      8.0483e+05      6.8965e+05       6.601e+05
v  Local Time Step           0.001        0.012481       0.0010009       0.0010068


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77848      2.4613e+05          70.789          8.6583


 TIME FOR THE TIME STEP              637:        0.82959E+02

===============================================================


 INSTANT    0.638000000E+01   TIME STEP NUMBER             638
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.179464739E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312810543E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11861E+03 0.89754E+01
   Friction velocity        uet   :  0.35644E-01 0.29928E+02
   Friction velocity        uk    :  0.47225E-01 0.29928E+02
   Dimensionless distance   yplus :  0.31367E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15039
   Nb of faces within the viscous sub-layer     :       9686
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15966E+02      60   0.10350E+00   0.74239E+02 0.35500E+02 
c  Velocity[X]                                      0.12295E+02 
c  Velocity[Y]                                      0.32266E+02 
c  Velocity[Z]                                      0.29677E+02 
c  Pressure     0.15585E+00     458   0.47963E-01   0.11834E+00 0.14819E+01 
c  k            0.80317E+00      21   0.15202E-03   0.19762E-01 0.20887E+02 
c  epsilon      0.74542E+04      16   0.28380E-03   0.13003E+08 0.89825E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00066182                             5
a  epsilon                 -15.615                             7
a  Local Time Step      1.8332e-08                        281420


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.6423          17.416          2.1164          0.3518
v  Velocity[Y]             -35.868          37.765           1.267         0.84897
v  Velocity[Z]             -54.472          35.018         -1.0394      -0.0053833
v  ǁVelocityǁ             0.011611          57.796          7.2445          7.2998
v  Pressure                 -82112       3.049e+05      1.8964e+05      1.6013e+05
v  k                    2.8826e-06          13.318         0.10048         0.10839
v  epsilon                 0.02961      3.0468e+06          4109.9          73.027
v  TurbVisc             4.1978e-12         0.49488       0.0036316        0.048048
v  CourantNb              0.071888           54551          48.972          8.3153
v  FourierNb              0.023435      2.3655e+05          21.971         0.34473
v  total_pressure       4.1789e+05       8.049e+05      6.8964e+05      6.6013e+05
v  Local Time Step           0.001        0.013729       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63362      2.4629e+05          70.943            8.66


 TIME FOR THE TIME STEP              638:        0.66271E+02

===============================================================


 INSTANT    0.639000000E+01   TIME STEP NUMBER             639
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.148995708E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312871831E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89738E+02 0.92589E+01
   Friction velocity        uet   :  0.37159E-01 0.31771E+02
   Friction velocity        uk    :  0.53206E-01 0.31771E+02
   Dimensionless distance   yplus :  0.35840E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15024
   Nb of faces within the viscous sub-layer     :       9657
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15971E+02      59   0.10592E+00   0.75593E+02 0.35775E+02 
c  Velocity[X]                                      0.12787E+02 
c  Velocity[Y]                                      0.31049E+02 
c  Velocity[Z]                                      0.31757E+02 
c  Pressure     0.16282E+00     415   0.50134E-01   0.12401E+00 0.15067E+01 
c  k            0.80359E+00      21   0.13888E-03   0.16160E-01 0.18783E+02 
c  epsilon      0.74105E+04      13   0.28296E-03   0.91054E+07 0.75697E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.8306e-05                             2
a  epsilon        
a  Local Time Step      1.8191e-08                        281428


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7743          18.527          2.1184         0.35174
v  Velocity[Y]             -35.925          42.574          1.2678         0.84659
v  Velocity[Z]             -64.215          39.007         -1.0407       -0.005855
v  ǁVelocityǁ             0.021536          69.802          7.2504          7.2997
v  Pressure                 -82150      3.0496e+05      1.8964e+05      1.6012e+05
v  k                    2.8735e-06          13.987         0.10048         0.10857
v  epsilon                0.029723      3.0448e+06          4077.7          73.099
v  TurbVisc             4.3118e-12         0.49488        0.003651         0.04808
v  CourantNb               0.06394           54973          49.057          8.3148
v  FourierNb              0.023439      2.3655e+05          21.974           0.345
v  total_pressure       4.1785e+05      8.0496e+05      6.8964e+05      6.6012e+05
v  Local Time Step           0.001        0.014923       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69907      2.4619e+05          71.031          8.6598


 TIME FOR THE TIME STEP              639:        0.80150E+02

===============================================================


 INSTANT    0.640000000E+01   TIME STEP NUMBER             640
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.558711085E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312857726E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12341E+03 0.10506E+02
   Friction velocity        uet   :  0.32183E-01 0.35017E+02
   Friction velocity        uk    :  0.61874E-01 0.35017E+02
   Dimensionless distance   yplus :  0.28130E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15018
   Nb of faces within the viscous sub-layer     :       9627
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15975E+02      65   0.10448E+00   0.72477E+02 0.35095E+02 
c  Velocity[X]                                      0.11884E+02 
c  Velocity[Y]                                      0.30191E+02 
c  Velocity[Z]                                      0.30402E+02 
c  Pressure     0.15982E+00     354   0.48902E-01   0.12203E+00 0.14321E+01 
c  k            0.80669E+00      24   0.17354E-03   0.24492E-01 0.23159E+02 
c  epsilon      0.74551E+04      13   0.28988E-03   0.10951E+08 0.82346E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.2814e-05                             1
a  epsilon        
a  Local Time Step      1.7941e-08                        281440


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7082          17.315           2.122         0.35185
v  Velocity[Y]             -35.196          40.032          1.2673         0.84458
v  Velocity[Z]             -53.797          34.429         -1.0422       -0.005764
v  ǁVelocityǁ              0.01097          56.978          7.2531          7.2994
v  Pressure                 -81975      3.0492e+05      1.8965e+05      1.6014e+05
v  k                    1.8068e-06          14.234         0.10104         0.10882
v  epsilon               0.0007325       3.093e+06          4115.8          73.388
v  TurbVisc             4.2739e-12         0.49488       0.0036718        0.048112
v  CourantNb               0.08735           55738          49.153          8.3146
v  FourierNb              0.023443      2.3655e+05          21.977         0.34517
v  total_pressure       4.1802e+05      8.0492e+05      6.8965e+05      6.6014e+05
v  Local Time Step           0.001        0.013359       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48875      2.4689e+05           71.13          8.6598


 TIME FOR THE TIME STEP              640:        0.77930E+02

===============================================================


 INSTANT    0.641000000E+01   TIME STEP NUMBER             641
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.165669505E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312852368E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87521E+02 0.10173E+02
   Friction velocity        uet   :  0.32303E-01 0.36382E+02
   Friction velocity        uk    :  0.51431E-01 0.36382E+02
   Dimensionless distance   yplus :  0.24067E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14978
   Nb of faces within the viscous sub-layer     :       9628
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15974E+02      54   0.10351E+00   0.70006E+02 0.34445E+02 
c  Velocity[X]                                      0.11304E+02 
c  Velocity[Y]                                      0.29811E+02 
c  Velocity[Z]                                      0.28892E+02 
c  Pressure     0.16046E+00     423   0.48938E-01   0.12295E+00 0.14892E+01 
c  k            0.80718E+00      22   0.13899E-03   0.29446E-01 0.25306E+02 
c  epsilon      0.74635E+04      14   0.25281E-03   0.69589E+07 0.65773E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.7756e-05                             2
a  epsilon        
a  Local Time Step      1.8184e-08                        281410


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7909          18.746          2.1193         0.35199
v  Velocity[Y]             -33.248          36.191          1.2688          0.8439
v  Velocity[Z]             -60.305          42.458         -1.0464      -0.0050549
v  ǁVelocityǁ            0.0088467          65.316           7.255          7.2988
v  Pressure                 -81923      3.0488e+05      1.8968e+05       1.601e+05
v  k                     2.814e-06          14.492         0.10117         0.10909
v  epsilon                0.029861      3.1166e+06          4107.4          73.565
v  TurbVisc             2.4634e-12         0.49488       0.0036958        0.048148
v  CourantNb              0.059068           54994          49.185          8.3145
v  FourierNb              0.023449      2.3655e+05           21.98         0.34544
v  total_pressure       4.1808e+05      8.0488e+05      6.8968e+05       6.601e+05
v  Local Time Step           0.001        0.014131       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.3123      2.4599e+05          71.164          8.6599


 TIME FOR THE TIME STEP              641:        0.70876E+02

===============================================================


 INSTANT    0.642000000E+01   TIME STEP NUMBER             642
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.399012050E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312792402E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10343E+03 0.93191E+01
   Friction velocity        uet   :  0.25617E-01 0.34937E+02
   Friction velocity        uk    :  0.54496E-01 0.34937E+02
   Dimensionless distance   yplus :  0.22121E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14987
   Nb of faces within the viscous sub-layer     :       9612
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15973E+02      60   0.10425E+00   0.70622E+02 0.34629E+02 
c  Velocity[X]                                      0.10953E+02 
c  Velocity[Y]                                      0.30396E+02 
c  Velocity[Z]                                      0.29273E+02 
c  Pressure     0.15972E+00     406   0.47425E-01   0.12262E+00 0.13985E+01 
c  k            0.80603E+00      27   0.20382E-03   0.35524E-01 0.27728E+02 
c  epsilon      0.74631E+04      15   0.85162E-03   0.17814E+08 0.10487E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.5163e-05                             1
a  epsilon        
a  Local Time Step      1.7743e-08                        281420


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.7347          17.332          2.1212         0.35239
v  Velocity[Y]             -38.235          42.649          1.2688         0.84357
v  Velocity[Z]             -48.862          34.507         -1.0444      -0.0040639
v  ǁVelocityǁ             0.022359          52.159          7.2548           7.298
v  Pressure                 -81763      3.0486e+05      1.8972e+05      1.6008e+05
v  k                    2.8394e-06          14.029         0.10167         0.10941
v  epsilon                0.030069      3.1883e+06          4133.6          73.848
v  TurbVisc             4.1548e-12         0.49488       0.0037211        0.048188
v  CourantNb              0.034991           56361           49.19          8.3158
v  FourierNb              0.023456      2.3655e+05          21.983         0.34562
v  total_pressure       4.1824e+05      8.0486e+05      6.8972e+05      6.6008e+05
v  Local Time Step           0.001         0.01448       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83583      2.4515e+05          71.173          8.6614


 TIME FOR THE TIME STEP              642:        0.69435E+02

===============================================================


 INSTANT    0.643000000E+01   TIME STEP NUMBER             643
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.480880502E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312746606E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.79996E+02 0.87233E+01
   Friction velocity        uet   :  0.87263E-02 0.34511E+02
   Friction velocity        uk    :  0.48261E-01 0.34511E+02
   Dimensionless distance   yplus :  0.14397E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14979
   Nb of faces within the viscous sub-layer     :       9615
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15965E+02      55   0.10328E+00   0.68633E+02 0.34090E+02 
c  Velocity[X]                                      0.10168E+02 
c  Velocity[Y]                                      0.27527E+02 
c  Velocity[Z]                                      0.30938E+02 
c  Pressure     0.15590E+00     415   0.45464E-01   0.11988E+00 0.14207E+01 
c  k            0.80719E+00      20   0.11672E-03   0.28652E-01 0.24830E+02 
c  epsilon      0.74830E+04      15   0.14793E-02   0.15418E+08 0.97599E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.9082e-06                             1
a  epsilon        
a  Local Time Step      1.8119e-08                        281419


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8098           18.55          2.1196         0.35264
v  Velocity[Y]             -36.934           39.21          1.2667         0.84351
v  Velocity[Z]             -65.876          42.031         -1.0433      -0.0024931
v  ǁVelocityǁ            0.0080011          71.616          7.2537          7.2973
v  Pressure                 -81538      3.0475e+05      1.8978e+05      1.6003e+05
v  k                    2.8477e-06          13.744          0.1018          0.1097
v  epsilon                0.029803      3.1963e+06          4123.9          73.984
v  TurbVisc             4.1319e-12         0.49488       0.0037484        0.048233
v  CourantNb              0.030747           55189          49.162          8.3169
v  FourierNb              0.023464      2.3655e+05          21.985         0.34584
v  total_pressure       4.1846e+05      8.0475e+05      6.8978e+05      6.6003e+05
v  Local Time Step           0.001        0.014458       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60208      2.4256e+05          71.146          8.6628


 TIME FOR THE TIME STEP              643:        0.74509E+02

===============================================================


 INSTANT    0.644000000E+01   TIME STEP NUMBER             644
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.286898625E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312581796E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12813E+03 0.10781E+02
   Friction velocity        uet   :  0.32933E-01 0.33589E+02
   Friction velocity        uk    :  0.56866E-01 0.33589E+02
   Dimensionless distance   yplus :  0.23778E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14994
   Nb of faces within the viscous sub-layer     :       9605
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15963E+02      59   0.10467E+00   0.68930E+02 0.34199E+02 
c  Velocity[X]                                      0.10400E+02 
c  Velocity[Y]                                      0.27566E+02 
c  Velocity[Z]                                      0.30965E+02 
c  Pressure     0.14895E+00     752   0.42584E-01   0.11437E+00 0.50051E+01 
c  k            0.81184E+00      25   0.36878E-03   0.60639E-01 0.34461E+02 
c  epsilon      0.75341E+04      12   0.81396E-03   0.82246E+07 0.70616E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.5708e-05                             1
a  epsilon        
a  Local Time Step      1.7925e-08                        281424


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.9057          17.341          2.1208         0.35336
v  Velocity[Y]             -36.956          45.894          1.2666         0.84401
v  Velocity[Z]             -52.439          34.367         -1.0414      -0.0028987
v  ǁVelocityǁ             0.011557          55.772          7.2526          7.2986
v  Pressure                 -80403      3.0594e+05      1.9104e+05      1.6095e+05
v  k                    2.9144e-06          13.331          0.1022         0.11002
v  epsilon                0.029136      3.2659e+06          4134.9          74.297
v  TurbVisc             4.2516e-12         0.49488       0.0037749        0.048278
v  CourantNb                0.0114           55789          49.169          8.3169
v  FourierNb              0.023474      2.3655e+05           21.99         0.34612
v  total_pressure        4.196e+05      8.0594e+05      6.9104e+05      6.6095e+05
v  Local Time Step           0.001        0.014471       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74602      2.4309e+05          71.159           8.663


 TIME FOR THE TIME STEP              644:        0.87048E+02

===============================================================


 INSTANT    0.645000000E+01   TIME STEP NUMBER             645
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.123309824E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312624417E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83965E+02 0.11332E+02
   Friction velocity        uet   :  0.24556E-01 0.34912E+02
   Friction velocity        uk    :  0.62382E-01 0.34912E+02
   Dimensionless distance   yplus :  0.20019E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14983
   Nb of faces within the viscous sub-layer     :       9605
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15970E+02      60   0.10498E+00   0.66329E+02 0.33516E+02 
c  Velocity[X]                                      0.10526E+02 
c  Velocity[Y]                                      0.26223E+02 
c  Velocity[Z]                                      0.29580E+02 
c  Pressure     0.14434E+00     408   0.40711E-01   0.11070E+00 0.13721E+01 
c  k            0.81784E+00      20   0.25011E-03   0.48955E-01 0.31524E+02 
c  epsilon      0.75696E+04      14   0.59862E-03   0.15995E+08 0.98255E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.6526e-05                             1
a  epsilon        
a  Local Time Step      1.7637e-08                        281421


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8446          18.465            2.12         0.35324
v  Velocity[Y]             -35.935          38.039          1.2652         0.84409
v  Velocity[Z]             -65.033          38.254         -1.0403      -0.0022691
v  ǁVelocityǁ             0.022988          70.711          7.2497          7.2985
v  Pressure                 -80570      3.0595e+05      1.9111e+05      1.6088e+05
v  k                     2.156e-06           13.51         0.10263         0.11034
v  epsilon                0.028158       3.268e+06          4155.2          74.626
v  TurbVisc              4.261e-12         0.49488       0.0038035        0.048325
v  CourantNb              0.030651           56700          49.174          8.3177
v  FourierNb              0.023484      2.3655e+05          21.993         0.34644
v  total_pressure       4.1943e+05      8.0595e+05      6.9111e+05      6.6088e+05
v  Local Time Step           0.001        0.011379       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94276      2.4572e+05          71.167          8.6641


 TIME FOR THE TIME STEP              645:        0.77356E+02

===============================================================


 INSTANT    0.646000000E+01   TIME STEP NUMBER             646
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.741604725E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312539814E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12602E+03 0.11464E+02
   Friction velocity        uet   :  0.15204E-01 0.33709E+02
   Friction velocity        uk    :  0.58706E-01 0.33709E+02
   Dimensionless distance   yplus :  0.21012E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14970
   Nb of faces within the viscous sub-layer     :       9578
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15965E+02      63   0.10355E+00   0.66790E+02 0.33659E+02 
c  Velocity[X]                                      0.10407E+02 
c  Velocity[Y]                                      0.26744E+02 
c  Velocity[Z]                                      0.29639E+02 
c  Pressure     0.13808E+00     894   0.39326E-01   0.10575E+00 0.47577E+01 
c  k            0.82186E+00      21   0.22057E-03   0.57618E-01 0.34210E+02 
c  epsilon      0.76335E+04      15   0.55350E-03   0.11904E+08 0.84316E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.3939e-05                             2
a  epsilon        
a  Local Time Step      1.7236e-08                        281428


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -7.912          17.603           2.118         0.35337
v  Velocity[Y]             -37.361          48.223          1.2612         0.84379
v  Velocity[Z]             -53.729          33.701         -1.0382      -0.0029519
v  ǁVelocityǁ             0.020786          57.018          7.2451          7.3004
v  Pressure                 -79770      3.0724e+05      1.9228e+05      1.6175e+05
v  k                    1.2926e-06          13.652         0.10313         0.11067
v  epsilon                0.027423      3.3276e+06          4173.7           74.96
v  TurbVisc             4.2005e-12         0.49488       0.0038303        0.048371
v  CourantNb                     0           58018          49.198          8.3164
v  FourierNb              0.023496      2.3655e+05          21.998         0.34668
v  total_pressure       4.2023e+05      8.0724e+05      6.9228e+05      6.6175e+05
v  Local Time Step           0.001        0.012517       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87846      2.4509e+05          71.196          8.6631


 TIME FOR THE TIME STEP              646:        0.96356E+02

===============================================================


 INSTANT    0.647000000E+01   TIME STEP NUMBER             647
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.187691448E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312603972E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87518E+02 0.10534E+02
   Friction velocity        uet   :  0.35615E-01 0.39060E+02
   Friction velocity        uk    :  0.36627E-01 0.39060E+02
   Dimensionless distance   yplus :  0.18464E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14977
   Nb of faces within the viscous sub-layer     :       9575
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15973E+02      60   0.10589E+00   0.66621E+02 0.33618E+02 
c  Velocity[X]                                      0.10456E+02 
c  Velocity[Y]                                      0.26465E+02 
c  Velocity[Z]                                      0.29700E+02 
c  Pressure     0.13472E+00     528   0.38287E-01   0.10284E+00 0.14476E+01 
c  k            0.82468E+00      22   0.31466E-03   0.81572E-01 0.39977E+02 
c  epsilon      0.76773E+04      17   0.50046E-03   0.13435E+08 0.89138E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.0355e-05                             1
a  epsilon        
a  Local Time Step      1.7415e-08                        281424


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.8677          18.578          2.1177         0.35373
v  Velocity[Y]             -35.604          36.034          1.2553         0.84298
v  Velocity[Z]             -65.775          42.698         -1.0349      -0.0026491
v  ǁVelocityǁ             0.010287          71.616           7.241          7.3007
v  Pressure                 -80183      3.0743e+05      1.9235e+05      1.6171e+05
v  k                    2.6958e-06          13.991         0.10345         0.11102
v  epsilon                0.026569      3.3333e+06          4202.2          75.259
v  TurbVisc             4.0861e-12         0.49488        0.003857        0.048422
v  CourantNb              0.020208           57422          49.102          8.3161
v  FourierNb              0.023507      2.3655e+05          22.001         0.34694
v  total_pressure       4.1982e+05      8.0743e+05      6.9235e+05      6.6171e+05
v  Local Time Step           0.001        0.013646       0.0010009       0.0010066


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69117      2.4245e+05          71.104           8.663


 TIME FOR THE TIME STEP              647:        0.83270E+02

===============================================================


 INSTANT    0.648000000E+01   TIME STEP NUMBER             648
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.227008567E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312563712E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12869E+03 0.10704E+02
   Friction velocity        uet   :  0.15424E-01 0.38847E+02
   Friction velocity        uk    :  0.58753E-01 0.38846E+02
   Dimensionless distance   yplus :  0.20756E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14999
   Nb of faces within the viscous sub-layer     :       9581
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15977E+02      55   0.10309E+00   0.64564E+02 0.33090E+02 
c  Velocity[X]                                      0.10464E+02 
c  Velocity[Y]                                      0.24272E+02 
c  Velocity[Z]                                      0.29828E+02 
c  Pressure     0.12957E+00     785   0.36791E-01   0.98617E-01 0.49737E+01 
c  k            0.82598E+00      21   0.32657E-03   0.88798E-01 0.41984E+02 
c  epsilon      0.77174E+04      13   0.30462E-03   0.77040E+07 0.67438E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00048809                             2
a  epsilon        
a  Local Time Step      1.7427e-08                        281440


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.9771          17.558          2.1203          0.3542
v  Velocity[Y]             -35.897          42.339          1.2549         0.84264
v  Velocity[Z]             -52.678          33.897          -1.035      -0.0040106
v  ǁVelocityǁ             0.012912          55.883          7.2415          7.3031
v  Pressure                 -79604       3.087e+05      1.9352e+05      1.6264e+05
v  k                    2.6921e-06          13.842         0.10374         0.11142
v  epsilon                0.026102      3.3651e+06            4203          75.537
v  TurbVisc             3.9848e-12         0.49488       0.0038838        0.048474
v  CourantNb             0.0050779           57383          49.047          8.3145
v  FourierNb               0.02352      2.3655e+05          22.004         0.34742
v  total_pressure        4.204e+05       8.087e+05      6.9352e+05      6.6264e+05
v  Local Time Step           0.001         0.01256       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57733      2.4501e+05          71.051          8.6619


 TIME FOR THE TIME STEP              648:        0.90364E+02

===============================================================


 INSTANT    0.649000000E+01   TIME STEP NUMBER             649
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.392659239E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312715607E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.78855E+02 0.10866E+02
   Friction velocity        uet   :  0.33995E-01 0.38843E+02
   Friction velocity        uk    :  0.40359E-01 0.38843E+02
   Dimensionless distance   yplus :  0.23680E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15014
   Nb of faces within the viscous sub-layer     :       9571
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15986E+02      60   0.10567E+00   0.62690E+02 0.32590E+02 
c  Velocity[X]                                      0.98407E+01 
c  Velocity[Y]                                      0.23385E+02 
c  Velocity[Z]                                      0.29464E+02 
c  Pressure     0.12569E+00     427   0.34455E-01   0.95554E-01 0.12658E+01 
c  k            0.82312E+00      22   0.28035E-03   0.68902E-01 0.36423E+02 
c  epsilon      0.77108E+04      14   0.23354E-03   0.36855E+07 0.46490E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010891                             2
a  epsilon        
a  Local Time Step      1.7416e-08                        281423


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.0169          19.185          2.1218         0.35419
v  Velocity[Y]             -36.448          32.647          1.2575         0.84209
v  Velocity[Z]             -65.622          40.281         -1.0354      -0.0047344
v  ǁVelocityǁ             0.016372          72.761          7.2414          7.3037
v  Pressure                 -80062      3.0886e+05      1.9354e+05       1.626e+05
v  k                    2.7451e-06          13.747         0.10394         0.11182
v  epsilon                0.026052      3.3405e+06          4200.5          75.777
v  TurbVisc              4.022e-12         0.49488       0.0039079        0.048536
v  CourantNb                     0           57419          49.007          8.3153
v  FourierNb              0.023533      2.3655e+05          22.004          0.3477
v  total_pressure       4.1994e+05      8.0886e+05      6.9354e+05       6.626e+05
v  Local Time Step           0.001        0.011999       0.0010009       0.0010068


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71158      2.4502e+05          71.012           8.663


 TIME FOR THE TIME STEP              649:        0.73217E+02

===============================================================


 INSTANT    0.650000000E+01   TIME STEP NUMBER             650
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.653166859E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312732177E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12824E+03 0.10873E+02
   Friction velocity        uet   :  0.17752E-01 0.39823E+02
   Friction velocity        uk    :  0.49071E-01 0.39823E+02
   Dimensionless distance   yplus :  0.56806E-03 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15016
   Nb of faces within the viscous sub-layer     :       9576
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15984E+02      62   0.10798E+00   0.61537E+02 0.32286E+02 
c  Velocity[X]                                      0.94375E+01 
c  Velocity[Y]                                      0.23876E+02 
c  Velocity[Z]                                      0.28223E+02 
c  Pressure     0.12523E+00     490   0.33496E-01   0.95205E-01 0.12057E+01 
c  k            0.82207E+00      21   0.26326E-03   0.56698E-01 0.33633E+02 
c  epsilon      0.77358E+04      14   0.22420E-03   0.53986E+07 0.56276E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00043878                             2
a  epsilon        
a  Local Time Step      1.7102e-08                        281405


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.007          17.733          2.1255         0.35414
v  Velocity[Y]             -38.992          45.837          1.2635         0.84149
v  Velocity[Z]             -59.438          33.941         -1.0384      -0.0048141
v  ǁVelocityǁ             0.020581          63.026          7.2472          7.3042
v  Pressure                 -80493        3.09e+05      1.9355e+05       1.626e+05
v  k                    2.7166e-06          13.353         0.10434          0.1122
v  epsilon                0.026245      3.3784e+06          4221.8          76.006
v  TurbVisc              4.089e-12         0.49488       0.0039306        0.048603
v  CourantNb             0.0097653           58473           48.97          8.3147
v  FourierNb              0.023545      2.3655e+05          22.003         0.34791
v  total_pressure       4.1951e+05        8.09e+05      6.9355e+05       6.626e+05
v  Local Time Step           0.001        0.011419       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76114       2.429e+05          70.972          8.6626


 TIME FOR THE TIME STEP              650:        0.83477E+02

===============================================================


 INSTANT    0.651000000E+01   TIME STEP NUMBER             651
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.465805667E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312695099E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10255E+03 0.11065E+02
   Friction velocity        uet   :  0.11772E-01 0.41973E+02
   Friction velocity        uk    :  0.11687E-01 0.41973E+02
   Dimensionless distance   yplus :  0.16361E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15025
   Nb of faces within the viscous sub-layer     :       9563
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15983E+02      61   0.10682E+00   0.61599E+02 0.32299E+02 
c  Velocity[X]                                      0.97083E+01 
c  Velocity[Y]                                      0.22893E+02 
c  Velocity[Z]                                      0.28997E+02 
c  Pressure     0.12577E+00     430   0.32406E-01   0.95418E-01 0.99212E+00 
c  k            0.81954E+00      22   0.29995E-03   0.82017E-01 0.40838E+02 
c  epsilon      0.77247E+04      13   0.30720E-03   0.66258E+07 0.62548E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014812                             4
a  epsilon        
a  Local Time Step      1.7019e-08                        281398


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.0214          18.704          2.1257         0.35379
v  Velocity[Y]             -38.054          40.275          1.2715         0.84093
v  Velocity[Z]             -65.782          40.856         -1.0411      -0.0042325
v  ǁVelocityǁ             0.019953          72.749          7.2538          7.3051
v  Pressure                 -80655      3.0902e+05      1.9357e+05      1.6262e+05
v  k                    2.5307e-06          13.684         0.10461         0.11253
v  epsilon                0.026568      3.3444e+06          4220.6           76.21
v  TurbVisc             4.5503e-12         0.49488       0.0039544         0.04867
v  CourantNb              0.056271           58758           49.05          8.3146
v  FourierNb              0.023558      2.3655e+05              22         0.34823
v  total_pressure       4.1935e+05      8.0902e+05      6.9357e+05      6.6262e+05
v  Local Time Step           0.001        0.012561       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69508      2.4584e+05          71.051          8.6628


 TIME FOR THE TIME STEP              651:        0.80167E+02

===============================================================


 INSTANT    0.652000000E+01   TIME STEP NUMBER             652
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.265282284E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312643089E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12833E+03 0.10683E+02
   Friction velocity        uet   :  0.13614E-01 0.40878E+02
   Friction velocity        uk    :  0.27377E-01 0.40878E+02
   Dimensionless distance   yplus :  0.39015E-03 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15055
   Nb of faces within the viscous sub-layer     :       9541
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15984E+02      59   0.10521E+00   0.62905E+02 0.32634E+02 
c  Velocity[X]                                      0.94064E+01 
c  Velocity[Y]                                      0.22767E+02 
c  Velocity[Z]                                      0.30732E+02 
c  Pressure     0.12222E+00     435   0.31630E-01   0.92682E-01 0.99759E+00 
c  k            0.81757E+00      22   0.26165E-03   0.72973E-01 0.38648E+02 
c  epsilon      0.78016E+04      13   0.65025E-03   0.42574E+08 0.15627E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00032534                             3
a  epsilon                -0.80051                             1
a  Local Time Step      1.6793e-08                        281395


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.1908          17.645          2.1225         0.35383
v  Velocity[Y]              -35.39          44.814          1.2829          0.8402
v  Velocity[Z]             -56.665          33.696         -1.0457      -0.0036058
v  ǁVelocityǁ            0.0066058          59.946          7.2645          7.3055
v  Pressure                 -80795      3.0906e+05       1.936e+05      1.6266e+05
v  k                    2.4282e-06          13.575         0.10518         0.11283
v  epsilon                0.026903      3.5857e+06          4267.6           76.46
v  TurbVisc             3.9313e-12         0.49488       0.0039812        0.048733
v  CourantNb              0.019426           59550          49.138          8.3155
v  FourierNb              0.023571      2.3655e+05          21.998         0.34853
v  total_pressure        4.192e+05      8.0906e+05       6.936e+05      6.6266e+05
v  Local Time Step           0.001        0.012419       0.0010009       0.0010068


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55656      2.4697e+05          71.137           8.664


 TIME FOR THE TIME STEP              652:        0.69696E+02

===============================================================


 INSTANT    0.653000000E+01   TIME STEP NUMBER             653
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.733336599E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312563996E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89496E+02 0.10560E+02
   Friction velocity        uet   :  0.39804E-01 0.42547E+02
   Friction velocity        uk    :  0.49272E-01 0.42547E+02
   Dimensionless distance   yplus :  0.10881E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15061
   Nb of faces within the viscous sub-layer     :       9535
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15985E+02      56   0.10471E+00   0.63626E+02 0.32814E+02 
c  Velocity[X]                                      0.95345E+01 
c  Velocity[Y]                                      0.24148E+02 
c  Velocity[Z]                                      0.29944E+02 
c  Pressure     0.12186E+00     487   0.31523E-01   0.92299E-01 0.95222E+00 
c  k            0.81971E+00      21   0.31176E-03   0.73687E-01 0.38007E+02 
c  epsilon      0.78273E+04      13   0.38920E-03   0.15902E+08 0.96197E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.7257e-05                             1
a  epsilon                 -4.0579                             1
a  Local Time Step      1.7137e-08                        281389


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.1207          18.412          2.1187          0.3539
v  Velocity[Y]             -36.993          49.397          1.2936         0.83966
v  Velocity[Z]             -65.963          40.535         -1.0475      -0.0030793
v  ǁVelocityǁ             0.011587          72.837          7.2747          7.3059
v  Pressure                 -80729      3.0903e+05      1.9364e+05      1.6272e+05
v  k                    2.5419e-06          13.709         0.10553         0.11313
v  epsilon                0.027054      3.3299e+06          4246.1          76.713
v  TurbVisc             4.3963e-12         0.49488       0.0040099        0.048793
v  CourantNb              0.026915           58354          49.334          8.3167
v  FourierNb              0.023584      2.3655e+05          21.999         0.34901
v  total_pressure       4.1927e+05      8.0903e+05      6.9364e+05      6.6272e+05
v  Local Time Step           0.001        0.011211       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65322      2.4778e+05          71.333          8.6657


 TIME FOR THE TIME STEP              653:        0.77897E+02

===============================================================


 INSTANT    0.654000000E+01   TIME STEP NUMBER             654
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.123679871E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312494867E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12714E+03 0.11773E+02
   Friction velocity        uet   :  0.34701E-01 0.47032E+02
   Friction velocity        uk    :  0.49115E-01 0.47032E+02
   Dimensionless distance   yplus :  0.17407E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15083
   Nb of faces within the viscous sub-layer     :       9518
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15994E+02      57   0.10939E+00   0.63645E+02 0.32817E+02 
c  Velocity[X]                                      0.97401E+01 
c  Velocity[Y]                                      0.25722E+02 
c  Velocity[Z]                                      0.28183E+02 
c  Pressure     0.12198E+00     550   0.32091E-01   0.92402E-01 0.10716E+01 
c  k            0.82609E+00      24   0.23232E-03   0.83112E-01 0.40998E+02 
c  epsilon      0.78603E+04      13   0.18726E-03   0.35409E+07 0.44835E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.6314e-05                             1
a  epsilon                 -2.0999                             1
a  Local Time Step      1.6694e-08                        281387


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.0851          17.564          2.1202         0.35405
v  Velocity[Y]             -35.576          45.875          1.3032         0.83879
v  Velocity[Z]             -59.289           34.31         -1.0477       -0.002982
v  ǁVelocityǁ            0.0089695            62.6          7.2844          7.3062
v  Pressure                 -80419      3.0902e+05      1.9371e+05      1.6282e+05
v  k                    2.3159e-06          13.729         0.10614         0.11343
v  epsilon                0.027125      3.3318e+06          4267.3          77.045
v  TurbVisc             4.1248e-12         0.49488       0.0040445        0.048853
v  CourantNb              0.019681           59901          49.445           8.318
v  FourierNb              0.023597      2.3655e+05              22         0.34924
v  total_pressure       4.1958e+05      8.0902e+05      6.9371e+05      6.6282e+05
v  Local Time Step           0.001        0.012332       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61846      2.4385e+05          71.445          8.6673


 TIME FOR THE TIME STEP              654:        0.85580E+02

===============================================================


 INSTANT    0.655000000E+01   TIME STEP NUMBER             655
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.108281800E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312527968E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10206E+03 0.11595E+02
   Friction velocity        uet   :  0.38219E-01 0.46465E+02
   Friction velocity        uk    :  0.47487E-01 0.46465E+02
   Dimensionless distance   yplus :  0.21928E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15104
   Nb of faces within the viscous sub-layer     :       9482
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15983E+02      52   0.10636E+00   0.62163E+02 0.32423E+02 
c  Velocity[X]                                      0.94918E+01 
c  Velocity[Y]                                      0.24925E+02 
c  Velocity[Z]                                      0.27747E+02 
c  Pressure     0.12414E+00     521   0.33310E-01   0.94258E-01 0.10626E+01 
c  k            0.82602E+00      27   0.24923E-03   0.94917E-01 0.44007E+02 
c  epsilon      0.78544E+04      15   0.18241E-03   0.39489E+07 0.47913E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.6121e-05                             1
a  epsilon                 -2.2252                             1
a  Local Time Step      1.6952e-08                        281395


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.1833          18.536          2.1177         0.35366
v  Velocity[Y]              -36.57           30.43          1.3109         0.83835
v  Velocity[Z]             -65.017          41.021         -1.0449      -0.0035306
v  ǁVelocityǁ             0.016268          70.692          7.2872          7.3056
v  Pressure                 -80011      3.0901e+05      1.9376e+05      1.6289e+05
v  k                    2.3997e-06          13.244         0.10671         0.11369
v  epsilon                0.026959      3.3006e+06          4267.5          77.262
v  TurbVisc             3.9734e-12         0.49488       0.0040816        0.048911
v  CourantNb              0.039616           58989          49.561          8.3194
v  FourierNb              0.023609      2.3655e+05          22.001         0.34953
v  total_pressure       4.1999e+05      8.0901e+05      6.9376e+05      6.6289e+05
v  Local Time Step           0.001         0.01109       0.0010009       0.0010068


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91067      2.4619e+05          71.562          8.6689


 TIME FOR THE TIME STEP              655:        0.79948E+02

===============================================================


 INSTANT    0.656000000E+01   TIME STEP NUMBER             656
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.554895981E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312594419E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12554E+03 0.10128E+02
   Friction velocity        uet   :  0.39032E-01 0.43894E+02
   Friction velocity        uk    :  0.48040E-01 0.43894E+02
   Dimensionless distance   yplus :  0.27786E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15138
   Nb of faces within the viscous sub-layer     :       9470
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15987E+02      59   0.10226E+00   0.60107E+02 0.31886E+02 
c  Velocity[X]                                      0.92922E+01 
c  Velocity[Y]                                      0.22866E+02 
c  Velocity[Z]                                      0.27949E+02 
c  Pressure     0.12198E+00     403   0.33145E-01   0.92638E-01 0.99619E+00 
c  k            0.81738E+00      23   0.39320E-03   0.92834E-01 0.43971E+02 
c  epsilon      0.77911E+04      15   0.25538E-03   0.63004E+07 0.60718E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.2595e-05                             1
a  epsilon        
a  Local Time Step      1.7105e-08                        281407


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.2513          17.627          2.1178         0.35377
v  Velocity[Y]             -35.155          35.108          1.3148         0.83801
v  Velocity[Z]             -54.849           34.36         -1.0428      -0.0045878
v  ǁVelocityǁ             0.012027          58.095          7.2923          7.3064
v  Pressure                 -79670      3.0902e+05      1.9378e+05      1.6292e+05
v  k                    2.3753e-06          13.441          0.1071         0.11384
v  epsilon                0.026702      3.2628e+06          4273.2          77.292
v  TurbVisc             3.9975e-12         0.49488       0.0041183        0.048965
v  CourantNb              0.069404           58462          49.569           8.318
v  FourierNb              0.023622      2.3655e+05          22.004         0.34982
v  total_pressure       4.2033e+05      8.0902e+05      6.9378e+05      6.6292e+05
v  Local Time Step           0.001        0.012199       0.0010009       0.0010068


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40802      2.4725e+05          71.573          8.6678


 TIME FOR THE TIME STEP              656:        0.75851E+02

===============================================================


 INSTANT    0.657000000E+01   TIME STEP NUMBER             657
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.488052627E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312714226E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84746E+02 0.88915E+01
   Friction velocity        uet   :  0.36519E-01 0.41051E+02
   Friction velocity        uk    :  0.49590E-01 0.41051E+02
   Dimensionless distance   yplus :  0.18160E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15151
   Nb of faces within the viscous sub-layer     :       9477
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15995E+02      56   0.10380E+00   0.57752E+02 0.31173E+02 
c  Velocity[X]                                      0.91149E+01 
c  Velocity[Y]                                      0.20897E+02 
c  Velocity[Z]                                      0.27741E+02 
c  Pressure     0.12053E+00     465   0.33148E-01   0.91562E-01 0.10748E+01 
c  k            0.81262E+00      21   0.30925E-03   0.64370E-01 0.36375E+02 
c  epsilon      0.77775E+04      14   0.20619E-03   0.42299E+07 0.49611E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -4.407e-05                             1
a  epsilon                -0.95539                             1
a  Local Time Step      1.7449e-08                        281389


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.1957          18.418          2.1143         0.35356
v  Velocity[Y]              -35.05           33.58          1.3174         0.83857
v  Velocity[Z]               -65.9          40.697         -1.0382      -0.0061201
v  ǁVelocityǁ            0.0099388           71.56          7.2912          7.3072
v  Pressure                 -79411      3.0903e+05      1.9377e+05      1.6295e+05
v  k                    2.5657e-06          12.918         0.10737         0.11398
v  epsilon                0.026581       3.215e+06          4272.2          77.337
v  TurbVisc             3.9549e-12         0.49488       0.0041481         0.04901
v  CourantNb            0.00085604           57308          49.608          8.3197
v  FourierNb              0.023634      2.3655e+05          22.005         0.35009
v  total_pressure       4.2059e+05      8.0903e+05      6.9377e+05      6.6295e+05
v  Local Time Step           0.001        0.012064       0.0010009       0.0010069


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51089      2.4781e+05          71.614          8.6698


 TIME FOR THE TIME STEP              657:        0.86567E+02

===============================================================


 INSTANT    0.658000000E+01   TIME STEP NUMBER             658
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.551502043E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312912964E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12834E+03 0.93178E+01
   Friction velocity        uet   :  0.33787E-01 0.37755E+02
   Friction velocity        uk    :  0.50971E-01 0.37755E+02
   Dimensionless distance   yplus :  0.10347E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15147
   Nb of faces within the viscous sub-layer     :       9458
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15997E+02      64   0.10336E+00   0.56422E+02 0.30864E+02 
c  Velocity[X]                                      0.91622E+01 
c  Velocity[Y]                                      0.19943E+02 
c  Velocity[Z]                                      0.27317E+02 
c  Pressure     0.12092E+00     423   0.32888E-01   0.91930E-01 0.11701E+01 
c  k            0.80975E+00      22   0.16941E-03   0.32759E-01 0.26218E+02 
c  epsilon      0.77290E+04      14   0.18857E-03   0.33796E+07 0.44698E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.2078e-05                             1
a  epsilon        
a  Local Time Step      1.6777e-08                        281405


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.2595          17.612          2.1112         0.35336
v  Velocity[Y]             -32.446           36.67          1.3174         0.83963
v  Velocity[Z]              -59.22          34.049         -1.0315      -0.0081779
v  ǁVelocityǁ             0.014956          62.633          7.2873          7.3084
v  Pressure                 -78882      3.0902e+05      1.9371e+05      1.6299e+05
v  k                    2.4257e-06          12.926         0.10743         0.11412
v  epsilon                0.026707      3.1984e+06          4260.7          77.307
v  TurbVisc             4.1097e-12         0.49488       0.0041717        0.049051
v  CourantNb             0.0048328           59606          49.565          8.3194
v  FourierNb              0.023647      2.3655e+05          22.005         0.35038
v  total_pressure       4.2112e+05      8.0902e+05      6.9371e+05      6.6299e+05
v  Local Time Step           0.001        0.013271       0.0010009        0.001007


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61907      2.4387e+05           71.57          8.6698


 TIME FOR THE TIME STEP              658:        0.85807E+02

===============================================================


 INSTANT    0.659000000E+01   TIME STEP NUMBER             659
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.633194590E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313186965E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10167E+03 0.88694E+01
   Friction velocity        uet   :  0.35156E-01 0.33239E+02
   Friction velocity        uk    :  0.37000E-01 0.33239E+02
   Dimensionless distance   yplus :  0.18288E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15132
   Nb of faces within the viscous sub-layer     :       9450
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16005E+02      54   0.10477E+00   0.53653E+02 0.30081E+02 
c  Velocity[X]                                      0.87102E+01 
c  Velocity[Y]                                      0.18683E+02 
c  Velocity[Z]                                      0.26260E+02 
c  Pressure     0.11812E+00    1208   0.31930E-01   0.89908E-01 0.90082E+01 
c  k            0.80882E+00      23   0.13520E-03   0.31713E-01 0.25735E+02 
c  epsilon      0.76605E+04      14   0.19848E-03   0.70824E+07 0.65131E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.3537e-05                             2
a  epsilon        
a  Local Time Step      1.6954e-08                        281377


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.2394          18.377           2.107         0.35237
v  Velocity[Y]             -36.808          36.116          1.3114          0.8399
v  Velocity[Z]             -65.819          39.682         -1.0234      -0.0069904
v  ǁVelocityǁ             0.012894          71.453          7.2767           7.304
v  Pressure                 -80546      3.0673e+05      1.9153e+05      1.6124e+05
v  k                     2.179e-06          12.802         0.10725         0.11426
v  epsilon                0.026879      3.1402e+06          4223.8          77.307
v  TurbVisc             4.3508e-12         0.49488       0.0041907        0.049088
v  CourantNb              0.048532           58984           49.48          8.3201
v  FourierNb              0.023662      2.3655e+05          22.005         0.35051
v  total_pressure       4.1945e+05      8.0673e+05      6.9153e+05      6.6124e+05
v  Local Time Step           0.001        0.012362       0.0010009       0.0010068


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59421      2.4737e+05          71.485          8.6706


 TIME FOR THE TIME STEP              659:        0.11346E+03

===============================================================


 INSTANT    0.660000000E+01   TIME STEP NUMBER             660
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.538666313E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312838998E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12830E+03 0.95770E+01
   Friction velocity        uet   :  0.35707E-01 0.30752E+02
   Friction velocity        uk    :  0.50509E-01 0.30752E+02
   Dimensionless distance   yplus :  0.15092E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15114
   Nb of faces within the viscous sub-layer     :       9479
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15991E+02      63   0.10216E+00   0.51752E+02 0.29593E+02 
c  Velocity[X]                                      0.75076E+01 
c  Velocity[Y]                                      0.17649E+02 
c  Velocity[Z]                                      0.26596E+02 
c  Pressure     0.11123E+00     518   0.29884E-01   0.84678E-01 0.13903E+01 
c  k            0.80823E+00      23   0.13240E-03   0.28924E-01 0.24543E+02 
c  epsilon      0.75690E+04      14   0.24030E-03   0.17820E+08 0.10365E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -1.645e-05                             1
a  epsilon        
a  Local Time Step       1.687e-08                        281387


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.1437          17.595          2.1065         0.35206
v  Velocity[Y]             -39.714          38.359          1.3032         0.84049
v  Velocity[Z]             -50.064          34.454         -1.0155      -0.0070612
v  ǁVelocityǁ             0.012399          53.469          7.2697          7.3025
v  Pressure                 -80004      3.0664e+05      1.9147e+05      1.6133e+05
v  k                    2.3741e-06          13.194         0.10693         0.11438
v  epsilon                0.027229      3.1033e+06          4210.3          77.213
v  TurbVisc             3.9378e-12         0.49488       0.0042015        0.049122
v  CourantNb              0.016977           59278          49.393          8.3128
v  FourierNb              0.023677      2.3655e+05          22.003         0.35079
v  total_pressure          4.2e+05      8.0664e+05      6.9147e+05      6.6133e+05
v  Local Time Step           0.001        0.013437       0.0010009       0.0010068


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66592      2.4842e+05          71.395          8.6636


 TIME FOR THE TIME STEP              660:        0.73607E+02

===============================================================


 INSTANT    0.661000000E+01   TIME STEP NUMBER             661
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.569823225E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313044095E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83433E+02 0.93459E+01
   Friction velocity        uet   :  0.26967E-01 0.26918E+02
   Friction velocity        uk    :  0.53263E-01 0.26918E+02
   Dimensionless distance   yplus :  0.16876E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15134
   Nb of faces within the viscous sub-layer     :       9479
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15989E+02      61   0.10515E+00   0.50737E+02 0.29277E+02 
c  Velocity[X]                                      0.74004E+01 
c  Velocity[Y]                                      0.17207E+02 
c  Velocity[Z]                                      0.26130E+02 
c  Pressure     0.10755E+00     975   0.28453E-01   0.81838E-01 0.31348E+01 
c  k            0.80827E+00      22   0.13762E-03   0.35606E-01 0.27192E+02 
c  epsilon      0.75214E+04      14   0.24582E-03   0.96804E+07 0.76772E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1178e-05                             1
a  epsilon                 -4.3124                             1
a  Local Time Step      1.6909e-08                        281383


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.2128           18.72          2.1042         0.35203
v  Velocity[Y]             -35.982          36.531          1.2869         0.84114
v  Velocity[Z]             -63.486          44.293         -1.0078      -0.0068115
v  ǁVelocityǁ             0.023533          68.586          7.2555          7.3002
v  Pressure                 -80341      3.0582e+05       1.907e+05      1.6082e+05
v  k                    2.3659e-06          13.405         0.10656         0.11451
v  epsilon                0.027915      3.0449e+06          4195.9          77.169
v  TurbVisc             4.1669e-12         0.49488       0.0042034        0.049153
v  CourantNb             0.0035573           59140          49.272          8.3133
v  FourierNb              0.023694      2.3655e+05          22.004          0.3508
v  total_pressure       4.1966e+05      8.0582e+05       6.907e+05      6.6082e+05
v  Local Time Step           0.001         0.01358        0.001001       0.0010068


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6514       2.469e+05          71.276          8.6641


 TIME FOR THE TIME STEP              661:        0.10711E+03

===============================================================


 INSTANT    0.662000000E+01   TIME STEP NUMBER             662
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.991031193E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313039106E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10685E+03 0.95991E+01
   Friction velocity        uet   :  0.29159E-01 0.25805E+02
   Friction velocity        uk    :  0.53867E-01 0.25805E+02
   Dimensionless distance   yplus :  0.16698E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15114
   Nb of faces within the viscous sub-layer     :       9506
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15993E+02      55   0.10758E+00   0.49094E+02 0.28853E+02 
c  Velocity[X]                                      0.72747E+01 
c  Velocity[Y]                                      0.16698E+02 
c  Velocity[Z]                                      0.25121E+02 
c  Pressure     0.10318E+00     950   0.26869E-01   0.78438E-01 0.25106E+01 
c  k            0.80901E+00      21   0.17284E-03   0.42004E-01 0.29453E+02 
c  epsilon      0.75061E+04      14   0.17843E-03   0.49922E+07 0.55214E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010595                             3
a  epsilon                 -71.765                             4
a  Local Time Step      1.6777e-08                        281377


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.2017          17.653          2.0997         0.35196
v  Velocity[Y]             -33.295          39.901          1.2736          0.8419
v  Velocity[Z]             -51.851          34.659        -0.99738      -0.0066533
v  ǁVelocityǁ             0.015552          55.223          7.2429          7.2996
v  Pressure                 -81675      3.0521e+05       1.901e+05      1.6043e+05
v  k                    2.1179e-06          13.892         0.10598         0.11466
v  epsilon                0.028729      3.0696e+06          4168.1           77.05
v  TurbVisc             3.9928e-12         0.49488       0.0042042        0.049183
v  CourantNb               0.07364           59604          49.107          8.3089
v  FourierNb              0.023713      2.3655e+05          22.002         0.35087
v  total_pressure       4.1833e+05      8.0521e+05       6.901e+05      6.6043e+05
v  Local Time Step           0.001        0.012629       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77619      2.4687e+05          71.109          8.6598


 TIME FOR THE TIME STEP              662:        0.10537E+03

===============================================================


 INSTANT    0.663000000E+01   TIME STEP NUMBER             663
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.615974079E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313058325E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.82195E+02 0.95384E+01
   Friction velocity        uet   :  0.23871E-01 0.23508E+02
   Friction velocity        uk    :  0.52897E-01 0.23508E+02
   Dimensionless distance   yplus :  0.16395E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15121
   Nb of faces within the viscous sub-layer     :       9527
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15978E+02      53   0.10323E+00   0.49148E+02 0.28800E+02 
c  Velocity[X]                                      0.74796E+01 
c  Velocity[Y]                                      0.16494E+02 
c  Velocity[Z]                                      0.25174E+02 
c  Pressure     0.10387E+00     429   0.26424E-01   0.79125E-01 0.92192E+00 
c  k            0.81015E+00      21   0.17008E-03   0.47204E-01 0.31052E+02 
c  epsilon      0.74640E+04      14   0.19424E-03   0.45296E+07 0.52806E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015655                             2
a  epsilon                  -206.6                             5
a  Local Time Step      1.7275e-08                        281382


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.0843          18.476           2.097         0.35172
v  Velocity[Y]             -35.667          36.145          1.2636         0.84272
v  Velocity[Z]             -65.389           38.43        -0.99165      -0.0075979
v  ǁVelocityǁ             0.012094          71.054          7.2352          7.2987
v  Pressure                 -84763      3.0515e+05      1.9005e+05      1.6045e+05
v  k                     2.132e-06          14.103         0.10554         0.11485
v  epsilon                0.028592      3.0413e+06          4152.5          77.018
v  TurbVisc             4.0909e-12         0.49488       0.0042015        0.049214
v  CourantNb             0.0035989           57887          48.937          8.3084
v  FourierNb              0.023735      2.3655e+05          22.003         0.35099
v  total_pressure       4.1524e+05      8.0515e+05      6.9005e+05      6.6045e+05
v  Local Time Step           0.001        0.012249       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88544      2.4805e+05           70.94          8.6593


 TIME FOR THE TIME STEP              663:        0.82249E+02

===============================================================


 INSTANT    0.664000000E+01   TIME STEP NUMBER             664
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.764420008E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313145840E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12694E+03 0.98588E+01
   Friction velocity        uet   :  0.13029E-01 0.22307E+02
   Friction velocity        uk    :  0.48422E-01 0.22307E+02
   Dimensionless distance   yplus :  0.15246E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15093
   Nb of faces within the viscous sub-layer     :       9546
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15984E+02      57   0.99941E-01   0.50054E+02 0.29109E+02 
c  Velocity[X]                                      0.73537E+01 
c  Velocity[Y]                                      0.16273E+02 
c  Velocity[Z]                                      0.26428E+02 
c  Pressure     0.10086E+00     365   0.25500E-01   0.76830E-01 0.83282E+00 
c  k            0.81016E+00      22   0.23504E-03   0.47710E-01 0.31156E+02 
c  epsilon      0.74483E+04      14   0.32466E-03   0.64840E+07 0.63235E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00056253                             2
a  epsilon        
a  Local Time Step      1.7343e-08                        281399


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.0761           17.63          2.0952         0.35131
v  Velocity[Y]             -37.553          40.062          1.2547         0.84311
v  Velocity[Z]             -56.116          34.374        -0.98984      -0.0091496
v  ǁVelocityǁ             0.015557          59.266          7.2317          7.2999
v  Pressure                 -86849      3.0513e+05      1.9002e+05      1.6046e+05
v  k                    2.2569e-06          14.211         0.10523         0.11502
v  epsilon                0.030304      3.0392e+06          4146.9          77.006
v  TurbVisc             4.0792e-12         0.49488       0.0041942        0.049248
v  CourantNb              0.012326           57659          48.889          8.3066
v  FourierNb              0.023758      2.3655e+05          22.005         0.35115
v  total_pressure       4.1315e+05      8.0513e+05      6.9002e+05      6.6046e+05
v  Local Time Step           0.001        0.013349       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77069      2.4952e+05          70.894          8.6577


 TIME FOR THE TIME STEP              664:        0.71861E+02

===============================================================


 INSTANT    0.665000000E+01   TIME STEP NUMBER             665
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.924206036E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313273427E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88089E+02 0.94482E+01
   Friction velocity        uet   :  0.25332E-01 0.22175E+02
   Friction velocity        uk    :  0.40944E-01 0.22175E+02
   Dimensionless distance   yplus :  0.16315E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15101
   Nb of faces within the viscous sub-layer     :       9562
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15988E+02      64   0.10419E+00   0.49638E+02 0.28944E+02 
c  Velocity[X]                                      0.72318E+01 
c  Velocity[Y]                                      0.16587E+02 
c  Velocity[Z]                                      0.25820E+02 
c  Pressure     0.99982E-01     915   0.25457E-01   0.76054E-01 0.56649E+01 
c  k            0.80958E+00      21   0.17753E-03   0.45735E-01 0.30365E+02 
c  epsilon      0.74471E+04      13   0.18351E-03   0.92181E+07 0.75462E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.7835e-05                             2
a  epsilon                 -35.082                             3
a  Local Time Step      1.7145e-08                        281404


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.1141          18.006          2.0936         0.35039
v  Velocity[Y]             -37.801          35.845          1.2457         0.84347
v  Velocity[Z]             -65.157          42.389        -0.99026      -0.0080864
v  ǁVelocityǁ             0.017752          70.828          7.2271          7.2979
v  Pressure                 -89264      3.0375e+05      1.8867e+05      1.5936e+05
v  k                    2.4214e-06          14.004         0.10502         0.11527
v  epsilon                0.030938       3.058e+06          4143.3          77.096
v  TurbVisc             4.0704e-12         0.49488       0.0041857        0.049281
v  CourantNb              0.014843           58327          48.862          8.3085
v  FourierNb              0.023783      2.3655e+05          22.008          0.3513
v  total_pressure       4.1074e+05      8.0375e+05      6.8867e+05      6.5936e+05
v  Local Time Step           0.001        0.014684       0.0010009       0.0010069


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78843      2.4924e+05           70.87          8.6598


 TIME FOR THE TIME STEP              665:        0.92983E+02

===============================================================


 INSTANT    0.666000000E+01   TIME STEP NUMBER             666
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.325001038E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313045365E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12650E+03 0.88920E+01
   Friction velocity        uet   :  0.34558E-01 0.22458E+02
   Friction velocity        uk    :  0.47735E-01 0.22458E+02
   Dimensionless distance   yplus :  0.19285E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15082
   Nb of faces within the viscous sub-layer     :       9592
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15976E+02      62   0.10478E+00   0.50477E+02 0.29252E+02 
c  Velocity[X]                                      0.76335E+01 
c  Velocity[Y]                                      0.17406E+02 
c  Velocity[Z]                                      0.25437E+02 
c  Pressure     0.10289E+00     262   0.26096E-01   0.78249E-01 0.70445E+00 
c  k            0.80952E+00      20   0.15531E-03   0.39508E-01 0.28121E+02 
c  epsilon      0.74325E+04      15   0.30928E-03   0.87056E+07 0.73427E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.3153e-05                             2
a  epsilon        
a  Local Time Step      1.7053e-08                        281393


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.1315          17.301          2.0951         0.35017
v  Velocity[Y]             -39.444          40.668           1.245         0.84388
v  Velocity[Z]             -52.884          35.038        -0.99513      -0.0074687
v  ǁVelocityǁ             0.016733          56.005          7.2287          7.2958
v  Pressure                 -89372       3.038e+05      1.8865e+05      1.5938e+05
v  k                    2.2416e-06          13.485         0.10513         0.11551
v  epsilon                0.031505      3.0864e+06          4139.7          77.179
v  TurbVisc             4.0865e-12         0.49488       0.0041827        0.049323
v  CourantNb              0.031172           58642          48.838          8.3055
v  FourierNb              0.023809      2.3655e+05          22.008         0.35147
v  total_pressure       4.1063e+05       8.038e+05      6.8865e+05      6.5938e+05
v  Local Time Step           0.001        0.015328       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.84504      2.4908e+05          70.846           8.657


 TIME FOR THE TIME STEP              666:        0.69794E+02

===============================================================


 INSTANT    0.667000000E+01   TIME STEP NUMBER             667
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.223168386E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313021474E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85209E+02 0.90497E+01
   Friction velocity        uet   :  0.25852E-01 0.22270E+02
   Friction velocity        uk    :  0.45816E-01 0.22270E+02
   Dimensionless distance   yplus :  0.13342E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15089
   Nb of faces within the viscous sub-layer     :       9593
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15961E+02      59   0.10365E+00   0.50553E+02 0.29288E+02 
c  Velocity[X]                                      0.77952E+01 
c  Velocity[Y]                                      0.17407E+02 
c  Velocity[Z]                                      0.25350E+02 
c  Pressure     0.10396E+00     599   0.26439E-01   0.79185E-01 0.66110E+00 
c  k            0.81137E+00      21   0.15711E-03   0.47810E-01 0.30790E+02 
c  epsilon      0.74662E+04      14   0.18442E-03   0.50707E+07 0.55886E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.0026e-05                             3
a  epsilon                 -31.429                             2
a  Local Time Step      1.6811e-08                        281353


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.202              18          2.0994         0.34973
v  Velocity[Y]             -34.019          34.018          1.2508         0.84414
v  Velocity[Z]              -62.86          39.928         -1.0048       -0.006681
v  ǁVelocityǁ             0.011998          68.444          7.2344          7.2943
v  Pressure                 -89052       3.038e+05      1.8863e+05       1.594e+05
v  k                    1.1668e-06          13.229         0.10536         0.11583
v  epsilon                0.031953      3.1144e+06          4153.2          77.457
v  TurbVisc             4.0924e-12         0.49488       0.0041816        0.049365
v  CourantNb              0.066645           59487           48.88          8.3046
v  FourierNb              0.023834      2.3655e+05           22.01         0.35128
v  total_pressure       4.1095e+05       8.038e+05      6.8863e+05       6.594e+05
v  Local Time Step           0.001        0.014494       0.0010009       0.0010068


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.84254      2.5047e+05           70.89          8.6559


 TIME FOR THE TIME STEP              667:        0.88061E+02

===============================================================


 INSTANT    0.668000000E+01   TIME STEP NUMBER             668
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.527925362E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312938593E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11909E+03 0.93251E+01
   Friction velocity        uet   :  0.14523E-01 0.20730E+02
   Friction velocity        uk    :  0.39521E-01 0.20730E+02
   Dimensionless distance   yplus :  0.22540E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15084
   Nb of faces within the viscous sub-layer     :       9589
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15960E+02      54   0.10592E+00   0.49277E+02 0.28916E+02 
c  Velocity[X]                                      0.75761E+01 
c  Velocity[Y]                                      0.16881E+02 
c  Velocity[Z]                                      0.24820E+02 
c  Pressure     0.10520E+00     396   0.26666E-01   0.80125E-01 0.68584E+00 
c  k            0.81120E+00      21   0.16772E-03   0.40846E-01 0.28359E+02 
c  epsilon      0.74660E+04      14   0.19503E-03   0.57711E+07 0.59639E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016196                             3
a  epsilon               -0.016704                             1
a  Local Time Step      1.7085e-08                        281364


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.2926          17.387          2.1005         0.34988
v  Velocity[Y]             -32.416           41.32          1.2569         0.84394
v  Velocity[Z]              -57.73          35.272          -1.015       -0.005582
v  ǁVelocityǁ             0.027798          61.148          7.2433          7.2927
v  Pressure                 -89040      3.0383e+05      1.8863e+05      1.5942e+05
v  k                    2.6109e-07          13.086         0.10546         0.11611
v  epsilon                0.016704      3.1461e+06          4150.4          77.631
v  TurbVisc             4.0643e-12         0.49488        0.004176        0.049414
v  CourantNb              0.033873           58530          48.911          8.3043
v  FourierNb               0.02386      2.3655e+05          22.007         0.35152
v  total_pressure       4.1096e+05      8.0383e+05      6.8863e+05      6.5942e+05
v  Local Time Step           0.001        0.015943       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71452      2.4691e+05          70.918          8.6559


 TIME FOR THE TIME STEP              668:        0.82469E+02

===============================================================


 INSTANT    0.669000000E+01   TIME STEP NUMBER             669
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.188218664E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312880313E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99082E+02 0.88310E+01
   Friction velocity        uet   :  0.19500E-01 0.19519E+02
   Friction velocity        uk    :  0.46407E-01 0.19519E+02
   Dimensionless distance   yplus :  0.23824E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15088
   Nb of faces within the viscous sub-layer     :       9566
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15954E+02      59   0.10283E+00   0.49104E+02 0.28866E+02 
c  Velocity[X]                                      0.75431E+01 
c  Velocity[Y]                                      0.16334E+02 
c  Velocity[Z]                                      0.25227E+02 
c  Pressure     0.10510E+00     350   0.26626E-01   0.80022E-01 0.70503E+00 
c  k            0.81313E+00      22   0.19106E-03   0.44201E-01 0.29337E+02 
c  epsilon      0.74723E+04      12   0.35537E-03   0.11554E+08 0.84297E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.9371e-05                             2
a  epsilon        
a  Local Time Step      1.7217e-08                        281386


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.3426          18.287          2.1068         0.34959
v  Velocity[Y]             -35.959          37.671          1.2611         0.84379
v  Velocity[Z]             -64.156           41.37         -1.0256      -0.0042986
v  ǁVelocityǁ              0.01028          69.791           7.253          7.2908
v  Pressure                 -89282      3.0386e+05      1.8864e+05      1.5941e+05
v  k                    2.4797e-06          12.639         0.10571         0.11648
v  epsilon               0.0058361      3.1729e+06          4168.3          77.947
v  TurbVisc             4.1516e-12         0.49488       0.0041692        0.049464
v  CourantNb              0.025068           58082          48.986          8.3042
v  FourierNb              0.023883      2.3655e+05          22.001         0.35148
v  total_pressure       4.1072e+05      8.0386e+05      6.8864e+05      6.5941e+05
v  Local Time Step           0.001         0.01605       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66481      2.4721e+05          70.988          8.6557


 TIME FOR THE TIME STEP              669:        0.75641E+02

===============================================================


 INSTANT    0.670000000E+01   TIME STEP NUMBER             670
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.106077522E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312717460E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12279E+03 0.10114E+02
   Friction velocity        uet   :  0.34425E-01 0.17196E+02
   Friction velocity        uk    :  0.38800E-01 0.17196E+02
   Dimensionless distance   yplus :  0.18593E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15114
   Nb of faces within the viscous sub-layer     :       9551
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15947E+02      63   0.10215E+00   0.49582E+02 0.29034E+02 
c  Velocity[X]                                      0.76748E+01 
c  Velocity[Y]                                      0.15870E+02 
c  Velocity[Z]                                      0.26038E+02 
c  Pressure     0.10214E+00     368   0.25971E-01   0.77833E-01 0.66423E+00 
c  k            0.81531E+00      23   0.20652E-03   0.53711E-01 0.32217E+02 
c  epsilon      0.75179E+04      15   0.96254E-03   0.14545E+08 0.94023E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014029                             2
a  epsilon                 -31.513                             1
a  Local Time Step      1.7133e-08                        281414


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.3571          17.141          2.1066         0.34932
v  Velocity[Y]             -36.807          41.383          1.2621         0.84394
v  Velocity[Z]             -53.208          34.792         -1.0295      -0.0030157
v  ǁVelocityǁ             0.021956          56.367          7.2565          7.2887
v  Pressure                 -88874       3.039e+05      1.8867e+05      1.5942e+05
v  k                    2.3069e-06          12.918         0.10588         0.11687
v  epsilon                0.032904      3.2108e+06          4176.7           78.27
v  TurbVisc             4.0858e-12         0.49488       0.0041732        0.049525
v  CourantNb                     0           58367          49.111           8.303
v  FourierNb              0.023904      2.3655e+05          21.999          0.3518
v  total_pressure       4.1113e+05       8.039e+05      6.8867e+05      6.5942e+05
v  Local Time Step           0.001        0.013961       0.0010009       0.0010066


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83562      2.4834e+05           71.11          8.6548


 TIME FOR THE TIME STEP              670:        0.74267E+02

===============================================================


 INSTANT    0.671000000E+01   TIME STEP NUMBER             671
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.189271759E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312580014E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80391E+02 0.94760E+01
   Friction velocity        uet   :  0.24943E-01 0.25412E+02
   Friction velocity        uk    :  0.45755E-01 0.25412E+02
   Dimensionless distance   yplus :  0.30738E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15097
   Nb of faces within the viscous sub-layer     :       9572
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15940E+02      63   0.10346E+00   0.49452E+02 0.28993E+02 
c  Velocity[X]                                      0.74443E+01 
c  Velocity[Y]                                      0.16596E+02 
c  Velocity[Z]                                      0.25412E+02 
c  Pressure     0.10258E+00     689   0.26034E-01   0.78031E-01 0.38761E+01 
c  k            0.81788E+00      21   0.22559E-03   0.45088E-01 0.29399E+02 
c  epsilon      0.75371E+04      13   0.64802E-03   0.17440E+08 0.10276E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018277                             2
a  epsilon        
a  Local Time Step      1.6928e-08                        281395


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.3825          18.213          2.1102         0.34892
v  Velocity[Y]             -39.388          40.037          1.2616          0.8446
v  Velocity[Z]             -64.104          37.432         -1.0355       -0.003088
v  ǁVelocityǁ             0.011743          69.716          7.2619          7.2889
v  Pressure                 -87428      3.0486e+05       1.896e+05      1.6015e+05
v  k                    4.5925e-07          13.126         0.10618         0.11725
v  epsilon                0.033025      3.2079e+06          4189.5          78.619
v  TurbVisc             4.0604e-12         0.49488       0.0041873         0.04959
v  CourantNb              0.039672           59075          49.136          8.3023
v  FourierNb              0.023924      2.3655e+05          21.998         0.35191
v  total_pressure       4.1257e+05      8.0486e+05       6.896e+05      6.6015e+05
v  Local Time Step           0.001        0.014644       0.0010009       0.0010066


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75639      2.4938e+05          71.134          8.6542


 TIME FOR THE TIME STEP              671:        0.84945E+02

===============================================================


 INSTANT    0.672000000E+01   TIME STEP NUMBER             672
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.502095603E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312549709E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12270E+03 0.10079E+02
   Friction velocity        uet   :  0.41521E-01 0.29375E+02
   Friction velocity        uk    :  0.47949E-01 0.29375E+02
   Dimensionless distance   yplus :  0.20483E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15117
   Nb of faces within the viscous sub-layer     :       9564
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15940E+02      53   0.10428E+00   0.49627E+02 0.29052E+02 
c  Velocity[X]                                      0.77112E+01 
c  Velocity[Y]                                      0.17160E+02 
c  Velocity[Z]                                      0.24756E+02 
c  Pressure     0.10281E+00     399   0.26023E-01   0.78164E-01 0.62511E+00 
c  k            0.81890E+00      23   0.27067E-03   0.48810E-01 0.30572E+02 
c  epsilon      0.75394E+04      16   0.32974E-03   0.13971E+08 0.92064E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.4057e-05                             2
a  epsilon        
a  Local Time Step      1.6902e-08                        281398


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.4118          17.098          2.1125         0.34859
v  Velocity[Y]             -35.211          39.995          1.2608         0.84507
v  Velocity[Z]             -57.143          35.022         -1.0355      -0.0027926
v  ǁVelocityǁ             0.015137          60.336          7.2634          7.2882
v  Pressure                 -87094      3.0501e+05      1.8964e+05      1.6017e+05
v  k                     2.222e-06          13.716         0.10644         0.11758
v  epsilon               0.0072031      3.2151e+06          4167.8          78.882
v  TurbVisc             3.3597e-12         0.49488       0.0042044        0.049655
v  CourantNb              0.012027           59166          49.169          8.3025
v  FourierNb              0.023941      2.3655e+05          21.999         0.35212
v  total_pressure       4.1291e+05      8.0501e+05      6.8964e+05      6.6017e+05
v  Local Time Step           0.001        0.013187       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90296      2.4832e+05          71.168          8.6547


 TIME FOR THE TIME STEP              672:        0.60105E+02

===============================================================


 INSTANT    0.673000000E+01   TIME STEP NUMBER             673
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.107471276E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312548158E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97162E+02 0.97840E+01
   Friction velocity        uet   :  0.41636E-01 0.21008E+02
   Friction velocity        uk    :  0.55627E-01 0.21008E+02
   Dimensionless distance   yplus :  0.22012E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15100
   Nb of faces within the viscous sub-layer     :       9552
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15936E+02      56   0.10480E+00   0.50091E+02 0.29182E+02 
c  Velocity[X]                                      0.74192E+01 
c  Velocity[Y]                                      0.17023E+02 
c  Velocity[Z]                                      0.25649E+02 
c  Pressure     0.10297E+00     786   0.26320E-01   0.78279E-01 0.46539E+01 
c  k            0.82112E+00      22   0.24319E-03   0.51160E-01 0.31282E+02 
c  epsilon      0.75129E+04      12   0.38128E-03   0.16266E+08 0.99257E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.3239e-05                             3
a  epsilon                 -31.369                             3
a  Local Time Step      1.6783e-08                        281386


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.3811          18.196          2.1153         0.34843
v  Velocity[Y]             -34.968          34.647          1.2555          0.8458
v  Velocity[Z]              -63.91          39.618         -1.0344      -0.0041212
v  ǁVelocityǁ             0.010098          69.554          7.2624          7.2897
v  Pressure                 -85391      3.0623e+05      1.9073e+05      1.6107e+05
v  k                    2.3027e-06          14.005          0.1067         0.11784
v  epsilon                0.033019      3.2005e+06            4166          79.083
v  TurbVisc             3.9778e-12         0.49488       0.0042208        0.049717
v  CourantNb              0.017102           59585          49.162          8.3018
v  FourierNb              0.023957      2.3655e+05          21.998         0.35244
v  total_pressure       4.1461e+05      8.0623e+05      6.9073e+05      6.6107e+05
v  Local Time Step           0.001        0.014506       0.0010009       0.0010066


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64046      2.4922e+05          71.161          8.6543


 TIME FOR THE TIME STEP              673:        0.95845E+02

===============================================================


 INSTANT    0.674000000E+01   TIME STEP NUMBER             674
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.560234428E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312707197E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12238E+03 0.10965E+02
   Friction velocity        uet   :  0.21375E-01 0.22385E+02
   Friction velocity        uk    :  0.26952E-01 0.22385E+02
   Dimensionless distance   yplus :  0.11064E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15111
   Nb of faces within the viscous sub-layer     :       9547
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15942E+02      60   0.10360E+00   0.51497E+02 0.29593E+02 
c  Velocity[X]                                      0.73200E+01 
c  Velocity[Y]                                      0.17585E+02 
c  Velocity[Z]                                      0.26591E+02 
c  Pressure     0.10229E+00     456   0.25735E-01   0.77790E-01 0.59968E+00 
c  k            0.82469E+00      22   0.27795E-03   0.51921E-01 0.30901E+02 
c  epsilon      0.75416E+04      13   0.43961E-03   0.10268E+08 0.78575E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.9177e-05                             1
a  epsilon        
a  Local Time Step      1.6815e-08                        281378


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.4291           17.06          2.1176         0.34815
v  Velocity[Y]             -38.512          42.147            1.25         0.84625
v  Velocity[Z]             -53.752           34.82         -1.0339      -0.0050425
v  ǁVelocityǁ            0.0068865          56.913          7.2608          7.2906
v  Pressure                 -84403      3.0632e+05      1.9074e+05      1.6107e+05
v  k                    2.3795e-06          13.895          0.1068         0.11798
v  epsilon                0.021217      3.2248e+06          4154.5          79.186
v  TurbVisc             3.9289e-12         0.49488        0.004237        0.049775
v  CourantNb              0.031754           59470          49.112          8.3032
v  FourierNb              0.023971      2.3655e+05              22         0.35254
v  total_pressure        4.156e+05      8.0632e+05      6.9074e+05      6.6107e+05
v  Local Time Step           0.001        0.013626       0.0010009       0.0010064


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0537      2.4528e+05          71.112          8.6557


 TIME FOR THE TIME STEP              674:        0.74913E+02

===============================================================


 INSTANT    0.675000000E+01   TIME STEP NUMBER             675
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.691078249E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312834870E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.81565E+02 0.10764E+02
   Friction velocity        uet   :  0.41822E-01 0.25301E+02
   Friction velocity        uk    :  0.42537E-01 0.25301E+02
   Dimensionless distance   yplus :  0.19620E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15101
   Nb of faces within the viscous sub-layer     :       9546
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15938E+02      54   0.10241E+00   0.53069E+02 0.30039E+02 
c  Velocity[X]                                      0.76178E+01 
c  Velocity[Y]                                      0.18345E+02 
c  Velocity[Z]                                      0.27107E+02 
c  Pressure     0.10321E+00     329   0.26044E-01   0.78379E-01 0.60509E+00 
c  k            0.82799E+00      23   0.36432E-03   0.49333E-01 0.30518E+02 
c  epsilon      0.75634E+04      16   0.99925E-03   0.16756E+08 0.10009E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.7221e-05                             1
a  epsilon                 -20.511                             1
a  Local Time Step      1.6873e-08                        281393


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5036          18.262          2.1197         0.34789
v  Velocity[Y]              -33.03          36.214          1.2439          0.8463
v  Velocity[Z]             -65.073          40.695         -1.0345       -0.005966
v  ǁVelocityǁ            0.0078428          70.749          7.2577          7.2916
v  Pressure                 -83758      3.0635e+05      1.9073e+05      1.6106e+05
v  k                    2.6072e-06          13.617         0.10711          0.1181
v  epsilon                0.033022      3.1931e+06          4181.1          79.321
v  TurbVisc             4.6385e-12         0.49488       0.0042508        0.049821
v  CourantNb              0.010457           59267          49.075          8.3037
v  FourierNb              0.023985      2.3655e+05          22.001         0.35263
v  total_pressure       4.1624e+05      8.0635e+05      6.9073e+05      6.6106e+05
v  Local Time Step           0.001        0.014988        0.001001       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.93966      2.4511e+05          71.075          8.6563


 TIME FOR THE TIME STEP              675:        0.71605E+02

===============================================================


 INSTANT    0.676000000E+01   TIME STEP NUMBER             676
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.315395461E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312972809E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12594E+03 0.10568E+02
   Friction velocity        uet   :  0.33989E-01 0.21521E+02
   Friction velocity        uk    :  0.50785E-01 0.21521E+02
   Dimensionless distance   yplus :  0.27460E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15090
   Nb of faces within the viscous sub-layer     :       9536
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15937E+02      57   0.10442E+00   0.49785E+02 0.29094E+02 
c  Velocity[X]                                      0.71828E+01 
c  Velocity[Y]                                      0.17328E+02 
c  Velocity[Z]                                      0.25275E+02 
c  Pressure     0.10037E+00     284   0.25318E-01   0.76094E-01 0.59414E+00 
c  k            0.82602E+00      22   0.17230E-03   0.41529E-01 0.28378E+02 
c  epsilon      0.75650E+04      16   0.37857E-03   0.11472E+08 0.83061E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.0378e-05                             1
a  epsilon        
a  Local Time Step      1.6796e-08                        281410


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.4688          17.477          2.1209         0.34795
v  Velocity[Y]             -34.074          39.374          1.2385         0.84621
v  Velocity[Z]             -53.721          34.392         -1.0319      -0.0068959
v  ǁVelocityǁ             0.026163          57.152          7.2567           7.293
v  Pressure                 -82791      3.0639e+05      1.9073e+05      1.6106e+05
v  k                    2.1386e-06          13.109         0.10715         0.11812
v  epsilon                0.033105      3.1972e+06            4166          79.235
v  TurbVisc              3.919e-12         0.49488       0.0042639        0.049862
v  CourantNb              0.018854           59537          49.055          8.3044
v  FourierNb              0.023998      2.3655e+05          22.003         0.35271
v  total_pressure       4.1721e+05      8.0639e+05      6.9073e+05      6.6106e+05
v  Local Time Step           0.001        0.013704       0.0010009       0.0010064


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88682      2.4402e+05          71.058          8.6571


 TIME FOR THE TIME STEP              676:        0.65549E+02

===============================================================


 INSTANT    0.677000000E+01   TIME STEP NUMBER             677
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.809450465E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312987464E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87138E+02 0.99929E+01
   Friction velocity        uet   :  0.27953E-01 0.19833E+02
   Friction velocity        uk    :  0.54859E-01 0.19833E+02
   Dimensionless distance   yplus :  0.25306E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15069
   Nb of faces within the viscous sub-layer     :       9520
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15937E+02      55   0.10387E+00   0.50439E+02 0.29242E+02 
c  Velocity[X]                                      0.80453E+01 
c  Velocity[Y]                                      0.17164E+02 
c  Velocity[Z]                                      0.25229E+02 
c  Pressure     0.10523E+00     378   0.26620E-01   0.79725E-01 0.67791E+00 
c  k            0.82482E+00      24   0.22612E-03   0.39135E-01 0.27468E+02 
c  epsilon      0.75663E+04      13   0.16208E-03   0.37980E+07 0.47762E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.8482e-05                             1
a  epsilon                -0.77439                             2
a  Local Time Step      1.6535e-08                        281409


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.4711          18.051          2.1221         0.34804
v  Velocity[Y]              -38.35          35.941          1.2378         0.84645
v  Velocity[Z]             -64.253          41.631         -1.0308      -0.0074211
v  ǁVelocityǁ             0.011708          69.824          7.2552          7.2938
v  Pressure                 -81471      3.0637e+05      1.9073e+05      1.6105e+05
v  k                      2.49e-06          13.265         0.10743         0.11812
v  epsilon                0.033301      3.1954e+06            4175          79.255
v  TurbVisc             4.0254e-12         0.49488       0.0042768        0.049893
v  CourantNb             0.0063925           60477          49.087          8.3055
v  FourierNb              0.024012      2.3655e+05          22.004         0.35287
v  total_pressure       4.1853e+05      8.0637e+05      6.9073e+05      6.6105e+05
v  Local Time Step           0.001        0.015074       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75683      2.4854e+05          71.091          8.6583


 TIME FOR THE TIME STEP              677:        0.77792E+02

===============================================================


 INSTANT    0.678000000E+01   TIME STEP NUMBER             678
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.586802837E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313002622E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12333E+03 0.11349E+02
   Friction velocity        uet   :  0.28933E-01 0.26081E+02
   Friction velocity        uk    :  0.51956E-01 0.26081E+02
   Dimensionless distance   yplus :  0.17181E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15049
   Nb of faces within the viscous sub-layer     :       9506
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15933E+02      57   0.10191E+00   0.53671E+02 0.30194E+02 
c  Velocity[X]                                      0.76850E+01 
c  Velocity[Y]                                      0.19402E+02 
c  Velocity[Z]                                      0.26583E+02 
c  Pressure     0.10681E+00     340   0.26947E-01   0.80901E-01 0.64058E+00 
c  k            0.82714E+00      23   0.26598E-03   0.53828E-01 0.31424E+02 
c  epsilon      0.76222E+04      15   0.44322E-03   0.68053E+07 0.63297E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.6011e-05                             1
a  epsilon        
a  Local Time Step      1.6824e-08                        281415


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.4228          17.769          2.1213         0.34819
v  Velocity[Y]             -38.695          44.073          1.2382         0.84668
v  Velocity[Z]             -56.161          34.751          -1.031      -0.0073111
v  ǁVelocityǁ             0.022211          59.338          7.2519          7.2948
v  Pressure                 -80667      3.0635e+05      1.9072e+05      1.6104e+05
v  k                    2.2794e-06          13.361         0.10769           0.118
v  epsilon                0.033537      3.2276e+06          4207.7          79.129
v  TurbVisc              4.014e-12         0.49488       0.0042937        0.049917
v  CourantNb              0.021385           59438          49.116          8.3055
v  FourierNb              0.024027      2.3655e+05          22.007         0.35291
v  total_pressure       4.1933e+05      8.0635e+05      6.9072e+05      6.6104e+05
v  Local Time Step           0.001        0.013549       0.0010009       0.0010064


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88607      2.4472e+05          71.123          8.6584


 TIME FOR THE TIME STEP              678:        0.70479E+02

===============================================================


 INSTANT    0.679000000E+01   TIME STEP NUMBER             679
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.950532839E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313007443E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88094E+02 0.11816E+02
   Friction velocity        uet   :  0.38085E-01 0.26995E+02
   Friction velocity        uk    :  0.39224E-01 0.26995E+02
   Dimensionless distance   yplus :  0.21746E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15051
   Nb of faces within the viscous sub-layer     :       9509
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15931E+02      53   0.10279E+00   0.54494E+02 0.30416E+02 
c  Velocity[X]                                      0.80638E+01 
c  Velocity[Y]                                      0.19698E+02 
c  Velocity[Z]                                      0.26732E+02 
c  Pressure     0.10810E+00     383   0.27835E-01   0.81885E-01 0.72618E+00 
c  k            0.83196E+00      22   0.32862E-03   0.51603E-01 0.30338E+02 
c  epsilon      0.76519E+04      14   0.21412E-03   0.54140E+07 0.55928E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.3469e-05                             1
a  epsilon        
a  Local Time Step      1.6887e-08                        281415


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.482          18.181          2.1196         0.34831
v  Velocity[Y]             -36.519          32.454          1.2368         0.84682
v  Velocity[Z]             -64.969          39.807         -1.0337      -0.0069774
v  ǁVelocityǁ            0.0068298          70.601          7.2497          7.2954
v  Pressure                 -80857      3.0626e+05      1.9072e+05      1.6101e+05
v  k                    2.6233e-06          14.784         0.10773         0.11781
v  epsilon                0.033641      3.2099e+06          4195.2          78.969
v  TurbVisc             4.2586e-12         0.49488       0.0043108        0.049926
v  CourantNb              0.092974           59218          49.122          8.3057
v  FourierNb              0.024044      2.3655e+05          22.012         0.35304
v  total_pressure       4.1914e+05      8.0626e+05      6.9072e+05      6.6101e+05
v  Local Time Step           0.001        0.014904       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74571      2.4692e+05          71.134          8.6587


 TIME FOR THE TIME STEP              679:        0.77772E+02

===============================================================


 INSTANT    0.680000000E+01   TIME STEP NUMBER             680
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.317414683E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312981865E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12532E+03 0.12307E+02
   Friction velocity        uet   :  0.93438E-02 0.30489E+02
   Friction velocity        uk    :  0.35837E-01 0.30489E+02
   Dimensionless distance   yplus :  0.21717E-02 0.24169E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15067
   Nb of faces within the viscous sub-layer     :       9487
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15926E+02      53   0.10641E+00   0.52879E+02 0.29986E+02 
c  Velocity[X]                                      0.80220E+01 
c  Velocity[Y]                                      0.19910E+02 
c  Velocity[Z]                                      0.24947E+02 
c  Pressure     0.11097E+00     437   0.28980E-01   0.84162E-01 0.73214E+00 
c  k            0.83727E+00      21   0.13716E-03   0.51512E-01 0.31824E+02 
c  epsilon      0.77081E+04      19   0.24030E-03   0.55210E+07 0.56566E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.6063e-05                             1
a  epsilon        
a  Local Time Step      1.6658e-08                        281438


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.4553           17.87          2.1194         0.34818
v  Velocity[Y]             -36.365          41.205          1.2342         0.84597
v  Velocity[Z]             -58.699           34.57         -1.0352      -0.0061757
v  ǁVelocityǁ             0.012184           62.14          7.2497          7.2963
v  Pressure                 -81088      3.0616e+05      1.9074e+05      1.6098e+05
v  k                    2.5052e-06          15.189         0.10791         0.11755
v  epsilon                0.033631      3.2382e+06          4214.1          78.819
v  TurbVisc             4.0633e-12         0.49488       0.0043257        0.049922
v  CourantNb              0.064214           60030          49.167          8.3055
v  FourierNb              0.024063      2.3655e+05          22.016         0.35295
v  total_pressure       4.1891e+05      8.0616e+05      6.9074e+05      6.6098e+05
v  Local Time Step           0.001        0.016394       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72176      2.4588e+05          71.182          8.6585


 TIME FOR THE TIME STEP              680:        0.82796E+02

===============================================================


 INSTANT    0.681000000E+01   TIME STEP NUMBER             681
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.112527947E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312886857E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10095E+03 0.11916E+02
   Friction velocity        uet   :  0.24179E-01 0.28910E+02
   Friction velocity        uk    :  0.46694E-01 0.28910E+02
   Dimensionless distance   yplus :  0.11123E-02 0.24501E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15062
   Nb of faces within the viscous sub-layer     :       9494
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15924E+02      52   0.10491E+00   0.53322E+02 0.30086E+02 
c  Velocity[X]                                      0.82910E+01 
c  Velocity[Y]                                      0.20370E+02 
c  Velocity[Z]                                      0.24661E+02 
c  Pressure     0.11389E+00     395   0.30083E-01   0.86337E-01 0.85671E+00 
c  k            0.83376E+00      21   0.13616E-03   0.54053E-01 0.32722E+02 
c  epsilon      0.77258E+04      12   0.92994E-03   0.11863E+08 0.83355E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023804                             1
a  epsilon        
a  Local Time Step      1.6704e-08                        281435


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.4758          18.245          2.1207         0.34798
v  Velocity[Y]             -37.632          37.452          1.2301         0.84477
v  Velocity[Z]             -63.646          43.136          -1.037      -0.0050071
v  ǁVelocityǁ             0.020829          69.251          7.2509          7.2972
v  Pressure                 -81384      3.0616e+05      1.9078e+05      1.6095e+05
v  k                     1.788e-06          14.584         0.10794         0.11717
v  epsilon                0.033446      3.2442e+06          4219.6          78.448
v  TurbVisc              4.238e-12         0.49488       0.0043384        0.049905
v  CourantNb             0.0010706           59865          49.179          8.3061
v  FourierNb              0.024083      2.3655e+05          22.018          0.3529
v  total_pressure       4.1862e+05      8.0616e+05      6.9078e+05      6.6095e+05
v  Local Time Step           0.001        0.014956       0.0010009       0.0010064


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62102      2.4701e+05          71.197           8.659


 TIME FOR THE TIME STEP              681:        0.70039E+02

===============================================================


 INSTANT    0.682000000E+01   TIME STEP NUMBER             682
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.930126510E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312755163E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12150E+03 0.10673E+02
   Friction velocity        uet   :  0.22646E-01 0.30605E+02
   Friction velocity        uk    :  0.26487E-01 0.30605E+02
   Dimensionless distance   yplus :  0.26036E-02 0.23993E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15054
   Nb of faces within the viscous sub-layer     :       9506
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15924E+02      57   0.10433E+00   0.55379E+02 0.30674E+02 
c  Velocity[X]                                      0.88509E+01 
c  Velocity[Y]                                      0.20643E+02 
c  Velocity[Z]                                      0.25885E+02 
c  Pressure     0.11638E+00     380   0.31103E-01   0.88121E-01 0.85776E+00 
c  k            0.82330E+00      23   0.53511E-03   0.79390E-01 0.36726E+02 
c  epsilon      0.77140E+04      16   0.55480E-03   0.56259E+07 0.55903E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -9.737e-05                             1
a  epsilon                 -3.0171                             1
a  Local Time Step      1.6901e-08                        281443


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.4346          17.549          2.1192         0.34797
v  Velocity[Y]             -36.694          41.903          1.2252          0.8438
v  Velocity[Z]             -53.412          34.257         -1.0364      -0.0034643
v  ǁVelocityǁ             0.018445          56.577          7.2505          7.2971
v  Pressure                 -81548      3.0625e+05      1.9083e+05      1.6094e+05
v  k                    2.0857e-06           14.11         0.10808         0.11675
v  epsilon                 0.03323      3.2808e+06          4224.3          77.943
v  TurbVisc             3.3717e-12         0.49488        0.004353        0.049872
v  CourantNb               0.13237           59166          49.228          8.3068
v  FourierNb              0.024106      2.3655e+05          22.022         0.35284
v  total_pressure       4.1845e+05      8.0625e+05      6.9083e+05      6.6094e+05
v  Local Time Step           0.001        0.015769       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91715      2.4609e+05           71.25          8.6597


 TIME FOR THE TIME STEP              682:        0.80701E+02

===============================================================


 INSTANT    0.683000000E+01   TIME STEP NUMBER             683
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.125021796E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312582570E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80700E+02 0.10229E+02
   Friction velocity        uet   :  0.35212E-01 0.30432E+02
   Friction velocity        uk    :  0.34933E-01 0.30432E+02
   Dimensionless distance   yplus :  0.23428E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15031
   Nb of faces within the viscous sub-layer     :       9507
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15915E+02      52   0.10612E+00   0.54779E+02 0.30505E+02 
c  Velocity[X]                                      0.89930E+01 
c  Velocity[Y]                                      0.19990E+02 
c  Velocity[Z]                                      0.25795E+02 
c  Pressure     0.11359E+00     680   0.30812E-01   0.86077E-01 0.11174E+01 
c  k            0.81451E+00      24   0.46926E-03   0.72532E-01 0.35194E+02 
c  epsilon      0.76756E+04      14   0.55646E-03   0.92815E+07 0.72692E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002451                             3
a  epsilon                 -3.9032                             1
a  Local Time Step       1.722e-08                        281420


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.495          18.016          2.1177         0.34833
v  Velocity[Y]             -37.734          39.589          1.2248          0.8434
v  Velocity[Z]             -64.337          37.863         -1.0359      -0.0017332
v  ǁVelocityǁ             0.017749          70.029          7.2476          7.2972
v  Pressure                 -81712      3.0644e+05      1.9102e+05      1.6105e+05
v  k                    1.9532e-06          13.429         0.10834         0.11631
v  epsilon                0.033131      3.2609e+06            4241          77.414
v  TurbVisc             3.9843e-12         0.49488       0.0043674         0.04983
v  CourantNb              0.010691           58071          49.237           8.306
v  FourierNb              0.024131      2.3655e+05          22.027         0.35267
v  total_pressure       4.1829e+05      8.0644e+05      6.9102e+05      6.6105e+05
v  Local Time Step           0.001        0.014689       0.0010009       0.0010064


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81561      2.4709e+05          71.264          8.6587


 TIME FOR THE TIME STEP              683:        0.80906E+02

===============================================================


 INSTANT    0.684000000E+01   TIME STEP NUMBER             684
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.314316456E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312404251E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12372E+03 0.98184E+01
   Friction velocity        uet   :  0.40913E-01 0.30445E+02
   Friction velocity        uk    :  0.46863E-01 0.30445E+02
   Dimensionless distance   yplus :  0.31759E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15029
   Nb of faces within the viscous sub-layer     :       9518
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15913E+02      59   0.10370E+00   0.53716E+02 0.30188E+02 
c  Velocity[X]                                      0.83757E+01 
c  Velocity[Y]                                      0.20062E+02 
c  Velocity[Z]                                      0.25278E+02 
c  Pressure     0.11392E+00     957   0.30674E-01   0.86201E-01 0.36537E+01 
c  k            0.80881E+00      24   0.39159E-03   0.84830E-01 0.41555E+02 
c  epsilon      0.76233E+04      13   0.26802E-03   0.10242E+08 0.78087E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00063922                             3
a  epsilon        
a  Local Time Step      1.7665e-08                        281425


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5557          17.434          2.1203         0.34917
v  Velocity[Y]              -38.34           46.34          1.2269          0.8432
v  Velocity[Z]             -53.316          34.224         -1.0358      -0.0014463
v  ǁVelocityǁ             0.017532          56.614          7.2524          7.2987
v  Pressure                 -81014      3.0729e+05      1.9189e+05      1.6174e+05
v  k                    1.7856e-06          13.178         0.10846          0.1159
v  epsilon                0.033105      3.2668e+06          4218.4           76.94
v  TurbVisc             4.2373e-12         0.49488       0.0043841        0.049784
v  CourantNb             0.0016181           56608          49.225          8.3055
v  FourierNb              0.024157      2.3655e+05          22.032         0.35259
v  total_pressure       4.1899e+05      8.0729e+05      6.9189e+05      6.6174e+05
v  Local Time Step           0.001        0.013928       0.0010009       0.0010064


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88355      2.4779e+05          71.258          8.6581


 TIME FOR THE TIME STEP              684:        0.95824E+02

===============================================================


 INSTANT    0.685000000E+01   TIME STEP NUMBER             685
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.700817228E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312400201E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.86868E+02 0.86152E+01
   Friction velocity        uet   :  0.15630E-01 0.27456E+02
   Friction velocity        uk    :  0.37007E-01 0.27456E+02
   Dimensionless distance   yplus :  0.29943E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15036
   Nb of faces within the viscous sub-layer     :       9525
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15921E+02      64   0.10489E+00   0.52898E+02 0.29924E+02 
c  Velocity[X]                                      0.85392E+01 
c  Velocity[Y]                                      0.19198E+02 
c  Velocity[Z]                                      0.25161E+02 
c  Pressure     0.11406E+00     752   0.30258E-01   0.86289E-01 0.52555E+01 
c  k            0.80387E+00      24   0.34897E-03   0.85501E-01 0.42753E+02 
c  epsilon      0.76025E+04      16   0.22100E-03   0.34551E+07 0.45678E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0018194                             3
a  epsilon                 -1.1966                             1
a  Local Time Step      1.7355e-08                        281414


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5111           18.11          2.1215         0.34995
v  Velocity[Y]             -36.274          47.639          1.2293         0.84341
v  Velocity[Z]             -63.488          44.327         -1.0379      -0.0032781
v  ǁVelocityǁ             0.022007          69.086          7.2555          7.3021
v  Pressure                 -80041      3.0865e+05      1.9319e+05      1.6275e+05
v  k                    1.8208e-06           12.72         0.10872         0.11553
v  epsilon                  0.0331      3.2659e+06          4220.7            76.6
v  TurbVisc               3.74e-12         0.49488       0.0043967        0.049734
v  CourantNb              0.028827           57619           49.31          8.3076
v  FourierNb              0.024185      2.3655e+05          22.035         0.35248
v  total_pressure       4.1996e+05      8.0865e+05      6.9319e+05      6.6275e+05
v  Local Time Step           0.001         0.01444       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.4039      2.5156e+05          71.345            8.66


 TIME FOR THE TIME STEP              685:        0.80225E+02

===============================================================


 INSTANT    0.686000000E+01   TIME STEP NUMBER             686
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.254095967E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312569317E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12076E+03 0.70914E+01
   Friction velocity        uet   :  0.29793E-01 0.24029E+02
   Friction velocity        uk    :  0.31631E-01 0.24029E+02
   Dimensionless distance   yplus :  0.17936E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15053
   Nb of faces within the viscous sub-layer     :       9534
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15935E+02      64   0.10621E+00   0.55323E+02 0.30616E+02 
c  Velocity[X]                                      0.91135E+01 
c  Velocity[Y]                                      0.19764E+02 
c  Velocity[Z]                                      0.26445E+02 
c  Pressure     0.11466E+00     354   0.29831E-01   0.86793E-01 0.88156E+00 
c  k            0.80167E+00      23   0.20989E-03   0.53891E-01 0.33961E+02 
c  epsilon      0.76401E+04      15   0.33949E-03   0.14717E+08 0.93488E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00013738                             2
a  epsilon        
a  Local Time Step      1.7457e-08                        281426


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5341          17.396          2.1232         0.35005
v  Velocity[Y]             -33.865          54.202          1.2357         0.84323
v  Velocity[Z]              -54.64          34.357         -1.0384      -0.0044888
v  ǁVelocityǁ            0.0076516          57.941          7.2567          7.3037
v  Pressure                 -80161      3.0872e+05      1.9322e+05      1.6272e+05
v  k                    2.0653e-06          12.883         0.10908         0.11525
v  epsilon                0.033105      3.3192e+06          4260.7          76.376
v  TurbVisc              4.009e-12         0.49488       0.0044065        0.049682
v  CourantNb              0.012394           57285          49.303          8.3105
v  FourierNb              0.024214      2.3655e+05          22.039         0.35241
v  total_pressure       4.1984e+05      8.0872e+05      6.9322e+05      6.6272e+05
v  Local Time Step           0.001        0.014375       0.0010009       0.0010064


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81865      2.5033e+05          71.341          8.6629


 TIME FOR THE TIME STEP              686:        0.69507E+02

===============================================================


 INSTANT    0.687000000E+01   TIME STEP NUMBER             687
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.356344130E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312715814E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93032E+02 0.68561E+01
   Friction velocity        uet   :  0.26654E-01 0.19149E+02
   Friction velocity        uk    :  0.52878E-01 0.19149E+02
   Dimensionless distance   yplus :  0.17418E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15078
   Nb of faces within the viscous sub-layer     :       9544
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15937E+02      60   0.10281E+00   0.56736E+02 0.31016E+02 
c  Velocity[X]                                      0.86230E+01 
c  Velocity[Y]                                      0.21021E+02 
c  Velocity[Z]                                      0.27092E+02 
c  Pressure     0.11797E+00     565   0.30167E-01   0.89418E-01 0.10890E+01 
c  k            0.80166E+00      27   0.18769E-03   0.55646E-01 0.34531E+02 
c  epsilon      0.76849E+04      16   0.67249E-03   0.44053E+08 0.16066E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.0395e-05                             2
a  epsilon                 -5.4316                             1
a  Local Time Step      1.7295e-08                        281429


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.604          18.354          2.1244         0.34974
v  Velocity[Y]             -36.261          38.515          1.2408         0.84306
v  Velocity[Z]             -64.871          38.862          -1.039       -0.005136
v  ǁVelocityǁ             0.015916          70.569          7.2618          7.3049
v  Pressure                 -80438      3.0878e+05      1.9326e+05      1.6269e+05
v  k                    2.3789e-06          13.018         0.10932         0.11503
v  epsilon                0.033081      3.5429e+06          4271.2          76.243
v  TurbVisc             4.3261e-12         0.49488       0.0044107        0.049633
v  CourantNb              0.083067           57822          49.256          8.3123
v  FourierNb              0.024244      2.3655e+05           22.04         0.35224
v  total_pressure       4.1956e+05      8.0878e+05      6.9326e+05      6.6269e+05
v  Local Time Step           0.001        0.014412       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82143      2.4602e+05          71.296          8.6645


 TIME FOR THE TIME STEP              687:        0.86117E+02

===============================================================


 INSTANT    0.688000000E+01   TIME STEP NUMBER             688
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.757320309E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312760482E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12504E+03 0.68721E+01
   Friction velocity        uet   :  0.33100E-01 0.19335E+02
   Friction velocity        uk    :  0.51973E-01 0.19335E+02
   Dimensionless distance   yplus :  0.18489E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15100
   Nb of faces within the viscous sub-layer     :       9535
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15947E+02      57   0.10409E+00   0.51957E+02 0.29668E+02 
c  Velocity[X]                                      0.81975E+01 
c  Velocity[Y]                                      0.18514E+02 
c  Velocity[Z]                                      0.25245E+02 
c  Pressure     0.11066E+00     389   0.28176E-01   0.83696E-01 0.98503E+00 
c  k            0.80188E+00      26   0.20997E-03   0.70873E-01 0.38741E+02 
c  epsilon      0.77614E+04      16   0.35933E-03   0.18608E+08 0.10447E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.4832e-05                             2
a  epsilon        
a  Local Time Step      1.7684e-08                        281415


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5379          17.509          2.1253         0.34941
v  Velocity[Y]             -38.621          35.126          1.2508         0.84307
v  Velocity[Z]             -52.558           33.85         -1.0416      -0.0052066
v  ǁVelocityǁ              0.01718          55.611          7.2703          7.3069
v  Pressure                 -80658      3.0888e+05      1.9329e+05      1.6264e+05
v  k                    2.2105e-06          13.689         0.10975         0.11493
v  epsilon                0.032868      3.3139e+06          4285.9          76.299
v  TurbVisc             4.0988e-12         0.49488       0.0044137        0.049585
v  CourantNb                     0           56549          49.278          8.3148
v  FourierNb              0.024273      2.3655e+05          22.044         0.35219
v  total_pressure       4.1934e+05      8.0888e+05      6.9329e+05      6.6264e+05
v  Local Time Step           0.001        0.014292       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66328      2.4562e+05          71.322           8.667


 TIME FOR THE TIME STEP              688:        0.70812E+02

===============================================================


 INSTANT    0.689000000E+01   TIME STEP NUMBER             689
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.206051076E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312754558E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88922E+02 0.68737E+01
   Friction velocity        uet   :  0.38529E-01 0.19005E+02
   Friction velocity        uk    :  0.53154E-01 0.19005E+02
   Dimensionless distance   yplus :  0.10604E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15117
   Nb of faces within the viscous sub-layer     :       9545
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15953E+02      50   0.10541E+00   0.52828E+02 0.29903E+02 
c  Velocity[X]                                      0.87232E+01 
c  Velocity[Y]                                      0.19209E+02 
c  Velocity[Z]                                      0.24896E+02 
c  Pressure     0.11050E+00     367   0.27637E-01   0.83453E-01 0.91746E+00 
c  k            0.80260E+00      24   0.23738E-03   0.65603E-01 0.37339E+02 
c  epsilon      0.77808E+04      14   0.53821E-03   0.98471E+07 0.75800E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.8701e-05                             1
a  epsilon        
a  Local Time Step      1.7353e-08                        281405


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.583          18.263          2.1252         0.34928
v  Velocity[Y]             -32.803          36.806          1.2579         0.84322
v  Velocity[Z]             -63.897          40.069         -1.0433      -0.0047012
v  ǁVelocityǁ             0.013278          69.506          7.2728          7.3065
v  Pressure                 -80946      3.0905e+05      1.9333e+05       1.626e+05
v  k                    2.4293e-06          13.806         0.11006         0.11496
v  epsilon                0.032437      3.3008e+06          4314.3          76.496
v  TurbVisc             4.1218e-12         0.49488       0.0044168        0.049546
v  CourantNb              0.029063           57627          49.376          8.3179
v  FourierNb                0.0243      2.3655e+05          22.045         0.35203
v  total_pressure       4.1905e+05      8.0905e+05      6.9333e+05       6.626e+05
v  Local Time Step           0.001        0.012635       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45121      2.4945e+05          71.421            8.67


 TIME FOR THE TIME STEP              689:        0.76522E+02

===============================================================


 INSTANT    0.690000000E+01   TIME STEP NUMBER             690
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.665162670E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312650230E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12208E+03 0.68625E+01
   Friction velocity        uet   :  0.35296E-01 0.19252E+02
   Friction velocity        uk    :  0.47746E-01 0.19252E+02
   Dimensionless distance   yplus :  0.11819E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15118
   Nb of faces within the viscous sub-layer     :       9538
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15950E+02      58   0.10526E+00   0.56246E+02 0.30846E+02 
c  Velocity[X]                                      0.85255E+01 
c  Velocity[Y]                                      0.20342E+02 
c  Velocity[Z]                                      0.27379E+02 
c  Pressure     0.11322E+00     325   0.28298E-01   0.85531E-01 0.75702E+00 
c  k            0.80168E+00      24   0.25400E-03   0.50994E-01 0.32804E+02 
c  epsilon      0.78020E+04      16   0.22424E-03   0.66491E+07 0.62176E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.4512e-05                             2
a  epsilon        
a  Local Time Step      1.7433e-08                        281399


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5431           17.72          2.1243         0.34949
v  Velocity[Y]             -32.986          41.118           1.269          0.8432
v  Velocity[Z]              -59.64          34.254         -1.0433        -0.00382
v  ǁVelocityǁ             0.010487          62.892           7.279          7.3062
v  Pressure                 -80937      3.0908e+05      1.9336e+05       1.626e+05
v  k                    2.7249e-06          13.666         0.10997         0.11503
v  epsilon                0.031869      3.3033e+06          4313.6          76.619
v  TurbVisc              4.247e-12         0.49488       0.0044144        0.049517
v  CourantNb              0.032703           57364          49.378          8.3181
v  FourierNb              0.024325      2.3655e+05          22.045         0.35211
v  total_pressure       4.1906e+05      8.0908e+05      6.9336e+05       6.626e+05
v  Local Time Step           0.001        0.013898       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36165      2.4714e+05          71.423          8.6702


 TIME FOR THE TIME STEP              690:        0.70771E+02

===============================================================


 INSTANT    0.691000000E+01   TIME STEP NUMBER             691
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.164693730E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312545821E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10423E+03 0.68330E+01
   Friction velocity        uet   :  0.37664E-01 0.22311E+02
   Friction velocity        uk    :  0.38939E-01 0.22311E+02
   Dimensionless distance   yplus :  0.10705E-02 0.23863E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15133
   Nb of faces within the viscous sub-layer     :       9538
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15951E+02      54   0.10626E+00   0.57431E+02 0.31183E+02 
c  Velocity[X]                                      0.82886E+01 
c  Velocity[Y]                                      0.20724E+02 
c  Velocity[Z]                                      0.28418E+02 
c  Pressure     0.11580E+00     611   0.29334E-01   0.87588E-01 0.32769E+01 
c  k            0.80031E+00      23   0.28018E-03   0.53475E-01 0.33612E+02 
c  epsilon      0.77781E+04      14   0.19697E-03   0.21594E+07 0.35549E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00025973                             2
a  epsilon        
a  Local Time Step      1.7599e-08                        281387


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5368           18.18          2.1229         0.34905
v  Velocity[Y]             -38.159          29.223          1.2809         0.84379
v  Velocity[Z]             -64.596            39.5         -1.0465        -0.00451
v  ǁVelocityǁ            0.0082504          70.236           7.287          7.3076
v  Pressure                 -80369      3.0986e+05      1.9413e+05      1.6323e+05
v  k                     2.026e-06          13.416         0.10989         0.11515
v  epsilon                0.031239      3.2522e+06          4305.3          76.877
v  TurbVisc             4.1999e-12         0.49488       0.0044039        0.049495
v  CourantNb              0.091855           56821          49.433          8.3188
v  FourierNb              0.024346      2.3655e+05          22.041         0.35201
v  total_pressure       4.1963e+05      8.0986e+05      6.9413e+05      6.6323e+05
v  Local Time Step           0.001        0.014643        0.001001       0.0010068


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58536      2.4897e+05          71.475          8.6708


 TIME FOR THE TIME STEP              691:        0.89909E+02

===============================================================


 INSTANT    0.692000000E+01   TIME STEP NUMBER             692
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.230330647E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312648151E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12406E+03 0.69124E+01
   Friction velocity        uet   :  0.27120E-01 0.25568E+02
   Friction velocity        uk    :  0.45842E-01 0.25568E+02
   Dimensionless distance   yplus :  0.27382E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15126
   Nb of faces within the viscous sub-layer     :       9531
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15958E+02      51   0.10658E+00   0.56044E+02 0.30739E+02 
c  Velocity[X]                                      0.84155E+01 
c  Velocity[Y]                                      0.20856E+02 
c  Velocity[Z]                                      0.26772E+02 
c  Pressure     0.11434E+00     329   0.29560E-01   0.86486E-01 0.74657E+00 
c  k            0.79971E+00      26   0.26535E-03   0.58661E-01 0.35167E+02 
c  epsilon      0.77845E+04      12   0.20306E-03   0.29048E+07 0.41098E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00051034                             4
a  epsilon                 -12.733                             3
a  Local Time Step      1.7774e-08                        281390


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5303          17.584          2.1215         0.34902
v  Velocity[Y]             -38.262          39.553          1.2925         0.84435
v  Velocity[Z]             -55.089          34.241         -1.0446      -0.0050067
v  ǁVelocityǁ             0.014023          58.216          7.2928          7.3091
v  Pressure                 -80295       3.099e+05      1.9413e+05      1.6324e+05
v  k                    2.3736e-06          12.844         0.10983         0.11531
v  epsilon                0.030883      3.2583e+06            4315           77.17
v  TurbVisc              3.815e-12         0.49488       0.0043927        0.049479
v  CourantNb                     0           56261          49.453           8.322
v  FourierNb              0.024363      2.3655e+05          22.036         0.35204
v  total_pressure        4.197e+05       8.099e+05      6.9413e+05      6.6324e+05
v  Local Time Step           0.001        0.013141        0.001001       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89297      2.4542e+05          71.489          8.6741


 TIME FOR THE TIME STEP              692:        0.55426E+02

===============================================================


 INSTANT    0.693000000E+01   TIME STEP NUMBER             693
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.581394376E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312701079E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98389E+02 0.84093E+01
   Friction velocity        uet   :  0.36468E-01 0.24002E+02
   Friction velocity        uk    :  0.49685E-01 0.24002E+02
   Dimensionless distance   yplus :  0.28779E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15144
   Nb of faces within the viscous sub-layer     :       9528
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15961E+02      54   0.10564E+00   0.55628E+02 0.30655E+02 
c  Velocity[X]                                      0.87570E+01 
c  Velocity[Y]                                      0.20931E+02 
c  Velocity[Z]                                      0.25940E+02 
c  Pressure     0.11446E+00     368   0.29801E-01   0.86678E-01 0.84560E+00 
c  k            0.80058E+00      23   0.24833E-03   0.48462E-01 0.31456E+02 
c  epsilon      0.77494E+04      13   0.21634E-03   0.29625E+07 0.41585E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003014                             4
a  epsilon                 -6.3259                             3
a  Local Time Step       1.764e-08                        281392


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5822          18.061          2.1223         0.34927
v  Velocity[Y]             -38.051          40.871          1.2988         0.84467
v  Velocity[Z]             -63.178          42.281         -1.0435      -0.0058076
v  ǁVelocityǁ            0.0092512          68.669          7.2977          7.3098
v  Pressure                 -80332      3.0995e+05      1.9411e+05      1.6325e+05
v  k                    1.8678e-06          13.189         0.10961         0.11553
v  epsilon                0.030591      3.2011e+06          4297.8          77.541
v  TurbVisc                  4e-12         0.49488        0.004386        0.049468
v  CourantNb                0.0365           56690          49.468          8.3255
v  FourierNb              0.024373      2.3655e+05          22.031         0.35228
v  total_pressure       4.1967e+05      8.0995e+05      6.9411e+05      6.6325e+05
v  Local Time Step           0.001        0.014455        0.001001       0.0010068


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7516      2.4597e+05            71.5          8.6778


 TIME FOR THE TIME STEP              693:        0.64670E+02

===============================================================


 INSTANT    0.694000000E+01   TIME STEP NUMBER             694
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.629444462E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312794311E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11952E+03 0.10363E+02
   Friction velocity        uet   :  0.38221E-01 0.18839E+02
   Friction velocity        uk    :  0.54862E-01 0.18839E+02
   Dimensionless distance   yplus :  0.50413E-03 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15160
   Nb of faces within the viscous sub-layer     :       9526
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15965E+02      51   0.10376E+00   0.55784E+02 0.30710E+02 
c  Velocity[X]                                      0.88531E+01 
c  Velocity[Y]                                      0.21824E+02 
c  Velocity[Z]                                      0.25106E+02 
c  Pressure     0.11725E+00     375   0.30798E-01   0.88882E-01 0.96346E+00 
c  k            0.80311E+00      22   0.38545E-03   0.84641E-01 0.41711E+02 
c  epsilon      0.77471E+04      13   0.19449E-03   0.19463E+07 0.33640E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001703                             2
a  epsilon        
a  Local Time Step      1.7427e-08                        281394


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5472          17.543          2.1234         0.35007
v  Velocity[Y]             -35.777          35.103          1.3032         0.84486
v  Velocity[Z]             -52.106          33.807         -1.0399      -0.0071102
v  ǁVelocityǁ            0.0047254          55.271          7.3005          7.3118
v  Pressure                 -80128      3.0987e+05      1.9408e+05      1.6329e+05
v  k                    2.7737e-06          13.374         0.10957         0.11576
v  epsilon                0.030476      3.2088e+06          4298.8           77.83
v  TurbVisc             3.8721e-12         0.49488       0.0043848        0.049466
v  CourantNb              0.066973           57383          49.457          8.3274
v  FourierNb              0.024378      2.3655e+05          22.028          0.3525
v  total_pressure       4.1987e+05      8.0987e+05      6.9408e+05      6.6329e+05
v  Local Time Step           0.001        0.014082        0.001001       0.0010069


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85748      2.4602e+05          71.485          8.6799


 TIME FOR THE TIME STEP              694:        0.80407E+02

===============================================================


 INSTANT    0.695000000E+01   TIME STEP NUMBER             695
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.131924470E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312964466E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.89452E+02 0.10878E+02
   Friction velocity        uet   :  0.32044E-01 0.17823E+02
   Friction velocity        uk    :  0.38078E-01 0.17823E+02
   Dimensionless distance   yplus :  0.17066E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15159
   Nb of faces within the viscous sub-layer     :       9523
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15976E+02      52   0.10490E+00   0.55542E+02 0.30615E+02 
c  Velocity[X]                                      0.88944E+01 
c  Velocity[Y]                                      0.21221E+02 
c  Velocity[Z]                                      0.25427E+02 
c  Pressure     0.11842E+00     452   0.31331E-01   0.89844E-01 0.10689E+01 
c  k            0.80844E+00      41   0.46478E-03   0.76912E-01 0.38650E+02 
c  epsilon      0.76984E+04      13   0.23935E-03   0.74085E+07 0.65759E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00029455                             2
a  epsilon        
a  Local Time Step      1.7404e-08                        281382


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.4665          18.374          2.1245         0.35054
v  Velocity[Y]             -38.695          40.665           1.304         0.84507
v  Velocity[Z]             -63.922          39.155         -1.0345      -0.0088098
v  ǁVelocityǁ              0.01266          69.434          7.2991          7.3127
v  Pressure                 -79904      3.0976e+05      1.9401e+05       1.633e+05
v  k                    2.3146e-06          13.993         0.10944         0.11604
v  epsilon                 0.03045      3.1321e+06          4260.3          78.248
v  TurbVisc             4.1973e-12         0.49488       0.0043867        0.049469
v  CourantNb              0.026588           57457          49.438          8.3306
v  FourierNb              0.024375      2.3655e+05          22.025         0.35241
v  total_pressure        4.201e+05      8.0976e+05      6.9401e+05       6.633e+05
v  Local Time Step           0.001           0.013        0.001001       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60038      2.4415e+05          71.463          8.6831


 TIME FOR THE TIME STEP              695:        0.81013E+02

===============================================================


 INSTANT    0.696000000E+01   TIME STEP NUMBER             696
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.240885950E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313164902E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12150E+03 0.11525E+02
   Friction velocity        uet   :  0.41731E-01 0.18176E+02
   Friction velocity        uk    :  0.42783E-01 0.18176E+02
   Dimensionless distance   yplus :  0.23193E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15167
   Nb of faces within the viscous sub-layer     :       9520
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15977E+02      53   0.10421E+00   0.57239E+02 0.31086E+02 
c  Velocity[X]                                      0.84366E+01 
c  Velocity[Y]                                      0.21204E+02 
c  Velocity[Z]                                      0.27598E+02 
c  Pressure     0.12086E+00     851   0.31805E-01   0.91828E-01 0.58950E+01 
c  k            0.81658E+00      26   0.61605E-03   0.11452E+00 0.47299E+02 
c  epsilon      0.76946E+04      13   0.27146E-03   0.88151E+07 0.71803E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012505                             2
a  epsilon               -0.063764                             1
a  Local Time Step      1.7527e-08                        281393


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.4174          17.587          2.1251         0.35068
v  Velocity[Y]             -39.743           43.72          1.3023         0.84528
v  Velocity[Z]              -55.04          34.337         -1.0268      -0.0083985
v  ǁVelocityǁ             0.017463          58.254          7.2957           7.311
v  Pressure                 -80804      3.0826e+05      1.9253e+05      1.6218e+05
v  k                    2.8344e-06          14.467         0.10937         0.11635
v  epsilon                 0.03044      3.1243e+06          4245.6          78.618
v  TurbVisc             3.9387e-12         0.49488       0.0043931         0.04948
v  CourantNb               0.15859           57054          49.387          8.3311
v  FourierNb              0.024368      2.3655e+05          22.024         0.35269
v  total_pressure        4.192e+05      8.0826e+05      6.9253e+05      6.6218e+05
v  Local Time Step           0.001          0.0143        0.001001       0.0010068


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87652      2.4601e+05          71.411          8.6838


 TIME FOR THE TIME STEP              696:        0.10815E+03

===============================================================


 INSTANT    0.697000000E+01   TIME STEP NUMBER             697
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.725694165E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313153045E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85309E+02 0.11013E+02
   Friction velocity        uet   :  0.28710E-01 0.16400E+02
   Friction velocity        uk    :  0.50645E-01 0.16400E+02
   Dimensionless distance   yplus :  0.19858E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15167
   Nb of faces within the viscous sub-layer     :       9513
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15975E+02      66   0.10456E+00   0.56308E+02 0.30811E+02 
c  Velocity[X]                                      0.83683E+01 
c  Velocity[Y]                                      0.21128E+02 
c  Velocity[Z]                                      0.26811E+02 
c  Pressure     0.11635E+00     495   0.30631E-01   0.88510E-01 0.13222E+01 
c  k            0.82751E+00      28   0.46482E-03   0.69176E-01 0.36237E+02 
c  epsilon      0.76451E+04      16   0.30410E-03   0.16152E+08 0.97389E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015123                             2
a  epsilon        
a  Local Time Step      1.7326e-08                        281386


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.3732          18.488          2.1254         0.35058
v  Velocity[Y]             -33.735          34.812          1.2941         0.84583
v  Velocity[Z]             -62.498          41.592         -1.0208      -0.0089352
v  ǁVelocityǁ             0.014572          67.519          7.2886          7.3095
v  Pressure                 -80454      3.0815e+05      1.9244e+05      1.6225e+05
v  k                     2.429e-06          13.892         0.10928         0.11668
v  epsilon                0.030326      3.0793e+06          4221.6          78.988
v  TurbVisc             4.2046e-12         0.49488       0.0044029        0.049499
v  CourantNb              0.062626           57718          49.354          8.3294
v  FourierNb              0.024352      2.3655e+05          22.025         0.35291
v  total_pressure       4.1955e+05      8.0815e+05      6.9244e+05      6.6225e+05
v  Local Time Step           0.001        0.014461        0.001001       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81493      2.4648e+05          71.378          8.6823


 TIME FOR THE TIME STEP              697:        0.95931E+02

===============================================================


 INSTANT    0.698000000E+01   TIME STEP NUMBER             698
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.256689644E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313243312E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11187E+03 0.11015E+02
   Friction velocity        uet   :  0.22880E-01 0.19863E+02
   Friction velocity        uk    :  0.41187E-01 0.19863E+02
   Dimensionless distance   yplus :  0.25345E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15142
   Nb of faces within the viscous sub-layer     :       9535
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15977E+02      54   0.10382E+00   0.51180E+02 0.29431E+02 
c  Velocity[X]                                      0.79553E+01 
c  Velocity[Y]                                      0.18369E+02 
c  Velocity[Z]                                      0.24856E+02 
c  Pressure     0.11009E+00     803   0.29474E-01   0.83796E-01 0.62046E+01 
c  k            0.82943E+00      31   0.15172E-03   0.43626E-01 0.29162E+02 
c  epsilon      0.76504E+04      16   0.32972E-03   0.11095E+08 0.80951E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021515                             2
a  epsilon        
a  Local Time Step      1.6786e-08                        281385


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.3645           17.72          2.1242         0.35012
v  Velocity[Y]             -32.302          34.328          1.2846         0.84611
v  Velocity[Z]             -49.678          34.449         -1.0116      -0.0076851
v  ǁVelocityǁ             0.022036            52.7          7.2771          7.3059
v  Pressure                 -81273      3.0656e+05      1.9091e+05      1.6109e+05
v  k                    1.9858e-06          13.815         0.10906         0.11693
v  epsilon                0.030391      3.0802e+06          4216.7          79.137
v  TurbVisc             4.1493e-12         0.49488       0.0044098        0.049526
v  CourantNb              0.073564           59574          49.299          8.3273
v  FourierNb              0.024331      2.3655e+05          22.024         0.35305
v  total_pressure       4.1873e+05      8.0656e+05      6.9091e+05      6.6109e+05
v  Local Time Step           0.001         0.01573        0.001001       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.80922       2.475e+05          71.323          8.6804


 TIME FOR THE TIME STEP              698:        0.11161E+03

===============================================================


 INSTANT    0.699000000E+01   TIME STEP NUMBER             699
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.722897551E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313130960E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.82182E+02 0.99537E+01
   Friction velocity        uet   :  0.35629E-01 0.18676E+02
   Friction velocity        uk    :  0.36236E-01 0.18676E+02
   Dimensionless distance   yplus :  0.20172E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15150
   Nb of faces within the viscous sub-layer     :       9567
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15967E+02      54   0.10249E+00   0.48639E+02 0.28608E+02 
c  Velocity[X]                                      0.75341E+01 
c  Velocity[Y]                                      0.16563E+02 
c  Velocity[Z]                                      0.24541E+02 
c  Pressure     0.10704E+00     467   0.29124E-01   0.81573E-01 0.14373E+01 
c  k            0.82567E+00      27   0.30820E-03   0.55454E-01 0.32087E+02 
c  epsilon      0.76003E+04      15   0.23690E-03   0.11040E+08 0.81469E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.4652e-05                             2
a  epsilon        
a  Local Time Step      1.6676e-08                        281392


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.3926          18.404           2.123         0.34995
v  Velocity[Y]             -36.542          35.415          1.2722         0.84653
v  Velocity[Z]             -64.939           43.73         -1.0053      -0.0076281
v  ǁVelocityǁ             0.018678          70.534          7.2641          7.3041
v  Pressure                 -80636      3.0646e+05      1.9084e+05      1.6117e+05
v  k                    2.8277e-06          12.843         0.10865         0.11717
v  epsilon                0.030596      3.0535e+06          4178.2           79.15
v  TurbVisc             3.9344e-12         0.49488       0.0044086        0.049554
v  CourantNb             0.0039949           59966           49.18          8.3228
v  FourierNb              0.024304      2.3655e+05          22.023         0.35312
v  total_pressure       4.1936e+05      8.0646e+05      6.9084e+05      6.6117e+05
v  Local Time Step           0.001        0.015983        0.001001       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6976      2.4658e+05          71.203           8.676


 TIME FOR THE TIME STEP              699:        0.79308E+02

===============================================================


 INSTANT    0.700000000E+01   TIME STEP NUMBER             700
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.544891328E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313159862E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12564E+03 0.10197E+02
   Friction velocity        uet   :  0.27341E-01 0.22050E+02
   Friction velocity        uk    :  0.53102E-01 0.22050E+02
   Dimensionless distance   yplus :  0.28135E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15141
   Nb of faces within the viscous sub-layer     :       9551
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15966E+02      60   0.10101E+00   0.52238E+02 0.29726E+02 
c  Velocity[X]                                      0.77631E+01 
c  Velocity[Y]                                      0.17309E+02 
c  Velocity[Z]                                      0.27166E+02 
c  Pressure     0.10970E+00     918   0.29370E-01   0.83611E-01 0.39986E+01 
c  k            0.82273E+00      27   0.23435E-03   0.42993E-01 0.28627E+02 
c  epsilon      0.75740E+04      13   0.27109E-03   0.73025E+07 0.66268E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001563                             2
a  epsilon        
a  Local Time Step       1.688e-08                        281394


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.3728           17.68           2.121         0.34985
v  Velocity[Y]              -38.08            40.7          1.2608         0.84683
v  Velocity[Z]             -52.448          34.481        -0.99842      -0.0067446
v  ǁVelocityǁ            0.0043993          55.581          7.2546          7.3013
v  Pressure                 -81008      3.0543e+05      1.8987e+05      1.6049e+05
v  k                    2.3022e-06          13.229         0.10843         0.11737
v  epsilon                0.030858      3.0364e+06          4187.3          79.118
v  TurbVisc             4.0919e-12         0.49488       0.0043992         0.04959
v  CourantNb                     0           59241          49.025          8.3184
v  FourierNb              0.024274      2.3655e+05           22.02         0.35326
v  total_pressure       4.1899e+05      8.0543e+05      6.8987e+05      6.6049e+05
v  Local Time Step           0.001        0.014293        0.001001       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74544      2.4364e+05          71.045          8.6717


 TIME FOR THE TIME STEP              700:        0.11020E+03

===============================================================


 INSTANT    0.701000000E+01   TIME STEP NUMBER             701
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.260998904E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.313153703E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.79388E+02 0.10525E+02
   Friction velocity        uet   :  0.16148E-01 0.22708E+02
   Friction velocity        uk    :  0.33175E-01 0.22708E+02
   Dimensionless distance   yplus :  0.15018E-02 0.23864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15138
   Nb of faces within the viscous sub-layer     :       9540
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16013E+02      59   0.10269E+00   0.10755E+03 0.41551E+02 
c  Velocity[X]                                      0.95328E+01 
c  Velocity[Y]                                      0.22179E+02 
c  Velocity[Z]                                      0.75836E+02 
c  Pressure     0.10656E+00    1408   0.61634E-01   0.81312E-01 0.20345E+03 
c  k            0.87009E+00      25   0.33252E-03   0.91177E-01 0.40930E+02 
c  epsilon      0.75168E+04      14   0.20532E-03   0.36095E+07 0.46993E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.4413e-05                             1
a  epsilon                 -4.8459                             2
a  Local Time Step      1.6622e-08                        281375


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.3567          19.365          2.1603         0.36265
v  Velocity[Y]             -38.641          37.113          1.2974         0.87587
v  Velocity[Z]             -63.273           39.83         -1.0036      -0.0035063
v  ǁVelocityǁ             0.015782          68.582           7.326          7.5012
v  Pressure                 -37482      3.8444e+05      2.3782e+05      2.0783e+05
v  k                    1.3745e-06          13.384         0.10805         0.11918
v  epsilon                0.031101      3.0206e+06          4155.6          79.578
v  TurbVisc             4.0756e-12         0.49488       0.0043845        0.049626
v  CourantNb              0.017783           60160          48.952          8.3155
v  FourierNb              0.024241      2.3655e+05          22.019         0.35334
v  total_pressure       4.6252e+05      8.8444e+05      7.3782e+05      7.0783e+05
v  Local Time Step           0.001        0.014141        0.001001       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6038      2.4762e+05           70.97          8.6689


 TIME FOR THE TIME STEP              701:        0.13444E+03

===============================================================


 INSTANT    0.702000000E+01   TIME STEP NUMBER             702
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.368384697E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328215391E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10473E+03 0.11568E+02
   Friction velocity        uet   :  0.17612E-01 0.19824E+02
   Friction velocity        uk    :  0.31188E-01 0.19824E+02
   Dimensionless distance   yplus :  0.22043E-02 0.24058E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15280
   Nb of faces within the viscous sub-layer     :       9539
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17002E+02      81   0.99353E-01   0.78051E+02 0.34939E+02 
c  Velocity[X]                                      0.10435E+02 
c  Velocity[Y]                                      0.23660E+02 
c  Velocity[Z]                                      0.43956E+02 
c  Pressure     0.13356E+00    1321   0.35694E-01   0.10116E+00 0.65069E+02 
c  k            0.88631E+00      25   0.23896E-03   0.76303E-01 0.36733E+02 
c  epsilon      0.77680E+04      16   0.48841E-03   0.16064E+08 0.96474E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00010471                             2
a  epsilon        
a  Local Time Step      1.6949e-08                        281403


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.3576          17.503          2.1771         0.36829
v  Velocity[Y]             -35.137          45.893          1.3197         0.89172
v  Velocity[Z]             -60.186          34.915        -0.99177      0.00089947
v  ǁVelocityǁ              0.01221          63.788          7.3652          7.6108
v  Pressure                 -54407      3.5471e+05      2.2511e+05      1.9341e+05
v  k                    2.4149e-06          13.607         0.10879         0.12085
v  epsilon                0.031393      3.0918e+06          4288.1          80.935
v  TurbVisc             1.6194e-12         0.51171       0.0043876        0.050207
v  CourantNb              0.021898           59001          49.499          8.5598
v  FourierNb              0.024206      2.3655e+05          22.011         0.35413
v  total_pressure       4.4559e+05      8.5471e+05      7.2511e+05      6.9341e+05
v  Local Time Step           0.001        0.015555       0.0010009       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74529      2.4343e+05          71.511           8.914


 TIME FOR THE TIME STEP              702:        0.13175E+03

===============================================================


 INSTANT    0.703000000E+01   TIME STEP NUMBER             703
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.204360857E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328444555E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10466E+03 0.10758E+02
   Friction velocity        uet   :  0.17888E-01 0.30880E+02
   Friction velocity        uk    :  0.36599E-01 0.30880E+02
   Dimensionless distance   yplus :  0.16532E-02 0.24336E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15319
   Nb of faces within the viscous sub-layer     :       9535
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17070E+02      73   0.10033E+00   0.61447E+02 0.30922E+02 
c  Velocity[X]                                      0.96996E+01 
c  Velocity[Y]                                      0.22884E+02 
c  Velocity[Z]                                      0.28864E+02 
c  Pressure     0.11796E+00    1505   0.44803E-01   0.88838E-01 0.10094E+03 
c  k            0.89573E+00      23   0.26744E-03   0.82483E-01 0.37740E+02 
c  epsilon      0.77488E+04      16   0.32663E-03   0.15775E+08 0.96641E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001135                             7
a  epsilon                 -33.368                             5
a  Local Time Step      1.5763e-08                        281405


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.3381          19.139          2.1841          0.3683
v  Velocity[Y]              -36.07          40.187          1.3167         0.89332
v  Velocity[Z]             -65.156          43.309         -1.0001      -0.0028803
v  ǁVelocityǁ              0.02338          71.344          7.3926          7.6255
v  Pressure                 -80226       3.272e+05      2.0545e+05      1.7288e+05
v  k                    2.6171e-06          13.265         0.10838         0.12209
v  epsilon                0.031488      3.0843e+06          4240.4           81.32
v  TurbVisc             3.8637e-12         0.51468       0.0043718        0.050531
v  CourantNb              0.017944           63439          49.599          8.5804
v  FourierNb              0.024171      2.3655e+05          22.005         0.35433
v  total_pressure       4.1977e+05       8.272e+05      7.0545e+05      6.7288e+05
v  Local Time Step           0.001        0.015339       0.0010008       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66453      2.4543e+05          71.604          8.9347


 TIME FOR THE TIME STEP              703:        0.14070E+03

===============================================================


 INSTANT    0.704000000E+01   TIME STEP NUMBER             704
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.104099431E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328378359E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12674E+03 0.99989E+01
   Friction velocity        uet   :  0.32363E-01 0.29173E+02
   Friction velocity        uk    :  0.43980E-01 0.29173E+02
   Dimensionless distance   yplus :  0.18221E-02 0.24580E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15347
   Nb of faces within the viscous sub-layer     :       9470
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16856E+02      65   0.10459E+00   0.66165E+02 0.32150E+02 
c  Velocity[X]                                      0.98350E+01 
c  Velocity[Y]                                      0.24457E+02 
c  Velocity[Z]                                      0.31873E+02 
c  Pressure     0.12728E+00    1732   0.38678E-01   0.95251E-01 0.36176E+02 
c  k            0.89579E+00      32   0.33671E-03   0.10445E+00 0.42014E+02 
c  epsilon      0.77727E+04      15   0.27512E-03   0.81789E+07 0.69137E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.4872e-05                             2
a  epsilon               -0.057531                             2
a  Local Time Step      1.5819e-08                        281404


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.4471          17.722          2.1845         0.36757
v  Velocity[Y]             -40.079          42.595          1.3043         0.89043
v  Velocity[Z]             -61.283          34.807         -1.0204      -0.0082464
v  ǁVelocityǁ             0.026082          64.756          7.4161          7.6081
v  Pressure                 -92547      3.2011e+05      1.9826e+05      1.6576e+05
v  k                    2.2835e-07          13.413          0.1087         0.12301
v  epsilon                 0.01316      3.1128e+06            4281          81.654
v  TurbVisc             4.1532e-12         0.51504       0.0043564        0.050776
v  CourantNb             0.0045392           63216          49.734          8.5937
v  FourierNb              0.024138      2.3655e+05          22.001         0.35443
v  total_pressure       4.0745e+05      8.2011e+05      6.9826e+05      6.6576e+05
v  Local Time Step           0.001        0.016873       0.0010008       0.0010059


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67065      2.4796e+05          71.735          8.9481


 TIME FOR THE TIME STEP              704:        0.14085E+03

===============================================================


 INSTANT    0.705000000E+01   TIME STEP NUMBER             705
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.932903263E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328545788E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10223E+03 0.88245E+01
   Friction velocity        uet   :  0.38245E-01 0.30624E+02
   Friction velocity        uk    :  0.38084E-01 0.30624E+02
   Dimensionless distance   yplus :  0.27220E-02 0.24737E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15380
   Nb of faces within the viscous sub-layer     :       9441
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16723E+02      68   0.10360E+00   0.67272E+02 0.32477E+02 
c  Velocity[X]                                      0.98027E+01 
c  Velocity[Y]                                      0.24579E+02 
c  Velocity[Z]                                      0.32891E+02 
c  Pressure     0.12312E+00     620   0.33730E-01   0.91530E-01 0.43157E+01 
c  k            0.89594E+00      24   0.33415E-03   0.10386E+00 0.41843E+02 
c  epsilon      0.77950E+04      14   0.42252E-03   0.16093E+08 0.96257E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013145                             3
a  epsilon                 -22.562                             3
a  Local Time Step      1.5647e-08                        281414


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5564          18.957          2.1817         0.36691
v  Velocity[Y]             -37.524          36.581          1.2945         0.88801
v  Velocity[Z]             -66.248          44.823         -1.0372      -0.0079513
v  ǁVelocityǁ             0.020763          73.075          7.4311          7.5943
v  Pressure                 -97153      3.2026e+05      1.9818e+05      1.6625e+05
v  k                    2.2579e-06          13.462         0.10918         0.12373
v  epsilon                0.032047       3.146e+06          4329.8          81.912
v  TurbVisc             3.9335e-12         0.51509       0.0043452        0.050997
v  CourantNb              0.064146           63911          49.973          8.6052
v  FourierNb              0.024109      2.3655e+05          21.998         0.35459
v  total_pressure       4.0285e+05      8.2026e+05      6.9818e+05      6.6625e+05
v  Local Time Step           0.001        0.017524       0.0010008       0.0010059


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66364      2.4946e+05          71.971          8.9598


 TIME FOR THE TIME STEP              705:        0.82806E+02

===============================================================


 INSTANT    0.706000000E+01   TIME STEP NUMBER             706
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.254138246E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328101190E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12513E+03 0.94260E+01
   Friction velocity        uet   :  0.29304E-01 0.30959E+02
   Friction velocity        uk    :  0.34860E-01 0.30959E+02
   Dimensionless distance   yplus :  0.39503E-02 0.24821E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15357
   Nb of faces within the viscous sub-layer     :       9401
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16692E+02      62   0.10517E+00   0.64353E+02 0.31708E+02 
c  Velocity[X]                                      0.95539E+01 
c  Velocity[Y]                                      0.24274E+02 
c  Velocity[Z]                                      0.30525E+02 
c  Pressure     0.11948E+00    1340   0.33015E-01   0.88291E-01 0.19214E+02 
c  k            0.89727E+00      25   0.33256E-03   0.99896E-01 0.41015E+02 
c  epsilon      0.78752E+04      15   0.97682E-03   0.33332E+08 0.13704E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00042746                             3
a  epsilon                 -9.9435                             3
a  Local Time Step      1.6005e-08                        281407


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.445          17.802          2.1833         0.36699
v  Velocity[Y]             -34.926          48.305          1.2955         0.88767
v  Velocity[Z]             -58.237          35.391         -1.0506      -0.0071931
v  ǁVelocityǁ             0.025075          61.583          7.4534          7.5947
v  Pressure                 -96381       3.246e+05      2.0191e+05      1.7007e+05
v  k                    2.1812e-06          13.995         0.10957         0.12432
v  epsilon                 0.02765      3.2183e+06          4381.5          82.109
v  TurbVisc             3.7518e-12         0.51509       0.0043429        0.051208
v  CourantNb             0.0091147           62481          50.104          8.6095
v  FourierNb              0.024086      2.3655e+05              22         0.35483
v  total_pressure       4.0362e+05       8.246e+05      7.0191e+05      6.7007e+05
v  Local Time Step           0.001        0.017012       0.0010008       0.0010059


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65098       2.476e+05          72.104          8.9643


 TIME FOR THE TIME STEP              706:        0.11515E+03

===============================================================


 INSTANT    0.707000000E+01   TIME STEP NUMBER             707
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.642873539E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328170312E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10828E+03 0.10088E+02
   Friction velocity        uet   :  0.13927E-01 0.31894E+02
   Friction velocity        uk    :  0.32297E-01 0.31894E+02
   Dimensionless distance   yplus :  0.33931E-02 0.24860E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15389
   Nb of faces within the viscous sub-layer     :       9403
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16722E+02      61   0.10577E+00   0.65712E+02 0.32072E+02 
c  Velocity[X]                                      0.98151E+01 
c  Velocity[Y]                                      0.24760E+02 
c  Velocity[Z]                                      0.31137E+02 
c  Pressure     0.12005E+00    1032   0.32764E-01   0.88246E-01 0.85236E+01 
c  k            0.89868E+00      24   0.33873E-03   0.10492E+00 0.42050E+02 
c  epsilon      0.79553E+04      14   0.45533E-03   0.24447E+08 0.11670E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011048                             2
a  epsilon        
a  Local Time Step      1.6038e-08                        281403


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.4866          19.264          2.1828         0.36679
v  Velocity[Y]             -37.345          38.049           1.299         0.88841
v  Velocity[Z]             -67.869          42.096         -1.0629      -0.0050667
v  ǁVelocityǁ             0.022653          74.715           7.473          7.5993
v  Pressure                 -94934      3.2677e+05      2.0354e+05      1.7169e+05
v  k                    2.6018e-06          14.419         0.11013         0.12484
v  epsilon                0.033423      3.2527e+06          4411.9          82.469
v  TurbVisc             3.8734e-12          0.5151       0.0043449        0.051407
v  CourantNb              0.011947           62353           50.32            8.62
v  FourierNb               0.02407      2.3655e+05              22         0.35515
v  total_pressure       4.0507e+05      8.2677e+05      7.0354e+05      6.7169e+05
v  Local Time Step           0.001        0.015203       0.0010008       0.0010058


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69374      2.4881e+05           72.32          8.9752


 TIME FOR THE TIME STEP              707:        0.10794E+03

===============================================================


 INSTANT    0.708000000E+01   TIME STEP NUMBER             708
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.755845594E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327810607E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13052E+03 0.10659E+02
   Friction velocity        uet   :  0.18455E-01 0.34276E+02
   Friction velocity        uk    :  0.45161E-01 0.34276E+02
   Dimensionless distance   yplus :  0.36586E-02 0.24876E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15386
   Nb of faces within the viscous sub-layer     :       9384
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16728E+02      60   0.10308E+00   0.64604E+02 0.31741E+02 
c  Velocity[X]                                      0.95059E+01 
c  Velocity[Y]                                      0.24367E+02 
c  Velocity[Z]                                      0.30731E+02 
c  Pressure     0.12201E+00     926   0.33030E-01   0.89286E-01 0.39753E+01 
c  k            0.89835E+00      26   0.32366E-03   0.10569E+00 0.42337E+02 
c  epsilon      0.79831E+04      16   0.50801E-03   0.20636E+08 0.10723E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00025952                             3
a  epsilon                 -4.7042                             2
a  Local Time Step      1.6387e-08                        281422


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5877           18.15          2.1872         0.36664
v  Velocity[Y]             -37.187          47.631          1.3039         0.88926
v  Velocity[Z]             -57.396           35.18         -1.0777      -0.0042554
v  ǁVelocityǁ             0.011919          60.845          7.4955           7.604
v  Pressure                 -90893      3.2812e+05      2.0451e+05      1.7241e+05
v  k                    1.9067e-06          15.216         0.11086          0.1252
v  epsilon                0.034466      3.3087e+06          4424.8          82.675
v  TurbVisc             3.8856e-12          0.5151       0.0043541        0.051591
v  CourantNb              0.049857           61024          50.447          8.6255
v  FourierNb              0.024062      2.3655e+05          22.001         0.35531
v  total_pressure       4.0911e+05      8.2812e+05      7.0451e+05      6.7241e+05
v  Local Time Step           0.001        0.014265       0.0010008       0.0010059


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72168      2.4578e+05          72.448          8.9808


 TIME FOR THE TIME STEP              708:        0.97766E+02

===============================================================


 INSTANT    0.709000000E+01   TIME STEP NUMBER             709
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.516903869E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327880464E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10528E+03 0.98138E+01
   Friction velocity        uet   :  0.16717E-01 0.32633E+02
   Friction velocity        uk    :  0.52103E-01 0.32633E+02
   Dimensionless distance   yplus :  0.41640E-02 0.24883E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15370
   Nb of faces within the viscous sub-layer     :       9362
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16735E+02      60   0.10327E+00   0.65268E+02 0.31926E+02 
c  Velocity[X]                                      0.97785E+01 
c  Velocity[Y]                                      0.24557E+02 
c  Velocity[Z]                                      0.30933E+02 
c  Pressure     0.12447E+00     865   0.33932E-01   0.90854E-01 0.56132E+01 
c  k            0.89845E+00      26   0.25770E-03   0.94359E-01 0.40006E+02 
c  epsilon      0.80914E+04      18   0.45759E-03   0.20794E+08 0.10612E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00097444                             6
a  epsilon                 -4.5934                             3
a  Local Time Step      1.6348e-08                        281433


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6347          19.268          2.1889         0.36655
v  Velocity[Y]             -39.303          37.228          1.3033         0.88999
v  Velocity[Z]              -66.98          44.547         -1.0905      -0.0058075
v  ǁVelocityǁ             0.016196          73.608          7.5127            7.61
v  Pressure                 -84941      3.2994e+05      2.0598e+05      1.7351e+05
v  k                    1.7958e-06          15.319         0.11192         0.12553
v  epsilon                0.035484      3.3629e+06          4509.2          83.053
v  TurbVisc             3.9977e-12          0.5151       0.0043695         0.05175
v  CourantNb               0.09385           61168          50.699          8.6344
v  FourierNb              0.024062      2.3655e+05          22.004         0.35541
v  total_pressure       4.1506e+05      8.2994e+05      7.0598e+05      6.7351e+05
v  Local Time Step           0.001        0.014091       0.0010008       0.0010059


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77893      2.5046e+05          72.704          8.9898


 TIME FOR THE TIME STEP              709:        0.10260E+03

===============================================================


 INSTANT    0.710000000E+01   TIME STEP NUMBER             710
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.156738562E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328105797E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13179E+03 0.95842E+01
   Friction velocity        uet   :  0.18568E-01 0.30103E+02
   Friction velocity        uk    :  0.41733E-01 0.30103E+02
   Dimensionless distance   yplus :  0.38412E-02 0.24886E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15376
   Nb of faces within the viscous sub-layer     :       9355
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16742E+02      61   0.10414E+00   0.67004E+02 0.32344E+02 
c  Velocity[X]                                      0.10236E+02 
c  Velocity[Y]                                      0.24600E+02 
c  Velocity[Z]                                      0.32168E+02 
c  Pressure     0.12723E+00     520   0.34725E-01   0.92322E-01 0.17175E+01 
c  k            0.89679E+00      29   0.26602E-03   0.84597E-01 0.37867E+02 
c  epsilon      0.82590E+04      18   0.11227E-02   0.37608E+08 0.14036E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00035944                             4
a  epsilon                 -5.4225                             2
a  Local Time Step       1.655e-08                        281447


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7727          18.653          2.1907         0.36675
v  Velocity[Y]             -39.652          45.822          1.2966         0.88979
v  Velocity[Z]              -62.63          35.359         -1.1003      -0.0062435
v  ǁVelocityǁ             0.028953          66.266          7.5242          7.6139
v  Pressure                 -84401      3.3019e+05      2.0602e+05      1.7339e+05
v  k                    1.1055e-07          14.749         0.11278         0.12579
v  epsilon                0.036382      4.6864e+06          4565.9          83.392
v  TurbVisc             3.6745e-12          0.5151       0.0043927        0.051889
v  CourantNb              0.098122           60421          50.838          8.6443
v  FourierNb               0.02407      2.3655e+05          22.006         0.35551
v  total_pressure        4.156e+05      8.3019e+05      7.0602e+05      6.7339e+05
v  Local Time Step           0.001        0.012018       0.0010008       0.0010057


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57667       2.475e+05          72.844          8.9998


 TIME FOR THE TIME STEP              710:        0.88859E+02

===============================================================


 INSTANT    0.711000000E+01   TIME STEP NUMBER             711
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.148752731E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328142494E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10618E+03 0.95681E+01
   Friction velocity        uet   :  0.26670E-01 0.33535E+02
   Friction velocity        uk    :  0.43366E-01 0.33535E+02
   Dimensionless distance   yplus :  0.19362E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15379
   Nb of faces within the viscous sub-layer     :       9336
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16740E+02      63   0.10677E+00   0.68923E+02 0.32773E+02 
c  Velocity[X]                                      0.10256E+02 
c  Velocity[Y]                                      0.26413E+02 
c  Velocity[Z]                                      0.32253E+02 
c  Pressure     0.13098E+00     502   0.35380E-01   0.94745E-01 0.14847E+01 
c  k            0.89628E+00      29   0.21357E-03   0.75460E-01 0.35887E+02 
c  epsilon      0.85333E+04      20   0.12594E-02   0.14257E+09 0.26209E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00034353                             4
a  epsilon                 -3.6558                             3
a  Local Time Step      1.6402e-08                        281451


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9145          19.767          2.1912         0.36677
v  Velocity[Y]             -36.083          49.064          1.2891         0.88964
v  Velocity[Z]             -68.685          40.368         -1.1056      -0.0054124
v  ǁVelocityǁ            0.0089965          75.835          7.5285          7.6155
v  Pressure                 -85939      3.3039e+05      2.0606e+05      1.7335e+05
v  k                    2.5096e-06          14.138         0.11409         0.12605
v  epsilon                0.037192        4.34e+06          4770.3          83.831
v  TurbVisc             9.6758e-15         0.51511        0.004416        0.052011
v  CourantNb              0.010578           60969          50.957          8.6515
v  FourierNb              0.024085      2.3655e+05          22.013         0.35561
v  total_pressure       4.1406e+05      8.3039e+05      7.0606e+05      6.7335e+05
v  Local Time Step           0.001        0.012481       0.0010008       0.0010058


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62022      2.4826e+05          72.969          9.0071


 TIME FOR THE TIME STEP              711:        0.72932E+02

===============================================================


 INSTANT    0.712000000E+01   TIME STEP NUMBER             712
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.503899170E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328000879E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13246E+03 0.92394E+01
   Friction velocity        uet   :  0.34563E-01 0.36949E+02
   Friction velocity        uk    :  0.54271E-01 0.36949E+02
   Dimensionless distance   yplus :  0.18703E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15363
   Nb of faces within the viscous sub-layer     :       9336
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16729E+02      60   0.10703E+00   0.68692E+02 0.32568E+02 
c  Velocity[X]                                      0.10206E+02 
c  Velocity[Y]                                      0.27031E+02 
c  Velocity[Z]                                      0.31455E+02 
c  Pressure     0.12973E+00     910   0.35217E-01   0.93408E-01 0.33888E+01 
c  k            0.89519E+00      29   0.20849E-03   0.61279E-01 0.32353E+02 
c  epsilon      0.86877E+04      19   0.57433E-03   0.13183E+09 0.25245E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018199                             2
a  epsilon                 -2.6265                             2
a  Local Time Step      1.7165e-08                        281452


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9587          18.765          2.1897         0.36671
v  Velocity[Y]             -34.525          50.733           1.282         0.88937
v  Velocity[Z]              -59.88          35.326         -1.1093      -0.0048195
v  ǁVelocityǁ            0.0095592          63.466          7.5331          7.6193
v  Pressure                 -86406      3.3121e+05      2.0684e+05      1.7399e+05
v  k                    1.3493e-07          13.437         0.11407         0.12624
v  epsilon                0.037904      4.4518e+06          4692.8          84.101
v  TurbVisc             4.4527e-12         0.51511       0.0044362        0.052119
v  CourantNb              0.013389           58260          51.003          8.6556
v  FourierNb              0.024106      2.3655e+05          22.021         0.35592
v  total_pressure       4.1359e+05      8.3121e+05      7.0684e+05      6.7399e+05
v  Local Time Step           0.001        0.012102       0.0010008       0.0010058


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.51197      2.4614e+05          73.023          9.0116


 TIME FOR THE TIME STEP              712:        0.10323E+03

===============================================================


 INSTANT    0.713000000E+01   TIME STEP NUMBER             713
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.193722871E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328000903E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11391E+03 0.89256E+01
   Friction velocity        uet   :  0.28233E-01 0.33482E+02
   Friction velocity        uk    :  0.53176E-01 0.33482E+02
   Dimensionless distance   yplus :  0.27292E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15389
   Nb of faces within the viscous sub-layer     :       9312
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16735E+02      58   0.10661E+00   0.67984E+02 0.32551E+02 
c  Velocity[X]                                      0.10012E+02 
c  Velocity[Y]                                      0.25989E+02 
c  Velocity[Z]                                      0.31983E+02 
c  Pressure     0.12979E+00     434   0.34959E-01   0.93369E-01 0.11230E+01 
c  k            0.89572E+00      28   0.20698E-03   0.63324E-01 0.32922E+02 
c  epsilon      0.87717E+04      16   0.46883E-03   0.65314E+08 0.17898E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00043197                             3
a  epsilon                 -4.5903                             2
a  Local Time Step      1.6851e-08                        281445


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -9.0048          19.287          2.1895         0.36655
v  Velocity[Y]             -37.132          37.859          1.2748         0.88915
v  Velocity[Z]             -68.288          43.686         -1.1098       -0.003344
v  ǁVelocityǁ             0.013318          75.257          7.5279          7.6204
v  Pressure                 -87318      3.3118e+05      2.0689e+05      1.7397e+05
v  k                    2.4033e-06          13.805         0.11482         0.12636
v  epsilon                0.038481      4.4223e+06          4771.6          84.194
v  TurbVisc             1.3328e-14         0.51511       0.0044416        0.052213
v  CourantNb              0.018717           59344          51.044          8.6604
v  FourierNb              0.024134      2.3655e+05          22.023         0.35602
v  total_pressure       4.1268e+05      8.3118e+05      7.0689e+05      6.7397e+05
v  Local Time Step           0.001         0.01189       0.0010008       0.0010059


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75233      2.5006e+05          73.067          9.0164


 TIME FOR THE TIME STEP              713:        0.82128E+02

===============================================================


 INSTANT    0.714000000E+01   TIME STEP NUMBER             714
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.180469915E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327840518E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13128E+03 0.10184E+02
   Friction velocity        uet   :  0.11987E-01 0.29514E+02
   Friction velocity        uk    :  0.63156E-01 0.29514E+02
   Dimensionless distance   yplus :  0.27816E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15359
   Nb of faces within the viscous sub-layer     :       9316
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16727E+02      57   0.10481E+00   0.66004E+02 0.31952E+02 
c  Velocity[X]                                      0.96902E+01 
c  Velocity[Y]                                      0.25558E+02 
c  Velocity[Z]                                      0.30756E+02 
c  Pressure     0.12965E+00    1261   0.34951E-01   0.92857E-01 0.61092E+01 
c  k            0.89723E+00      28   0.23501E-03   0.77656E-01 0.36540E+02 
c  epsilon      0.88366E+04      16   0.61172E-03   0.22308E+08 0.10392E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021925                             2
a  epsilon                 -3.6261                             2
a  Local Time Step      1.6981e-08                        281452


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9836          18.645          2.1949         0.36701
v  Velocity[Y]             -42.242           51.35          1.2707         0.88927
v  Velocity[Z]             -61.979          34.566         -1.1127      -0.0042662
v  ǁVelocityǁ             0.016013          65.704          7.5318          7.6263
v  Pressure                 -86580      3.3268e+05      2.0842e+05      1.7525e+05
v  k                     2.909e-06          14.067          0.1147         0.12643
v  epsilon                0.039128      4.4536e+06          4794.2          84.297
v  TurbVisc             4.5484e-12         0.51511       0.0044416        0.052295
v  CourantNb              0.058772           58888          50.981          8.6611
v  FourierNb              0.024166      2.3655e+05          22.031         0.35596
v  total_pressure       4.1342e+05      8.3268e+05      7.0842e+05      6.7525e+05
v  Local Time Step           0.001        0.013079       0.0010008       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.8726      2.4736e+05          73.012          9.0171


 TIME FOR THE TIME STEP              714:        0.12591E+03

===============================================================


 INSTANT    0.715000000E+01   TIME STEP NUMBER             715
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.127208638E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328192707E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11997E+03 0.10054E+02
   Friction velocity        uet   :  0.17594E-01 0.24396E+02
   Friction velocity        uk    :  0.49147E-01 0.24396E+02
   Dimensionless distance   yplus :  0.31130E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15376
   Nb of faces within the viscous sub-layer     :       9318
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16747E+02      70   0.10887E+00   0.66042E+02 0.32057E+02 
c  Velocity[X]                                      0.98380E+01 
c  Velocity[Y]                                      0.25487E+02 
c  Velocity[Z]                                      0.30718E+02 
c  Pressure     0.12806E+00     455   0.34175E-01   0.91504E-01 0.11683E+01 
c  k            0.89955E+00      25   0.22151E-03   0.82262E-01 0.37660E+02 
c  epsilon      0.88504E+04      16   0.26308E-03   0.55075E+07 0.51671E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00036318                             3
a  epsilon                 -3.6002                             2
a  Local Time Step      1.6914e-08                        281448


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9794          19.054          2.2007          0.3668
v  Velocity[Y]             -37.635          34.997          1.2748         0.88934
v  Velocity[Z]             -67.676          41.921         -1.1085      -0.0044572
v  ǁVelocityǁ             0.017977          73.625          7.5333          7.6286
v  Pressure                 -87129      3.3266e+05      2.0845e+05      1.7518e+05
v  k                    2.4788e-06          14.486         0.11463         0.12643
v  epsilon                0.039555      4.4422e+06          4791.9          84.336
v  TurbVisc             4.4798e-12         0.51511       0.0044236        0.052365
v  CourantNb              0.012538           59121          51.026          8.6699
v  FourierNb              0.024203      2.3655e+05          22.033         0.35581
v  total_pressure       4.1287e+05      8.3266e+05      7.0845e+05      6.7518e+05
v  Local Time Step           0.001        0.011526       0.0010008       0.0010062


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67426      2.4523e+05          73.059          9.0257


 TIME FOR THE TIME STEP              715:        0.74372E+02

===============================================================


 INSTANT    0.716000000E+01   TIME STEP NUMBER             716
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.215172255E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328035145E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13313E+03 0.10613E+02
   Friction velocity        uet   :  0.30498E-01 0.32472E+02
   Friction velocity        uk    :  0.43559E-01 0.32472E+02
   Dimensionless distance   yplus :  0.31886E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15385
   Nb of faces within the viscous sub-layer     :       9293
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16741E+02      57   0.10863E+00   0.67630E+02 0.32296E+02 
c  Velocity[X]                                      0.95790E+01 
c  Velocity[Y]                                      0.26687E+02 
c  Velocity[Z]                                      0.31364E+02 
c  Pressure     0.13126E+00     361   0.34589E-01   0.93435E-01 0.97814E+00 
c  k            0.90081E+00      26   0.30334E-03   0.10776E+00 0.43300E+02 
c  epsilon      0.88070E+04      15   0.20656E-03   0.53598E+07 0.51090E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021076                             3
a  epsilon                 -3.7107                             2
a  Local Time Step      1.6832e-08                        281462


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9419          18.111          2.2071         0.36657
v  Velocity[Y]             -34.373          51.764          1.2817         0.88898
v  Velocity[Z]             -63.694          34.769         -1.0998      -0.0042572
v  ǁVelocityǁ             0.020886          67.125          7.5367          7.6317
v  Pressure                 -87173      3.3267e+05      2.0845e+05      1.7517e+05
v  k                    2.7836e-06          14.575         0.11418         0.12638
v  epsilon                0.039866      4.3928e+06          4779.4          84.252
v  TurbVisc              4.491e-12         0.51511        0.004398        0.052422
v  CourantNb            0.00066543           59412          51.035          8.6704
v  FourierNb              0.024243      2.3655e+05          22.034         0.35561
v  total_pressure       4.1283e+05      8.3267e+05      7.0845e+05      6.7517e+05
v  Local Time Step           0.001         0.01143       0.0010008        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69494      2.4409e+05          73.069           9.026


 TIME FOR THE TIME STEP              716:        0.75626E+02

===============================================================


 INSTANT    0.717000000E+01   TIME STEP NUMBER             717
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.236263360E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328005447E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12532E+03 0.98401E+01
   Friction velocity        uet   :  0.13221E-01 0.36265E+02
   Friction velocity        uk    :  0.39148E-01 0.36265E+02
   Dimensionless distance   yplus :  0.17347E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15403
   Nb of faces within the viscous sub-layer     :       9257
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16738E+02      60   0.10460E+00   0.66133E+02 0.32064E+02 
c  Velocity[X]                                      0.98055E+01 
c  Velocity[Y]                                      0.24577E+02 
c  Velocity[Z]                                      0.31751E+02 
c  Pressure     0.12800E+00     442   0.33650E-01   0.91024E-01 0.10094E+01 
c  k            0.90298E+00      22   0.26807E-03   0.12059E+00 0.45891E+02 
c  epsilon      0.87848E+04      14   0.19817E-03   0.35075E+07 0.41321E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0017289                             5
a  epsilon                 -4.0847                             2
a  Local Time Step      1.6602e-08                        281447


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9083          18.774          2.2152         0.36629
v  Velocity[Y]             -36.645          44.518          1.2876         0.88817
v  Velocity[Z]             -66.758          44.127         -1.0896      -0.0036133
v  ǁVelocityǁ             0.027417          72.525          7.5401          7.6334
v  Pressure                 -87097      3.3272e+05      2.0846e+05      1.7518e+05
v  k                    1.1599e-06          13.892         0.11364         0.12624
v  epsilon                0.040035      4.4003e+06          4769.3          84.058
v  TurbVisc              4.515e-12         0.51511        0.004367        0.052469
v  CourantNb              0.042112           60233          51.088          8.6747
v  FourierNb              0.024285      2.3655e+05          22.031         0.35543
v  total_pressure        4.129e+05      8.3272e+05      7.0846e+05      6.7518e+05
v  Local Time Step           0.001        0.012573       0.0010008       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69861      2.4751e+05          73.118          9.0302


 TIME FOR THE TIME STEP              717:        0.87748E+02

===============================================================


 INSTANT    0.718000000E+01   TIME STEP NUMBER             718
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.198434355E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327911533E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12995E+03 0.11008E+02
   Friction velocity        uet   :  0.46355E-02 0.35258E+02
   Friction velocity        uk    :  0.32335E-01 0.35258E+02
   Dimensionless distance   yplus :  0.24178E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15415
   Nb of faces within the viscous sub-layer     :       9246
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16742E+02      62   0.10429E+00   0.67834E+02 0.32347E+02 
c  Velocity[X]                                      0.97305E+01 
c  Velocity[Y]                                      0.25454E+02 
c  Velocity[Z]                                      0.32649E+02 
c  Pressure     0.13091E+00     466   0.34031E-01   0.92723E-01 0.99387E+00 
c  k            0.90585E+00      22   0.36612E-03   0.14033E+00 0.49053E+02 
c  epsilon      0.87575E+04      14   0.44071E-03   0.14551E+08 0.84331E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019823                             3
a  epsilon                  -1.906                             2
a  Local Time Step      1.6672e-08                        281453


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.8667           18.85          2.2212         0.36611
v  Velocity[Y]             -39.985          52.787          1.2965          0.8872
v  Velocity[Z]             -64.768          35.637         -1.0782      -0.0026706
v  ǁVelocityǁ             0.017908          68.292          7.5489          7.6361
v  Pressure                 -86941      3.3287e+05      2.0849e+05      1.7524e+05
v  k                    2.2024e-06          14.046         0.11321         0.12609
v  epsilon                 0.04003       4.345e+06          4747.4           83.88
v  TurbVisc             8.0044e-13         0.51511       0.0043415        0.052504
v  CourantNb              0.037597           59980          51.116          8.6773
v  FourierNb              0.024328      2.3655e+05          22.025         0.35544
v  total_pressure       4.1306e+05      8.3287e+05      7.0849e+05      6.7524e+05
v  Local Time Step           0.001         0.01383       0.0010008       0.0010062


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39386      2.4568e+05          73.142          9.0328


 TIME FOR THE TIME STEP              718:        0.81283E+02

===============================================================


 INSTANT    0.719000000E+01   TIME STEP NUMBER             719
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.132776495E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327805203E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12906E+03 0.11095E+02
   Friction velocity        uet   :  0.88285E-02 0.30896E+02
   Friction velocity        uk    :  0.43750E-01 0.30896E+02
   Dimensionless distance   yplus :  0.29833E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15439
   Nb of faces within the viscous sub-layer     :       9240
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16743E+02      60   0.10697E+00   0.70314E+02 0.33039E+02 
c  Velocity[X]                                      0.96195E+01 
c  Velocity[Y]                                      0.26860E+02 
c  Velocity[Z]                                      0.33835E+02 
c  Pressure     0.12670E+00     783   0.32661E-01   0.89713E-01 0.46267E+01 
c  k            0.91011E+00      25   0.20747E-03   0.10226E+00 0.42320E+02 
c  epsilon      0.87517E+04      13   0.19958E-03   0.62205E+07 0.55118E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00033465                             4
a  epsilon                 -4.1063                             2
a  Local Time Step       1.648e-08                        281449


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9419          18.206          2.2288         0.36627
v  Velocity[Y]             -37.187          39.272          1.3028         0.88706
v  Velocity[Z]             -65.527          44.678         -1.0755      -0.0035632
v  ǁVelocityǁ            0.0052025          71.158          7.5582          7.6403
v  Pressure                 -85954      3.3424e+05      2.0962e+05      1.7618e+05
v  k                    1.9186e-06          14.115         0.11309         0.12595
v  epsilon                0.039939      4.3632e+06          4735.3          83.769
v  TurbVisc             4.6161e-12         0.51511       0.0043285        0.052529
v  CourantNb               0.01199           60679          51.181          8.6824
v  FourierNb              0.024371      2.3655e+05          22.021         0.35531
v  total_pressure       4.1405e+05      8.3424e+05      7.0962e+05      6.7618e+05
v  Local Time Step           0.001        0.012615       0.0010008       0.0010062


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64766      2.4699e+05          73.203          9.0377


 TIME FOR THE TIME STEP              719:        0.94549E+02

===============================================================


 INSTANT    0.720000000E+01   TIME STEP NUMBER             720
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.100950813E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327874053E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12574E+03 0.11824E+02
   Friction velocity        uet   :  0.25778E-01 0.29603E+02
   Friction velocity        uk    :  0.45871E-01 0.29603E+02
   Dimensionless distance   yplus :  0.77192E-03 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15464
   Nb of faces within the viscous sub-layer     :       9249
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16755E+02      58   0.10683E+00   0.67350E+02 0.32238E+02 
c  Velocity[X]                                      0.99064E+01 
c  Velocity[Y]                                      0.25434E+02 
c  Velocity[Z]                                      0.32009E+02 
c  Pressure     0.12691E+00     900   0.32777E-01   0.89687E-01 0.27078E+01 
c  k            0.91239E+00      23   0.23710E-03   0.89327E-01 0.39286E+02 
c  epsilon      0.87168E+04      13   0.32863E-03   0.15868E+08 0.88230E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020057                             3
a  epsilon                 -3.1317                             2
a  Local Time Step      1.6342e-08                        281458


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9385          18.214           2.231         0.36692
v  Velocity[Y]             -34.072          48.974          1.3067         0.88704
v  Velocity[Z]             -62.337          34.765          -1.081       -0.004864
v  ǁVelocityǁ             0.023382          65.652          7.5648           7.644
v  Pressure                 -85519      3.3507e+05      2.1024e+05      1.7668e+05
v  k                    2.6359e-06          14.783          0.1133         0.12589
v  epsilon                0.040116      4.4014e+06          4727.1          83.768
v  TurbVisc             4.1944e-12         0.51511       0.0043362        0.052546
v  CourantNb              0.018226           61191           51.17          8.6885
v  FourierNb              0.024414      2.3655e+05          22.023         0.35535
v  total_pressure       4.1448e+05      8.3507e+05      7.1024e+05      6.7668e+05
v  Local Time Step           0.001        0.012837       0.0010008       0.0010063


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58559      2.4445e+05          73.193          9.0438


 TIME FOR THE TIME STEP              720:        0.10193E+03

===============================================================


 INSTANT    0.721000000E+01   TIME STEP NUMBER             721
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.203093212E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328016312E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12105E+03 0.10921E+02
   Friction velocity        uet   :  0.18750E-01 0.24295E+02
   Friction velocity        uk    :  0.53821E-01 0.24295E+02
   Dimensionless distance   yplus :  0.31000E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15506
   Nb of faces within the viscous sub-layer     :       9263
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16768E+02      62   0.10765E+00   0.68577E+02 0.32595E+02 
c  Velocity[X]                                      0.99279E+01 
c  Velocity[Y]                                      0.26172E+02 
c  Velocity[Z]                                      0.32477E+02 
c  Pressure     0.12673E+00     536   0.32927E-01   0.89639E-01 0.12669E+01 
c  k            0.91342E+00      25   0.19018E-03   0.75191E-01 0.35820E+02 
c  epsilon      0.87377E+04      13   0.25057E-03   0.59547E+07 0.53944E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00029705                             6
a  epsilon                 -2.7771                             3
a  Local Time Step      1.6474e-08                        281478


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.8826          18.961          2.2303         0.36729
v  Velocity[Y]             -38.226          33.502          1.3178         0.88692
v  Velocity[Z]              -67.49          39.938         -1.0895      -0.0055216
v  ǁVelocityǁ             0.022136           73.34          7.5818          7.6476
v  Pressure                 -85829      3.3523e+05      2.1025e+05      1.7666e+05
v  k                    5.3227e-07          14.796         0.11347          0.1259
v  epsilon                 0.04068      4.4127e+06          4730.6          83.786
v  TurbVisc             4.3037e-12         0.51511       0.0043543         0.05256
v  CourantNb              0.049709           60702          51.176          8.6927
v  FourierNb              0.024454      2.3655e+05          22.026         0.35552
v  total_pressure       4.1417e+05      8.3523e+05      7.1025e+05      6.7666e+05
v  Local Time Step           0.001        0.012263       0.0010008       0.0010063


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71933      2.4538e+05          73.201          9.0482


 TIME FOR THE TIME STEP              721:        0.85255E+02

===============================================================


 INSTANT    0.722000000E+01   TIME STEP NUMBER             722
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.122176677E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327994389E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13221E+03 0.11400E+02
   Friction velocity        uet   :  0.14037E-01 0.22835E+02
   Friction velocity        uk    :  0.42726E-01 0.22835E+02
   Dimensionless distance   yplus :  0.29137E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15542
   Nb of faces within the viscous sub-layer     :       9262
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16773E+02      60   0.10793E+00   0.70025E+02 0.32891E+02 
c  Velocity[X]                                      0.10128E+02 
c  Velocity[Y]                                      0.27079E+02 
c  Velocity[Z]                                      0.32818E+02 
c  Pressure     0.13215E+00     381   0.34531E-01   0.93439E-01 0.10171E+01 
c  k            0.91647E+00      23   0.19726E-03   0.58061E-01 0.31496E+02 
c  epsilon      0.87446E+04      17   0.25406E-03   0.11728E+08 0.75542E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00056835                             5
a  epsilon                 -289.27                             3
a  Local Time Step      1.6917e-08                        281459


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9271          18.244          2.2303         0.36747
v  Velocity[Y]             -41.043          43.891          1.3299         0.88688
v  Velocity[Z]             -63.211          35.144         -1.0954      -0.0059218
v  ǁVelocityǁ              0.01545          66.889          7.6004          7.6502
v  Pressure                 -86092      3.3533e+05      2.1025e+05      1.7668e+05
v  k                    2.6868e-06          14.656         0.11408         0.12601
v  epsilon                0.041134      4.4602e+06          4741.8          84.039
v  TurbVisc             1.8925e-13         0.51511       0.0043833        0.052572
v  CourantNb            0.00078556           59114          51.255          8.6985
v  FourierNb              0.024491      2.3655e+05          22.025         0.35587
v  total_pressure       4.1391e+05      8.3533e+05      7.1025e+05      6.7668e+05
v  Local Time Step           0.001         0.01349       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6247      2.4083e+05           73.28          9.0544


 TIME FOR THE TIME STEP              722:        0.73800E+02

===============================================================


 INSTANT    0.723000000E+01   TIME STEP NUMBER             723
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.698396364E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328074507E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11474E+03 0.12210E+02
   Friction velocity        uet   :  0.64979E-02 0.26624E+02
   Friction velocity        uk    :  0.64635E-02 0.26624E+02
   Dimensionless distance   yplus :  0.30908E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15539
   Nb of faces within the viscous sub-layer     :       9252
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16777E+02      58   0.10562E+00   0.72952E+02 0.33589E+02 
c  Velocity[X]                                      0.11144E+02 
c  Velocity[Y]                                      0.29471E+02 
c  Velocity[Z]                                      0.32337E+02 
c  Pressure     0.13989E+00     381   0.36565E-01   0.99091E-01 0.11545E+01 
c  k            0.92053E+00      24   0.18141E-03   0.68039E-01 0.34158E+02 
c  epsilon      0.88586E+04      12   0.19956E-03   0.24253E+08 0.10747E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0017337                             5
a  epsilon                 -3.9965                             4
a  Local Time Step      1.6697e-08                        281459


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -9.0003          18.755          2.2314         0.36737
v  Velocity[Y]             -37.505          47.067          1.3397         0.88701
v  Velocity[Z]             -66.852           45.45         -1.0977      -0.0063105
v  ǁVelocityǁ             0.025209          72.727          7.6145          7.6519
v  Pressure                 -86447       3.354e+05      2.1024e+05      1.7669e+05
v  k                    2.8536e-06          14.561         0.11453         0.12619
v  epsilon                0.040992      4.6259e+06            4776          84.362
v  TurbVisc              4.202e-12         0.51511       0.0044265        0.052583
v  CourantNb              0.072324           59893          51.487          8.7024
v  FourierNb              0.024526      2.3655e+05          22.025         0.35606
v  total_pressure       4.1355e+05       8.354e+05      7.1024e+05      6.7669e+05
v  Local Time Step           0.001        0.014839       0.0010009       0.0010066


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63064      2.4514e+05          73.512          9.0585


 TIME FOR THE TIME STEP              723:        0.73617E+02

===============================================================


 INSTANT    0.724000000E+01   TIME STEP NUMBER             724
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.618933692E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328063355E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13076E+03 0.12145E+02
   Friction velocity        uet   :  0.30548E-01 0.30560E+02
   Friction velocity        uk    :  0.47131E-01 0.30560E+02
   Dimensionless distance   yplus :  0.30171E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15562
   Nb of faces within the viscous sub-layer     :       9234
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16781E+02      66   0.10789E+00   0.72372E+02 0.33401E+02 
c  Velocity[X]                                      0.10806E+02 
c  Velocity[Y]                                      0.29181E+02 
c  Velocity[Z]                                      0.32385E+02 
c  Pressure     0.14427E+00     380   0.37980E-01   0.10221E+00 0.11978E+01 
c  k            0.92052E+00      25   0.38153E-03   0.97159E-01 0.39489E+02 
c  epsilon      0.89051E+04      13   0.21409E-03   0.66486E+07 0.55791E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016193                             2
a  epsilon                 -2.1222                             2
a  Local Time Step      1.7296e-08                        281446


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9755          18.196          2.2292         0.36758
v  Velocity[Y]             -33.755           40.93          1.3466         0.88678
v  Velocity[Z]             -64.125          35.522         -1.0948      -0.0066172
v  ǁVelocityǁ             0.013242          67.674          7.6186          7.6539
v  Pressure                 -86417       3.354e+05      2.1022e+05      1.7673e+05
v  k                     1.391e-06          13.816         0.11548          0.1264
v  epsilon                0.040529      4.5498e+06          4805.8          84.702
v  TurbVisc             4.0672e-12         0.51511       0.0044893        0.052595
v  CourantNb              0.020684           57816          51.634          8.7057
v  FourierNb              0.024555      2.3655e+05          22.029         0.35656
v  total_pressure       4.1358e+05       8.354e+05      7.1022e+05      6.7673e+05
v  Local Time Step           0.001        0.014232       0.0010009       0.0010066


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77612      2.4432e+05          73.663          9.0622


 TIME FOR THE TIME STEP              724:        0.83012E+02

===============================================================


 INSTANT    0.725000000E+01   TIME STEP NUMBER             725
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.327874453E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328107312E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11656E+03 0.10881E+02
   Friction velocity        uet   :  0.38884E-01 0.30002E+02
   Friction velocity        uk    :  0.53273E-01 0.30002E+02
   Dimensionless distance   yplus :  0.28235E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15568
   Nb of faces within the viscous sub-layer     :       9236
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16786E+02      55   0.10735E+00   0.74893E+02 0.34004E+02 
c  Velocity[X]                                      0.11335E+02 
c  Velocity[Y]                                      0.30771E+02 
c  Velocity[Z]                                      0.32787E+02 
c  Pressure     0.14613E+00     438   0.38692E-01   0.10367E+00 0.13791E+01 
c  k            0.91582E+00      27   0.56031E-03   0.25452E+00 0.66075E+02 
c  epsilon      0.88590E+04      16   0.26933E-03   0.79491E+07 0.61730E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00024776                             3
a  epsilon                  -4.815                             2
a  Local Time Step      1.7073e-08                        281455


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9572          18.592          2.2297         0.36741
v  Velocity[Y]             -38.484          41.304          1.3486         0.88669
v  Velocity[Z]             -67.336          41.537         -1.0912      -0.0072219
v  ǁVelocityǁ              0.01804          73.217          7.6199          7.6566
v  Pressure                 -86315      3.3533e+05      2.1017e+05      1.7678e+05
v  k                    2.1556e-06            14.3         0.11602         0.12667
v  epsilon                0.040166      4.5107e+06          4797.7          84.934
v  TurbVisc             4.3813e-12         0.51511       0.0045651        0.052607
v  CourantNb             0.0070843           58571          51.675          8.7086
v  FourierNb              0.024581      2.3654e+05          22.037         0.35717
v  total_pressure       4.1368e+05      8.3533e+05      7.1017e+05      6.7678e+05
v  Local Time Step           0.001        0.015656       0.0010009       0.0010066


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77872      2.5017e+05          73.712          9.0658


 TIME FOR THE TIME STEP              725:        0.74485E+02

===============================================================


 INSTANT    0.726000000E+01   TIME STEP NUMBER             726
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.691991135E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328233115E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13212E+03 0.90289E+01
   Friction velocity        uet   :  0.31405E-01 0.23911E+02
   Friction velocity        uk    :  0.56861E-01 0.23911E+02
   Dimensionless distance   yplus :  0.26839E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15573
   Nb of faces within the viscous sub-layer     :       9224
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16794E+02      56   0.10732E+00   0.74498E+02 0.33873E+02 
c  Velocity[X]                                      0.11086E+02 
c  Velocity[Y]                                      0.31498E+02 
c  Velocity[Z]                                      0.31915E+02 
c  Pressure     0.14789E+00     464   0.39532E-01   0.10507E+00 0.13523E+01 
c  k            0.90713E+00      30   0.48825E-03   0.17892E+00 0.55226E+02 
c  epsilon      0.88144E+04      16   0.50971E-03   0.54730E+08 0.16073E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018696                             3
a  epsilon                 -3.0538                             2
a  Local Time Step      1.6901e-08                        281457


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -8.86          18.092          2.2283         0.36729
v  Velocity[Y]             -39.059          38.243          1.3436         0.88649
v  Velocity[Z]             -61.072           35.09         -1.0841      -0.0085417
v  ǁVelocityǁ            0.0033653          64.769          7.6162          7.6591
v  Pressure                 -86113      3.3542e+05      2.1012e+05      1.7678e+05
v  k                    3.0886e-07          14.649         0.11672         0.12696
v  epsilon                0.040434      4.4343e+06          4828.4          85.148
v  TurbVisc             4.1723e-12         0.51511       0.0046364        0.052622
v  CourantNb              0.016496           59170          51.609          8.7116
v  FourierNb              0.024601      2.3655e+05          22.042         0.35767
v  total_pressure       4.1389e+05      8.3542e+05      7.1012e+05      6.7678e+05
v  Local Time Step           0.001        0.017221       0.0010008       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61182      2.4878e+05          73.652          9.0692


 TIME FOR THE TIME STEP              726:        0.73883E+02

===============================================================


 INSTANT    0.727000000E+01   TIME STEP NUMBER             727
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.591294463E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328373985E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11565E+03 0.74187E+01
   Friction velocity        uet   :  0.13257E-01 0.22556E+02
   Friction velocity        uk    :  0.59436E-01 0.22556E+02
   Dimensionless distance   yplus :  0.22556E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15557
   Nb of faces within the viscous sub-layer     :       9243
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16805E+02      57   0.10714E+00   0.76471E+02 0.34321E+02 
c  Velocity[X]                                      0.12260E+02 
c  Velocity[Y]                                      0.33443E+02 
c  Velocity[Z]                                      0.30768E+02 
c  Pressure     0.15148E+00     823   0.40908E-01   0.10773E+00 0.32263E+01 
c  k            0.90450E+00      23   0.38613E-03   0.11974E+00 0.44910E+02 
c  epsilon      0.86754E+04      16   0.25575E-03   0.53969E+08 0.16281E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00026402                             3
a  epsilon                 -2.7977                             2
a  Local Time Step      1.6801e-08                        281452


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.768          18.358          2.2278          0.3672
v  Velocity[Y]             -39.908           33.02          1.3376         0.88656
v  Velocity[Z]             -66.411          44.542         -1.0748      -0.0092123
v  ǁVelocityǁ              0.01044          72.193          7.6095          7.6602
v  Pressure                 -86213      3.3468e+05      2.0929e+05      1.7619e+05
v  k                     2.138e-06          14.972         0.11688          0.1273
v  epsilon                0.039658      4.3508e+06          4758.6          85.321
v  TurbVisc              2.459e-13         0.51511       0.0046998        0.052638
v  CourantNb             0.0097937           59520          51.523          8.7152
v  FourierNb              0.024616      2.3655e+05          22.049         0.35808
v  total_pressure       4.1379e+05      8.3468e+05      7.0929e+05      6.7619e+05
v  Local Time Step           0.001        0.018943       0.0010008       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.36075      2.4856e+05          73.571          9.0733


 TIME FOR THE TIME STEP              727:        0.86230E+02

===============================================================


 INSTANT    0.728000000E+01   TIME STEP NUMBER             728
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.460004836E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328474179E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12927E+03 0.88783E+01
   Friction velocity        uet   :  0.29572E-01 0.20784E+02
   Friction velocity        uk    :  0.46989E-01 0.20784E+02
   Dimensionless distance   yplus :  0.26520E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15571
   Nb of faces within the viscous sub-layer     :       9243
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16807E+02      56   0.10813E+00   0.79908E+02 0.35049E+02 
c  Velocity[X]                                      0.12426E+02 
c  Velocity[Y]                                      0.35158E+02 
c  Velocity[Z]                                      0.32324E+02 
c  Pressure     0.15459E+00     585   0.41458E-01   0.10981E+00 0.14473E+01 
c  k            0.90250E+00      26   0.49247E-03   0.20334E+00 0.58566E+02 
c  epsilon      0.86301E+04      17   0.66477E-03   0.23923E+08 0.10816E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002343                             2
a  epsilon                 -56.181                             3
a  Local Time Step      1.6901e-08                        281461


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7214          18.014          2.2266         0.36767
v  Velocity[Y]             -35.354          36.827           1.333         0.88643
v  Velocity[Z]             -61.737           35.56          -1.065       -0.010817
v  ǁVelocityǁ            0.0085198          65.291          7.6056          7.6622
v  Pressure                 -85440      3.3471e+05      2.0916e+05      1.7621e+05
v  k                    2.2002e-06          15.111         0.11734         0.12768
v  epsilon                0.039049       4.289e+06          4778.7          85.627
v  TurbVisc             4.4225e-12         0.51511       0.0047561        0.052663
v  CourantNb              0.013476           59166          51.405          8.7144
v  FourierNb              0.024623      2.3655e+05          22.054         0.35861
v  total_pressure       4.1456e+05      8.3471e+05      7.0916e+05      6.7621e+05
v  Local Time Step           0.001        0.020838       0.0010008       0.0010066


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56771      2.4821e+05          73.459           9.073


 TIME FOR THE TIME STEP              728:        0.75020E+02

===============================================================


 INSTANT    0.729000000E+01   TIME STEP NUMBER             729
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.276625679E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328676395E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11082E+03 0.98402E+01
   Friction velocity        uet   :  0.50700E-02 0.26330E+02
   Friction velocity        uk    :  0.62011E-01 0.26330E+02
   Dimensionless distance   yplus :  0.15027E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15577
   Nb of faces within the viscous sub-layer     :       9249
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16819E+02      63   0.11044E+00   0.76684E+02 0.34390E+02 
c  Velocity[X]                                      0.12098E+02 
c  Velocity[Y]                                      0.33050E+02 
c  Velocity[Z]                                      0.31536E+02 
c  Pressure     0.15483E+00    1007   0.41898E-01   0.10995E+00 0.98658E+01 
c  k            0.90409E+00      31   0.44532E-03   0.18315E+00 0.55348E+02 
c  epsilon      0.85476E+04      15   0.45123E-03   0.20388E+08 0.10103E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00034194                            11
a  epsilon                 -9.9547                             7
a  Local Time Step      1.6659e-08                        281452


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7306          18.122          2.2246         0.36709
v  Velocity[Y]             -35.661          38.372          1.3211         0.88528
v  Velocity[Z]              -66.15          45.731          -1.052      -0.0077458
v  ǁVelocityǁ             0.021071          71.743          7.5949          7.6586
v  Pressure                 -86865      3.3212e+05      2.0649e+05      1.7415e+05
v  k                    1.9644e-06          14.754         0.11717         0.12817
v  epsilon                0.038645      4.2256e+06          4701.1          86.024
v  TurbVisc             4.1868e-12         0.51511       0.0048087        0.052693
v  CourantNb             0.0031663           60028          51.398          8.7165
v  FourierNb              0.024622      2.3655e+05          22.057         0.35912
v  total_pressure       4.1313e+05      8.3212e+05      7.0649e+05      6.7415e+05
v  Local Time Step           0.001        0.022921       0.0010008       0.0010064


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63168      2.4931e+05          73.455          9.0756


 TIME FOR THE TIME STEP              729:        0.11174E+03

===============================================================


 INSTANT    0.730000000E+01   TIME STEP NUMBER             730
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.979419725E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328205447E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12767E+03 0.11193E+02
   Friction velocity        uet   :  0.27723E-01 0.28289E+02
   Friction velocity        uk    :  0.57573E-01 0.28289E+02
   Dimensionless distance   yplus :  0.36097E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15552
   Nb of faces within the viscous sub-layer     :       9251
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16793E+02      67   0.10768E+00   0.73317E+02 0.33645E+02 
c  Velocity[X]                                      0.11323E+02 
c  Velocity[Y]                                      0.31214E+02 
c  Velocity[Z]                                      0.30780E+02 
c  Pressure     0.15296E+00     447   0.40878E-01   0.10854E+00 0.15454E+01 
c  k            0.90773E+00      28   0.45341E-03   0.20668E+00 0.58693E+02 
c  epsilon      0.84056E+04      15   0.26288E-03   0.33837E+08 0.13167E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002892                             3
a  epsilon                 -4.7321                             2
a  Local Time Step      1.6464e-08                        281441


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6903          18.186           2.225         0.36664
v  Velocity[Y]             -39.553          41.281          1.3152         0.88491
v  Velocity[Z]             -62.731           35.82         -1.0446      -0.0064047
v  ǁVelocityǁ            0.0088888          66.301          7.5931          7.6562
v  Pressure                 -85485      3.3216e+05      2.0646e+05      1.7422e+05
v  k                    2.3069e-06          14.937         0.11721         0.12873
v  epsilon                0.019705      4.1342e+06            4647          86.486
v  TurbVisc             2.6176e-12         0.51511       0.0048579        0.052735
v  CourantNb             0.0084857           60737          51.285          8.7105
v  FourierNb              0.024613      2.3655e+05          22.059         0.35984
v  total_pressure       4.1452e+05      8.3216e+05      7.0646e+05      6.7422e+05
v  Local Time Step           0.001        0.025214       0.0010009       0.0010066


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.48673      2.4819e+05          73.344          9.0703


 TIME FOR THE TIME STEP              730:        0.80361E+02

===============================================================


 INSTANT    0.731000000E+01   TIME STEP NUMBER             731
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.959985539E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328197764E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11278E+03 0.10817E+02
   Friction velocity        uet   :  0.34911E-01 0.22227E+02
   Friction velocity        uk    :  0.34620E-01 0.22227E+02
   Dimensionless distance   yplus :  0.25846E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15550
   Nb of faces within the viscous sub-layer     :       9237
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16802E+02      56   0.10696E+00   0.71137E+02 0.33083E+02 
c  Velocity[X]                                      0.10418E+02 
c  Velocity[Y]                                      0.29353E+02 
c  Velocity[Z]                                      0.31365E+02 
c  Pressure     0.14723E+00     414   0.39396E-01   0.10441E+00 0.15108E+01 
c  k            0.91180E+00      25   0.48569E-03   0.19328E+00 0.56388E+02 
c  epsilon      0.83519E+04      14   0.35830E-03   0.28625E+08 0.12179E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00046197                             4
a  epsilon                 -1.5242                             2
a  Local Time Step      1.6292e-08                        281412


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6534          18.343          2.2269          0.3662
v  Velocity[Y]             -36.805          39.115          1.3118         0.88518
v  Velocity[Z]              -65.71          44.935         -1.0407      -0.0057117
v  ǁVelocityǁ             0.024432          71.214          7.5956          7.6553
v  Pressure                 -84143      3.3219e+05      2.0646e+05      1.7427e+05
v  k                    2.3233e-06          14.916         0.11749         0.12923
v  epsilon                0.038122       4.082e+06          4618.1          86.936
v  TurbVisc             5.2756e-12         0.51511       0.0048975        0.052787
v  CourantNb              0.028782           61378          51.302            8.71
v  FourierNb              0.024596      2.3655e+05          22.052          0.3603
v  total_pressure       4.1586e+05      8.3219e+05      7.0646e+05      6.7427e+05
v  Local Time Step           0.001        0.027735       0.0010009       0.0010066


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63371      2.4889e+05          73.354          9.0703


 TIME FOR THE TIME STEP              731:        0.71349E+02

===============================================================


 INSTANT    0.732000000E+01   TIME STEP NUMBER             732
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.126516567E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328136372E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12641E+03 0.10713E+02
   Friction velocity        uet   :  0.39303E-01 0.24077E+02
   Friction velocity        uk    :  0.59323E-01 0.24077E+02
   Dimensionless distance   yplus :  0.29081E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15544
   Nb of faces within the viscous sub-layer     :       9215
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16802E+02      67   0.10675E+00   0.73052E+02 0.33549E+02 
c  Velocity[X]                                      0.10440E+02 
c  Velocity[Y]                                      0.28291E+02 
c  Velocity[Z]                                      0.34320E+02 
c  Pressure     0.14309E+00     421   0.37544E-01   0.10126E+00 0.14465E+01 
c  k            0.91198E+00      26   0.35123E-03   0.16122E+00 0.51328E+02 
c  epsilon      0.83666E+04      15   0.22185E-03   0.76021E+07 0.62667E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022101                             5
a  epsilon                 -4.6365                             2
a  Local Time Step      1.6162e-08                        281442


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7449           18.16          2.2255         0.36587
v  Velocity[Y]             -34.333          45.916          1.3121         0.88632
v  Velocity[Z]             -56.079          35.481         -1.0411      -0.0056939
v  ǁVelocityǁ              0.02707           59.54          7.5989          7.6529
v  Pressure                 -83071      3.3217e+05      2.0646e+05      1.7432e+05
v  k                    2.3099e-06          14.659         0.11798         0.12958
v  epsilon                0.037938      4.0836e+06            4642           87.17
v  TurbVisc             4.0771e-12         0.51511       0.0049336        0.052842
v  CourantNb             0.0020641           61875          51.301          8.7106
v  FourierNb              0.024571      2.3655e+05          22.047         0.36074
v  total_pressure       4.1693e+05      8.3217e+05      7.0646e+05      6.7432e+05
v  Local Time Step           0.001        0.030508       0.0010009       0.0010066


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62402      2.4583e+05          73.347          9.0713


 TIME FOR THE TIME STEP              732:        0.75660E+02

===============================================================


 INSTANT    0.733000000E+01   TIME STEP NUMBER             733
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.776053686E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328156617E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93916E+02 0.10183E+02
   Friction velocity        uet   :  0.69098E-02 0.28106E+02
   Friction velocity        uk    :  0.63578E-01 0.28106E+02
   Dimensionless distance   yplus :  0.29228E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15539
   Nb of faces within the viscous sub-layer     :       9214
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16815E+02      66   0.10679E+00   0.70547E+02 0.32935E+02 
c  Velocity[X]                                      0.99466E+01 
c  Velocity[Y]                                      0.26615E+02 
c  Velocity[Z]                                      0.33985E+02 
c  Pressure     0.13214E+00     459   0.34458E-01   0.93498E-01 0.12968E+01 
c  k            0.91064E+00      25   0.29896E-03   0.13735E+00 0.47138E+02 
c  epsilon      0.83463E+04      15   0.22829E-03   0.96570E+07 0.70729E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002386                             4
a  epsilon                -0.94652                             2
a  Local Time Step      1.6168e-08                        281453


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5326          18.277          2.2224         0.36593
v  Velocity[Y]             -36.672          40.719          1.3089         0.88743
v  Velocity[Z]             -66.841          42.975         -1.0474      -0.0064896
v  ǁVelocityǁ            0.0060814          72.485          7.6021          7.6526
v  Pressure                 -86255      3.3219e+05      2.0646e+05      1.7433e+05
v  k                      1.68e-06          14.451         0.11798         0.12986
v  epsilon                0.037952      4.1115e+06          4624.2          87.276
v  TurbVisc             4.8104e-12         0.51511       0.0049604        0.052892
v  CourantNb              0.061527           61849          51.433          8.7087
v  FourierNb              0.024539      2.3655e+05          22.044         0.36121
v  total_pressure       4.1375e+05      8.3219e+05      7.0646e+05      6.7433e+05
v  Local Time Step           0.001        0.033559       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56994      2.4967e+05          73.477          9.0699


 TIME FOR THE TIME STEP              733:        0.73556E+02

===============================================================


 INSTANT    0.734000000E+01   TIME STEP NUMBER             734
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.878614404E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328237585E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13091E+03 0.10160E+02
   Friction velocity        uet   :  0.30595E-01 0.27929E+02
   Friction velocity        uk    :  0.49535E-01 0.27929E+02
   Dimensionless distance   yplus :  0.24365E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15536
   Nb of faces within the viscous sub-layer     :       9187
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16812E+02      59   0.10872E+00   0.70592E+02 0.33020E+02 
c  Velocity[X]                                      0.98304E+01 
c  Velocity[Y]                                      0.26648E+02 
c  Velocity[Z]                                      0.34113E+02 
c  Pressure     0.12861E+00     575   0.33486E-01   0.91029E-01 0.12841E+01 
c  k            0.91200E+00      23   0.23465E-03   0.10121E+00 0.40151E+02 
c  epsilon      0.83231E+04      14   0.26810E-03   0.97952E+07 0.71422E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017867                             2
a  epsilon                 -3.4719                             2
a  Local Time Step      1.6176e-08                        281453


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5806          18.031          2.2172          0.3664
v  Velocity[Y]             -38.597          44.308          1.3052         0.88814
v  Velocity[Z]             -56.724          36.018         -1.0565      -0.0074125
v  ǁVelocityǁ             0.013206          60.096          7.6042          7.6521
v  Pressure                 -90801      3.3208e+05      2.0644e+05      1.7429e+05
v  k                    2.9012e-06          13.488         0.11803          0.1301
v  epsilon                0.037979      4.0834e+06          4620.5          87.335
v  TurbVisc             2.5144e-12         0.51511       0.0049811        0.052938
v  CourantNb              0.035827           61819          51.442          8.7103
v  FourierNb                0.0245      2.3655e+05          22.041         0.36168
v  total_pressure        4.092e+05      8.3208e+05      7.0644e+05      6.7429e+05
v  Local Time Step           0.001        0.036915       0.0010009       0.0010067


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5588       2.462e+05          73.484          9.0719


 TIME FOR THE TIME STEP              734:        0.86389E+02

===============================================================


 INSTANT    0.735000000E+01   TIME STEP NUMBER             735
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.820581475E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328325298E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.94983E+02 0.11390E+02
   Friction velocity        uet   :  0.31015E-01 0.26160E+02
   Friction velocity        uk    :  0.58279E-01 0.26160E+02
   Dimensionless distance   yplus :  0.29723E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15520
   Nb of faces within the viscous sub-layer     :       9173
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16814E+02      55   0.10746E+00   0.71477E+02 0.33148E+02 
c  Velocity[X]                                      0.10100E+02 
c  Velocity[Y]                                      0.27637E+02 
c  Velocity[Z]                                      0.33740E+02 
c  Pressure     0.13158E+00     490   0.34400E-01   0.93120E-01 0.12047E+01 
c  k            0.91656E+00      23   0.27849E-03   0.94399E-01 0.38333E+02 
c  epsilon      0.83365E+04      18   0.28453E-03   0.98056E+07 0.71353E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00024066                             4
a  epsilon                 -1.7364                             2
a  Local Time Step      1.6015e-08                        281451


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6275          18.717          2.2142         0.36662
v  Velocity[Y]             -38.591          41.808          1.2963         0.88825
v  Velocity[Z]             -67.291          41.641         -1.0641      -0.0084594
v  ǁVelocityǁ             0.013203          73.145          7.6063          7.6525
v  Pressure                 -93219      3.3193e+05      2.0644e+05      1.7423e+05
v  k                    2.4394e-06          13.484           0.118          0.1304
v  epsilon                0.038014      4.1658e+06          4601.5           87.56
v  TurbVisc             4.4582e-12         0.51511       0.0049879        0.052982
v  CourantNb              0.017159           62442          51.426          8.7112
v  FourierNb              0.024458      2.3655e+05           22.04         0.36171
v  total_pressure       4.0678e+05      8.3193e+05      7.0644e+05      6.7423e+05
v  Local Time Step           0.001        0.027861       0.0010008       0.0010064


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62462      2.4231e+05          73.466          9.0729


 TIME FOR THE TIME STEP              735:        0.81861E+02

===============================================================


 INSTANT    0.736000000E+01   TIME STEP NUMBER             736
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.240083538E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328401063E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13297E+03 0.12033E+02
   Friction velocity        uet   :  0.34964E-01 0.24883E+02
   Friction velocity        uk    :  0.53815E-01 0.24883E+02
   Dimensionless distance   yplus :  0.22156E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15514
   Nb of faces within the viscous sub-layer     :       9152
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16816E+02      60   0.10632E+00   0.73284E+02 0.33625E+02 
c  Velocity[X]                                      0.10893E+02 
c  Velocity[Y]                                      0.29272E+02 
c  Velocity[Z]                                      0.33120E+02 
c  Pressure     0.13575E+00     513   0.35482E-01   0.95940E-01 0.12172E+01 
c  k            0.92119E+00      22   0.25533E-03   0.79736E-01 0.35054E+02 
c  epsilon      0.83870E+04      18   0.32974E-03   0.58302E+07 0.54657E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014298                             6
a  epsilon                 -7.2118                            12
a  Local Time Step      1.6289e-08                        281471


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6387          17.901          2.2098         0.36709
v  Velocity[Y]              -35.02          43.186          1.2891         0.88791
v  Velocity[Z]             -53.522          36.124         -1.0733      -0.0088354
v  ǁVelocityǁ             0.016969          56.798          7.6073          7.6521
v  Pressure                 -92398      3.3178e+05      2.0643e+05      1.7415e+05
v  k                    1.5381e-06          13.691          0.1181         0.13068
v  epsilon                0.030478      4.1693e+06          4616.3           87.84
v  TurbVisc             4.1856e-12         0.51511       0.0049816        0.053031
v  CourantNb              0.013274           61393          51.435          8.7124
v  FourierNb              0.024414      2.3655e+05           22.04         0.36195
v  total_pressure        4.076e+05      8.3178e+05      7.0643e+05      6.7415e+05
v  Local Time Step           0.001        0.028069       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70841      2.4452e+05          73.475          9.0744


 TIME FOR THE TIME STEP              736:        0.83857E+02

===============================================================


 INSTANT    0.737000000E+01   TIME STEP NUMBER             737
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.983532328E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328451689E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93531E+02 0.11547E+02
   Friction velocity        uet   :  0.37973E-01 0.21026E+02
   Friction velocity        uk    :  0.56562E-01 0.21026E+02
   Dimensionless distance   yplus :  0.22449E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15510
   Nb of faces within the viscous sub-layer     :       9154
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16818E+02      58   0.10957E+00   0.72508E+02 0.33447E+02 
c  Velocity[X]                                      0.11277E+02 
c  Velocity[Y]                                      0.28435E+02 
c  Velocity[Z]                                      0.32796E+02 
c  Pressure     0.14244E+00     476   0.37082E-01   0.10067E+00 0.12693E+01 
c  k            0.92129E+00      23   0.20746E-03   0.74593E-01 0.33741E+02 
c  epsilon      0.83871E+04      15   0.23632E-03   0.76669E+07 0.62864E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00026869                             4
a  epsilon                 -3.9173                             3
a  Local Time Step       1.616e-08                        281473


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6681          18.683          2.2081         0.36735
v  Velocity[Y]             -34.551          42.959          1.2859         0.88816
v  Velocity[Z]             -65.772           45.01         -1.0817      -0.0081702
v  ǁVelocityǁ             0.010519           71.66          7.6111          7.6516
v  Pressure                 -88282      3.3186e+05      2.0644e+05      1.7404e+05
v  k                    2.3724e-06          14.073         0.11822         0.13097
v  epsilon                0.020351      4.2107e+06            4612          88.017
v  TurbVisc             4.3643e-12         0.51511       0.0049701        0.053079
v  CourantNb                     0           61880          51.447          8.7124
v  FourierNb               0.02437      2.3655e+05          22.041           0.362
v  total_pressure       4.1172e+05      8.3186e+05      7.0644e+05      6.7404e+05
v  Local Time Step           0.001        0.024252       0.0010009       0.0010064


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.79181      2.4535e+05          73.488          9.0744


 TIME FOR THE TIME STEP              737:        0.86507E+02

===============================================================


 INSTANT    0.738000000E+01   TIME STEP NUMBER             738
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.641874007E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328387071E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12805E+03 0.11206E+02
   Friction velocity        uet   :  0.18924E-01 0.18579E+02
   Friction velocity        uk    :  0.40519E-01 0.18579E+02
   Dimensionless distance   yplus :  0.15312E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15491
   Nb of faces within the viscous sub-layer     :       9139
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16811E+02      66   0.10739E+00   0.73046E+02 0.33546E+02 
c  Velocity[X]                                      0.11576E+02 
c  Velocity[Y]                                      0.28836E+02 
c  Velocity[Z]                                      0.32635E+02 
c  Pressure     0.14182E+00     457   0.37199E-01   0.10023E+00 0.12590E+01 
c  k            0.92439E+00      23   0.25365E-03   0.74676E-01 0.33547E+02 
c  epsilon      0.84575E+04      16   0.19258E-03   0.99210E+07 0.70975E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017309                             3
a  epsilon                 -2.3245                             3
a  Local Time Step       1.655e-08                        281471


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.722          17.779          2.2088         0.36745
v  Velocity[Y]             -40.327          47.892          1.2841         0.88852
v  Velocity[Z]             -60.691          36.151         -1.0917      -0.0070464
v  ǁVelocityǁ            0.0070254          64.375          7.6121          7.6495
v  Pressure                 -84800      3.3195e+05      2.0646e+05      1.7395e+05
v  k                    2.7144e-06          14.199         0.11887          0.1313
v  epsilon                0.039683      4.2562e+06          4663.7          88.313
v  TurbVisc             4.2199e-12         0.51511       0.0049568        0.053129
v  CourantNb                     0           60424          51.499          8.7131
v  FourierNb              0.024328      2.3655e+05          22.046         0.36194
v  total_pressure        4.152e+05      8.3195e+05      7.0646e+05      6.7395e+05
v  Local Time Step           0.001        0.016994       0.0010008       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76059      2.4805e+05          73.545           9.075


 TIME FOR THE TIME STEP              738:        0.78837E+02

===============================================================


 INSTANT    0.739000000E+01   TIME STEP NUMBER             739
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.678887138E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328252707E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10636E+03 0.12218E+02
   Friction velocity        uet   :  0.38359E-01 0.17835E+02
   Friction velocity        uk    :  0.51629E-01 0.17835E+02
   Dimensionless distance   yplus :  0.19548E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15481
   Nb of faces within the viscous sub-layer     :       9154
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16799E+02      61   0.10590E+00   0.72734E+02 0.33525E+02 
c  Velocity[X]                                      0.12099E+02 
c  Velocity[Y]                                      0.28861E+02 
c  Velocity[Z]                                      0.31774E+02 
c  Pressure     0.14291E+00     428   0.38105E-01   0.10114E+00 0.12945E+01 
c  k            0.92905E+00      22   0.23384E-03   0.84606E-01 0.35325E+02 
c  epsilon      0.85304E+04      15   0.20997E-03   0.85004E+07 0.65241E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019655                             9
a  epsilon                 -10.182                            10
a  Local Time Step      1.6719e-08                        281472


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6464          18.822          2.2126         0.36741
v  Velocity[Y]              -39.09          37.909          1.2824          0.8884
v  Velocity[Z]             -66.414           39.38            -1.1      -0.0054013
v  ǁVelocityǁ             0.010633          72.406          7.6162          7.6479
v  Pressure                 -85894      3.3204e+05       2.065e+05       1.739e+05
v  k                    3.5524e-07          14.376         0.11935         0.13164
v  epsilon                0.040276      4.2956e+06          4684.8          88.611
v  TurbVisc             4.4017e-12         0.51511       0.0049486        0.053185
v  CourantNb            0.00098353           59811          51.557          8.7097
v  FourierNb               0.02429      2.3655e+05          22.049         0.36199
v  total_pressure       4.1411e+05      8.3204e+05       7.065e+05       6.739e+05
v  Local Time Step           0.001        0.018061       0.0010008       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.59938       2.454e+05          73.606          9.0717


 TIME FOR THE TIME STEP              739:        0.81081E+02

===============================================================


 INSTANT    0.740000000E+01   TIME STEP NUMBER             740
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.912915929E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328063803E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12994E+03 0.11905E+02
   Friction velocity        uet   :  0.25329E-01 0.17447E+02
   Friction velocity        uk    :  0.53681E-01 0.17447E+02
   Dimensionless distance   yplus :  0.18233E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15492
   Nb of faces within the viscous sub-layer     :       9145
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16800E+02      61   0.11039E+00   0.68172E+02 0.32406E+02 
c  Velocity[X]                                      0.11477E+02 
c  Velocity[Y]                                      0.26662E+02 
c  Velocity[Z]                                      0.30033E+02 
c  Pressure     0.13807E+00     589   0.37945E-01   0.97659E-01 0.12996E+01 
c  k            0.92955E+00      23   0.40127E-03   0.96360E-01 0.37061E+02 
c  epsilon      0.86020E+04      17   0.51328E-03   0.21118E+08 0.10212E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021337                             3
a  epsilon                 -4.0215                             3
a  Local Time Step      1.6602e-08                        281455


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7139          18.708           2.216         0.36707
v  Velocity[Y]             -35.798          51.312          1.2792         0.88771
v  Velocity[Z]             -57.706          35.543         -1.1033      -0.0032828
v  ǁVelocityǁ             0.014206          61.017          7.6146          7.6463
v  Pressure                 -86853      3.3216e+05       2.066e+05      1.7393e+05
v  k                    1.2528e-06          14.642         0.12003         0.13201
v  epsilon               0.0030082      4.3522e+06          4721.8          88.908
v  TurbVisc             4.3306e-12         0.51511       0.0049462        0.053248
v  CourantNb              0.075091           60234          51.637          8.7089
v  FourierNb              0.024257      2.3655e+05          22.051          0.3619
v  total_pressure       4.1315e+05      8.3216e+05       7.066e+05      6.7393e+05
v  Local Time Step           0.001        0.016423       0.0010008        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65288      2.4662e+05          73.687          9.0708


 TIME FOR THE TIME STEP              740:        0.81750E+02

===============================================================


 INSTANT    0.741000000E+01   TIME STEP NUMBER             741
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.106164399E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327823299E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10614E+03 0.11130E+02
   Friction velocity        uet   :  0.22223E-01 0.19770E+02
   Friction velocity        uk    :  0.31567E-01 0.19770E+02
   Dimensionless distance   yplus :  0.20282E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15467
   Nb of faces within the viscous sub-layer     :       9141
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16789E+02      58   0.10936E+00   0.66911E+02 0.32184E+02 
c  Velocity[X]                                      0.11244E+02 
c  Velocity[Y]                                      0.25067E+02 
c  Velocity[Z]                                      0.30599E+02 
c  Pressure     0.13958E+00     587   0.37565E-01   0.98825E-01 0.18061E+01 
c  k            0.92688E+00      23   0.36769E-03   0.15372E+00 0.47673E+02 
c  epsilon      0.86744E+04      14   0.89545E-03   0.35330E+08 0.13109E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021907                             4
a  epsilon                 -5.1732                             5
a  Local Time Step      1.6696e-08                        281465


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7709           19.13          2.2208         0.36676
v  Velocity[Y]             -34.967          41.114          1.2785         0.88761
v  Velocity[Z]             -67.157          42.952         -1.1044      -0.0013473
v  ǁVelocityǁ            0.0081613           73.25          7.6115          7.6441
v  Pressure                 -87356      3.3251e+05      2.0698e+05      1.7421e+05
v  k                    2.3791e-06          14.636         0.12062         0.13237
v  epsilon                0.041407      4.4161e+06            4788          89.074
v  TurbVisc             4.3857e-12         0.51511       0.0049536         0.05332
v  CourantNb              0.012689           59893          51.674          8.7066
v  FourierNb               0.02423      2.3655e+05          22.055         0.36195
v  total_pressure       4.1264e+05      8.3251e+05      7.0698e+05      6.7421e+05
v  Local Time Step           0.001         0.01341       0.0010008        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.77282      2.4772e+05          73.728          9.0685


 TIME FOR THE TIME STEP              741:        0.81853E+02

===============================================================


 INSTANT    0.742000000E+01   TIME STEP NUMBER             742
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.124367021E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327628254E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13230E+03 0.10185E+02
   Friction velocity        uet   :  0.28788E-01 0.18674E+02
   Friction velocity        uk    :  0.40749E-01 0.18674E+02
   Dimensionless distance   yplus :  0.14900E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15502
   Nb of faces within the viscous sub-layer     :       9133
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16781E+02      66   0.10626E+00   0.66889E+02 0.32164E+02 
c  Velocity[X]                                      0.10487E+02 
c  Velocity[Y]                                      0.26200E+02 
c  Velocity[Z]                                      0.30202E+02 
c  Pressure     0.13420E+00     987   0.36408E-01   0.95065E-01 0.11310E+02 
c  k            0.92238E+00      25   0.42625E-03   0.13537E+00 0.44595E+02 
c  epsilon      0.86908E+04      14   0.31139E-03   0.18243E+08 0.94466E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018449                             4
a  epsilon                 -2.9677                             4
a  Local Time Step      1.6858e-08                        281462


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7503          18.796           2.225         0.36699
v  Velocity[Y]             -40.254          46.581          1.2845         0.88835
v  Velocity[Z]             -61.058           34.91         -1.1061      -0.0044998
v  ǁVelocityǁ             0.017814          64.837          7.6147          7.6485
v  Pressure                 -85004      3.3552e+05      2.0995e+05      1.7662e+05
v  k                    2.2046e-06           14.48         0.12103         0.13282
v  epsilon                0.039123      4.4657e+06          4765.7          89.273
v  TurbVisc             4.2634e-12         0.51511       0.0049666        0.053394
v  CourantNb              0.043672           59319          51.666          8.7042
v  FourierNb              0.024211      2.3655e+05          22.058         0.36203
v  total_pressure         4.15e+05      8.3552e+05      7.0995e+05      6.7662e+05
v  Local Time Step           0.001        0.014751       0.0010008       0.0010059


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.67741      2.4599e+05          73.724          9.0663


 TIME FOR THE TIME STEP              742:        0.96671E+02

===============================================================


 INSTANT    0.743000000E+01   TIME STEP NUMBER             743
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.654437555E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328275322E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10779E+03 0.95174E+01
   Friction velocity        uet   :  0.23334E-01 0.21657E+02
   Friction velocity        uk    :  0.50381E-01 0.21657E+02
   Dimensionless distance   yplus :  0.27635E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15499
   Nb of faces within the viscous sub-layer     :       9127
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16804E+02      59   0.10809E+00   0.67195E+02 0.32191E+02 
c  Velocity[X]                                      0.99852E+01 
c  Velocity[Y]                                      0.26160E+02 
c  Velocity[Z]                                      0.31050E+02 
c  Pressure     0.13201E+00     369   0.34966E-01   0.93452E-01 0.12330E+01 
c  k            0.92113E+00      24   0.44107E-03   0.13905E+00 0.44883E+02 
c  epsilon      0.87930E+04      14   0.50156E-03   0.42659E+08 0.14211E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00024942                             4
a  epsilon                 -5.3666                             4
a  Local Time Step      1.6622e-08                        281456


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7597          19.563          2.2267         0.36669
v  Velocity[Y]             -37.818          43.859          1.2898         0.88848
v  Velocity[Z]              -68.78           41.73         -1.1093      -0.0062674
v  ǁVelocityǁ             0.017235          75.869          7.6139          7.6507
v  Pressure                 -85520      3.3555e+05      2.0995e+05      1.7655e+05
v  k                    2.2061e-06          14.406         0.12188         0.13327
v  epsilon                  0.0424      4.6246e+06          4857.6          89.609
v  TurbVisc             4.2699e-12         0.51511        0.004983        0.053477
v  CourantNb              0.065021           60162          51.715          8.7108
v  FourierNb              0.024199      2.3655e+05          22.058         0.36224
v  total_pressure       4.1448e+05      8.3555e+05      7.0995e+05      6.7655e+05
v  Local Time Step           0.001        0.015264       0.0010008       0.0010059


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66316      2.4742e+05          73.773           9.073


 TIME FOR THE TIME STEP              743:        0.66096E+02

===============================================================


 INSTANT    0.744000000E+01   TIME STEP NUMBER             744
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.880902440E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328208250E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13273E+03 0.10246E+02
   Friction velocity        uet   :  0.13332E-01 0.18618E+02
   Friction velocity        uk    :  0.47020E-01 0.18618E+02
   Dimensionless distance   yplus :  0.23140E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15503
   Nb of faces within the viscous sub-layer     :       9143
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16807E+02      59   0.10823E+00   0.66253E+02 0.31964E+02 
c  Velocity[X]                                      0.96401E+01 
c  Velocity[Y]                                      0.25900E+02 
c  Velocity[Z]                                      0.30713E+02 
c  Pressure     0.12927E+00     342   0.33934E-01   0.91458E-01 0.11155E+01 
c  k            0.92083E+00      25   0.35816E-03   0.11465E+00 0.40913E+02 
c  epsilon      0.88517E+04      16   0.51214E-03   0.15468E+08 0.85652E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016074                             8
a  epsilon                 -9.8918                            12
a  Local Time Step      1.6669e-08                        281459


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6903          18.187          2.2283         0.36658
v  Velocity[Y]             -34.959          45.939           1.298          0.8882
v  Velocity[Z]             -56.541          35.132         -1.1129       -0.007289
v  ǁVelocityǁ             0.011522           59.87          7.6159          7.6524
v  Pressure                 -85544      3.3554e+05      2.0993e+05       1.765e+05
v  k                    2.4454e-06          14.047         0.12203         0.13368
v  epsilon                0.033199      4.5688e+06          4837.2          89.773
v  TurbVisc             4.2807e-12         0.51511       0.0050018        0.053563
v  CourantNb              0.029465           59991          51.693          8.7089
v  FourierNb              0.024196      2.3655e+05          22.059         0.36258
v  total_pressure       4.1446e+05      8.3554e+05      7.0993e+05       6.765e+05
v  Local Time Step           0.001        0.016414       0.0010008        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.84599      2.4807e+05          73.751          9.0715


 TIME FOR THE TIME STEP              744:        0.71178E+02

===============================================================


 INSTANT    0.745000000E+01   TIME STEP NUMBER             745
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.517049883E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328308088E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10251E+03 0.98445E+01
   Friction velocity        uet   :  0.10702E-01 0.19107E+02
   Friction velocity        uk    :  0.34245E-01 0.19107E+02
   Dimensionless distance   yplus :  0.15265E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15529
   Nb of faces within the viscous sub-layer     :       9146
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16809E+02      59   0.10868E+00   0.64493E+02 0.31559E+02 
c  Velocity[X]                                      0.92928E+01 
c  Velocity[Y]                                      0.25285E+02 
c  Velocity[Z]                                      0.29915E+02 
c  Pressure     0.13446E+00     338   0.34432E-01   0.94981E-01 0.10478E+01 
c  k            0.92407E+00      26   0.41463E-03   0.14316E+00 0.45626E+02 
c  epsilon      0.88713E+04      17   0.34188E-03   0.12583E+08 0.76895E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00024406                             5
a  epsilon                 -5.5703                             3
a  Local Time Step      1.6273e-08                        281459


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7156          19.075          2.2292         0.36612
v  Velocity[Y]              -35.51          35.035          1.3086         0.88753
v  Velocity[Z]             -68.683          43.215         -1.1161      -0.0074181
v  ǁVelocityǁ             0.017055          74.683          7.6215          7.6536
v  Pressure                 -85683      3.3554e+05      2.0991e+05      1.7645e+05
v  k                    2.3177e-06          14.501         0.12267         0.13409
v  epsilon                 0.03861      4.5629e+06          4874.5          90.184
v  TurbVisc             4.4032e-12         0.51511       0.0050235        0.053648
v  CourantNb                     0           61450          51.683           8.711
v  FourierNb                0.0242      2.3655e+05          22.055         0.36284
v  total_pressure       4.1432e+05      8.3554e+05      7.0991e+05      6.7645e+05
v  Local Time Step           0.001        0.012618       0.0010008       0.0010057


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5999      2.4589e+05          73.737          9.0738


 TIME FOR THE TIME STEP              745:        0.64835E+02

===============================================================


 INSTANT    0.746000000E+01   TIME STEP NUMBER             746
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.103413245E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328334144E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13677E+03 0.11860E+02
   Friction velocity        uet   :  0.15551E-01 0.24776E+02
   Friction velocity        uk    :  0.24861E-01 0.24776E+02
   Dimensionless distance   yplus :  0.93608E-03 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15530
   Nb of faces within the viscous sub-layer     :       9184
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16805E+02      61   0.10972E+00   0.65528E+02 0.31780E+02 
c  Velocity[X]                                      0.94269E+01 
c  Velocity[Y]                                      0.25548E+02 
c  Velocity[Z]                                      0.30553E+02 
c  Pressure     0.12967E+00     292   0.32978E-01   0.91428E-01 0.91358E+00 
c  k            0.93033E+00      27   0.67404E-03   0.21682E+00 0.54387E+02 
c  epsilon      0.88949E+04      18   0.29921E-03   0.19024E+08 0.93815E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014653                             3
a  epsilon                 -1.4857                             2
a  Local Time Step      1.6528e-08                        281440


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7123           18.39          2.2296         0.36584
v  Velocity[Y]             -40.359          51.169          1.3198          0.8869
v  Velocity[Z]             -55.081          34.713         -1.1184      -0.0070076
v  ǁVelocityǁ             0.017393          58.515          7.6301          7.6544
v  Pressure                 -85694      3.3553e+05      2.0989e+05      1.7645e+05
v  k                    1.9676e-06          14.729         0.12287         0.13443
v  epsilon                0.043799      4.5191e+06          4859.4          90.547
v  TurbVisc             4.4562e-12         0.51511       0.0050452        0.053727
v  CourantNb              0.034311           60504          51.743          8.7116
v  FourierNb              0.024214      2.3655e+05          22.052         0.36311
v  total_pressure       4.1431e+05      8.3553e+05      7.0989e+05      6.7645e+05
v  Local Time Step           0.001         0.01388       0.0010008       0.0010058


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90915      2.4636e+05          73.795          9.0747


 TIME FOR THE TIME STEP              746:        0.67950E+02

===============================================================


 INSTANT    0.747000000E+01   TIME STEP NUMBER             747
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.957437779E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328322914E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.94694E+02 0.11988E+02
   Friction velocity        uet   :  0.25181E-01 0.25507E+02
   Friction velocity        uk    :  0.36120E-01 0.25507E+02
   Dimensionless distance   yplus :  0.18493E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15536
   Nb of faces within the viscous sub-layer     :       9186
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16801E+02      67   0.11038E+00   0.67638E+02 0.32314E+02 
c  Velocity[X]                                      0.99822E+01 
c  Velocity[Y]                                      0.25675E+02 
c  Velocity[Z]                                      0.31981E+02 
c  Pressure     0.12761E+00     299   0.31923E-01   0.89891E-01 0.87608E+00 
c  k            0.94007E+00      26   0.64309E-03   0.19284E+00 0.51789E+02 
c  epsilon      0.89930E+04      18   0.32463E-03   0.13809E+08 0.78683E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023868                             3
a  epsilon                 -5.5848                             2
a  Local Time Step      1.6042e-08                        281457


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7365          19.118          2.2363          0.3656
v  Velocity[Y]             -37.594          44.442          1.3308         0.88669
v  Velocity[Z]             -68.397          42.982         -1.1171      -0.0065343
v  ǁVelocityǁ              0.02538          74.296          7.6422          7.6548
v  Pressure                 -85833      3.3551e+05      2.0988e+05      1.7644e+05
v  k                    4.6242e-09          16.681          0.1235         0.13474
v  epsilon                0.043848      4.5424e+06          4890.1           91.05
v  TurbVisc             4.4315e-12         0.51511       0.0050679        0.053796
v  CourantNb             0.0069704           62336          51.811           8.713
v  FourierNb              0.024236      2.3655e+05          22.049          0.3635
v  total_pressure       4.1417e+05      8.3551e+05      7.0988e+05      6.7644e+05
v  Local Time Step           0.001        0.013826       0.0010008       0.0010057


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.73928       2.483e+05           73.86          9.0766


 TIME FOR THE TIME STEP              747:        0.74921E+02

===============================================================


 INSTANT    0.748000000E+01   TIME STEP NUMBER             748
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.109686417E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328269440E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13559E+03 0.12433E+02
   Friction velocity        uet   :  0.14694E-01 0.27029E+02
   Friction velocity        uk    :  0.42791E-01 0.27029E+02
   Dimensionless distance   yplus :  0.24644E-02 0.25696E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15541
   Nb of faces within the viscous sub-layer     :       9182
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16803E+02      67   0.10866E+00   0.66971E+02 0.32157E+02 
c  Velocity[X]                                      0.96078E+01 
c  Velocity[Y]                                      0.25538E+02 
c  Velocity[Z]                                      0.31825E+02 
c  Pressure     0.12442E+00     328   0.31236E-01   0.87637E-01 0.82252E+00 
c  k            0.94351E+00      27   0.33293E-03   0.13448E+00 0.44142E+02 
c  epsilon      0.91149E+04      20   0.50888E-03   0.77737E+08 0.18551E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012329                             3
a  epsilon                 -1.1099                             2
a  Local Time Step      1.6251e-08                        281457


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7234          18.333          2.2372         0.36606
v  Velocity[Y]             -34.466          55.896          1.3393         0.88637
v  Velocity[Z]             -62.533          34.215         -1.1203      -0.0061758
v  ǁVelocityǁ             0.021712          66.115          7.6522          7.6559
v  Pressure                 -85910       3.355e+05      2.0987e+05      1.7645e+05
v  k                    1.6679e-07          17.446         0.12411         0.13498
v  epsilon                0.013958      4.5267e+06          4944.2          91.381
v  TurbVisc             1.0893e-17         0.51511       0.0050902        0.053857
v  CourantNb              0.064526           61535          51.939          8.7146
v  FourierNb              0.024267      2.3655e+05          22.048         0.36379
v  total_pressure       4.1409e+05       8.355e+05      7.0987e+05      6.7645e+05
v  Local Time Step           0.001        0.014206       0.0010008       0.0010057


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65434      2.4728e+05          73.988          9.0783


 TIME FOR THE TIME STEP              748:        0.73939E+02

===============================================================


 INSTANT    0.749000000E+01   TIME STEP NUMBER             749
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.543718192E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328215559E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11197E+03 0.11518E+02
   Friction velocity        uet   :  0.12798E-01 0.23399E+02
   Friction velocity        uk    :  0.47428E-01 0.23399E+02
   Dimensionless distance   yplus :  0.26055E-02 0.26283E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15549
   Nb of faces within the viscous sub-layer     :       9140
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16798E+02      58   0.10723E+00   0.65854E+02 0.31835E+02 
c  Velocity[X]                                      0.94671E+01 
c  Velocity[Y]                                      0.24941E+02 
c  Velocity[Z]                                      0.31446E+02 
c  Pressure     0.12244E+00     282   0.30802E-01   0.86329E-01 0.84471E+00 
c  k            0.93967E+00      33   0.47025E-03   0.13253E+00 0.43507E+02 
c  epsilon      0.91526E+04      15   0.27337E-03   0.37683E+08 0.13060E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023585                             8
a  epsilon                 -10.013                            10
a  Local Time Step       1.578e-08                        281459


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7423           18.99           2.239         0.36666
v  Velocity[Y]             -37.851          48.183          1.3481         0.88607
v  Velocity[Z]             -68.434          44.268          -1.126      -0.0057855
v  ǁVelocityǁ             0.017488          74.341          7.6622          7.6569
v  Pressure                 -86148      3.3551e+05      2.0987e+05      1.7646e+05
v  k                    2.4739e-06          15.906         0.12459         0.13519
v  epsilon                  0.0213      4.5626e+06          4936.5          91.734
v  TurbVisc             4.5013e-12         0.51511       0.0051102        0.053912
v  CourantNb              0.051103           63371          51.966          8.7178
v  FourierNb              0.024307      2.3655e+05          22.045         0.36392
v  total_pressure       4.1385e+05      8.3551e+05      7.0987e+05      6.7646e+05
v  Local Time Step           0.001        0.015145       0.0010008       0.0010058


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66275      2.4577e+05          74.011          9.0817


 TIME FOR THE TIME STEP              749:        0.74594E+02

===============================================================


 INSTANT    0.750000000E+01   TIME STEP NUMBER             750
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.817645800E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328210039E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13603E+03 0.11630E+02
   Friction velocity        uet   :  0.22656E-01 0.19532E+02
   Friction velocity        uk    :  0.59712E-01 0.19532E+02
   Dimensionless distance   yplus :  0.19112E-02 0.25081E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15578
   Nb of faces within the viscous sub-layer     :       9134
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16803E+02      56   0.11102E+00   0.66745E+02 0.32058E+02 
c  Velocity[X]                                      0.95861E+01 
c  Velocity[Y]                                      0.25113E+02 
c  Velocity[Z]                                      0.32046E+02 
c  Pressure     0.12180E+00     351   0.30751E-01   0.85812E-01 0.89671E+00 
c  k            0.93311E+00      31   0.42528E-03   0.12558E+00 0.42698E+02 
c  epsilon      0.92023E+04      18   0.36707E-03   0.68030E+08 0.17294E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00011539                             3
a  epsilon                -0.79087                             2
a  Local Time Step       1.577e-08                        281459


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7569          18.247          2.2368         0.36711
v  Velocity[Y]              -39.56          41.196          1.3577         0.88609
v  Velocity[Z]             -57.543          34.846         -1.1353      -0.0057111
v  ǁVelocityǁ             0.015882          60.887          7.6703          7.6582
v  Pressure                 -86310      3.3556e+05      2.0986e+05      1.7646e+05
v  k                    2.4519e-06          14.419          0.1248         0.13531
v  epsilon                 0.01364      4.5076e+06          4958.2          92.016
v  TurbVisc             4.1899e-12         0.51511       0.0051199        0.053957
v  CourantNb             0.0088073           63411          51.996          8.7203
v  FourierNb              0.024354      2.3655e+05          22.047         0.36404
v  total_pressure       4.1369e+05      8.3556e+05      7.0986e+05      6.7646e+05
v  Local Time Step           0.001        0.012097       0.0010008       0.0010056


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71324      2.4533e+05          74.043          9.0843


 TIME FOR THE TIME STEP              750:        0.88464E+02

===============================================================


 INSTANT    0.751000000E+01   TIME STEP NUMBER             751
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.160981715E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328173432E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10561E+03 0.11332E+02
   Friction velocity        uet   :  0.72191E-02 0.23658E+02
   Friction velocity        uk    :  0.41879E-01 0.23658E+02
   Dimensionless distance   yplus :  0.18123E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15599
   Nb of faces within the viscous sub-layer     :       9122
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16802E+02      57   0.10995E+00   0.70496E+02 0.32915E+02 
c  Velocity[X]                                      0.10198E+02 
c  Velocity[Y]                                      0.27491E+02 
c  Velocity[Z]                                      0.32808E+02 
c  Pressure     0.12783E+00     319   0.32350E-01   0.90119E-01 0.92813E+00 
c  k            0.92255E+00      33   0.35536E-03   0.13180E+00 0.44248E+02 
c  epsilon      0.91753E+04      16   0.31527E-03   0.43547E+08 0.14059E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022911                             2
a  epsilon                 -5.5668                             2
a  Local Time Step      1.5503e-08                        281467


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7604          19.119          2.2307         0.36704
v  Velocity[Y]             -38.371          50.847          1.3715         0.88589
v  Velocity[Z]             -69.537           39.89         -1.1387       -0.005517
v  ǁVelocityǁ             0.016397          75.574          7.6784          7.6591
v  Pressure                 -86539      3.3555e+05      2.0985e+05      1.7646e+05
v  k                    2.0119e-06          13.963          0.1244         0.13531
v  epsilon                0.043361      4.5367e+06          4945.1          91.785
v  TurbVisc             4.4449e-12         0.51511       0.0051166        0.053993
v  CourantNb              0.015243           64503          52.096          8.7233
v  FourierNb               0.02441      2.3655e+05          22.046         0.36397
v  total_pressure       4.1346e+05      8.3555e+05      7.0985e+05      6.7646e+05
v  Local Time Step           0.001        0.013307       0.0010008       0.0010057


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7193      2.4568e+05          74.142          9.0873


 TIME FOR THE TIME STEP              751:        0.76611E+02

===============================================================


 INSTANT    0.752000000E+01   TIME STEP NUMBER             752
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.179673227E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328133864E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13989E+03 0.10825E+02
   Friction velocity        uet   :  0.94136E-02 0.24296E+02
   Friction velocity        uk    :  0.32076E-01 0.24296E+02
   Dimensionless distance   yplus :  0.20586E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15605
   Nb of faces within the viscous sub-layer     :       9107
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16801E+02      57   0.10780E+00   0.72786E+02 0.33490E+02 
c  Velocity[X]                                      0.10135E+02 
c  Velocity[Y]                                      0.28918E+02 
c  Velocity[Z]                                      0.33732E+02 
c  Pressure     0.13273E+00     380   0.33711E-01   0.93617E-01 0.10020E+01 
c  k            0.91443E+00      27   0.67686E-03   0.15832E+00 0.46656E+02 
c  epsilon      0.91316E+04      17   0.27551E-03   0.61436E+07 0.50667E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001556                             3
a  epsilon                 -31.072                             3
a  Local Time Step      1.5665e-08                        281504


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.8017          18.078          2.2274         0.36743
v  Velocity[Y]             -34.788          38.558          1.3788         0.88556
v  Velocity[Z]             -59.374          35.109         -1.1376      -0.0053199
v  ǁVelocityǁ             0.016295          62.862          7.6803          7.6593
v  Pressure                 -86643      3.3553e+05      2.0984e+05      1.7647e+05
v  k                    1.9164e-06          14.829         0.12404         0.13527
v  epsilon                0.043629      4.4988e+06          4942.1          91.674
v  TurbVisc             2.8318e-12         0.51511       0.0051065        0.054021
v  CourantNb              0.059738           63838          52.169          8.7253
v  FourierNb              0.024471      2.3655e+05          22.046         0.36391
v  total_pressure       4.1336e+05      8.3553e+05      7.0984e+05      6.7647e+05
v  Local Time Step           0.001        0.014638       0.0010008       0.0010058


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82547      2.4474e+05          74.215          9.0893


 TIME FOR THE TIME STEP              752:        0.67859E+02

===============================================================


 INSTANT    0.753000000E+01   TIME STEP NUMBER             753
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.214211376E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328104857E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11158E+03 0.11113E+02
   Friction velocity        uet   :  0.31529E-01 0.20147E+02
   Friction velocity        uk    :  0.42110E-01 0.20147E+02
   Dimensionless distance   yplus :  0.20161E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15621
   Nb of faces within the viscous sub-layer     :       9081
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16800E+02      55   0.11034E+00   0.73152E+02 0.33546E+02 
c  Velocity[X]                                      0.10348E+02 
c  Velocity[Y]                                      0.29637E+02 
c  Velocity[Z]                                      0.33167E+02 
c  Pressure     0.13828E+00     395   0.35190E-01   0.97581E-01 0.10512E+01 
c  k            0.91207E+00      28   0.21468E-03   0.13009E+00 0.45725E+02 
c  epsilon      0.90901E+04      18   0.17974E-03   0.39185E+07 0.42541E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016819                             8
a  epsilon                  -13.25                            11
a  Local Time Step      1.5643e-08                        281489


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.8482          19.004          2.2277         0.36808
v  Velocity[Y]             -36.567          37.698          1.3867         0.88513
v  Velocity[Z]             -71.278          42.861         -1.1318      -0.0050884
v  ǁVelocityǁ            0.0062258           77.46          7.6833          7.6583
v  Pressure                 -86919      3.3551e+05      2.0984e+05      1.7646e+05
v  k                    1.6949e-06          14.933         0.12358         0.13516
v  epsilon               0.0012807      4.5172e+06          4934.9           91.48
v  TurbVisc             4.2462e-12         0.51511       0.0051008        0.054042
v  CourantNb               0.01199           63925          52.183          8.7278
v  FourierNb              0.024539      2.3655e+05          22.047         0.36382
v  total_pressure       4.1308e+05      8.3551e+05      7.0984e+05      6.7646e+05
v  Local Time Step           0.001        0.016102       0.0010008       0.0010058


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76132      2.4886e+05           74.23          9.0917


 TIME FOR THE TIME STEP              753:        0.79742E+02

===============================================================


 INSTANT    0.754000000E+01   TIME STEP NUMBER             754
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.145883656E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327999346E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14638E+03 0.10068E+02
   Friction velocity        uet   :  0.32915E-01 0.20753E+02
   Friction velocity        uk    :  0.45619E-01 0.20753E+02
   Dimensionless distance   yplus :  0.21075E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15593
   Nb of faces within the viscous sub-layer     :       9083
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16785E+02      58   0.10688E+00   0.76458E+02 0.34293E+02 
c  Velocity[X]                                      0.10888E+02 
c  Velocity[Y]                                      0.32405E+02 
c  Velocity[Z]                                      0.33166E+02 
c  Pressure     0.14037E+00     429   0.36343E-01   0.99300E-01 0.11825E+01 
c  k            0.90731E+00      24   0.23828E-03   0.13666E+00 0.47247E+02 
c  epsilon      0.90264E+04      15   0.17104E-03   0.37602E+07 0.41821E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021777                             4
a  epsilon                 -4.1991                             2
a  Local Time Step      1.5992e-08                        281495


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.8064          18.021          2.2247           0.369
v  Velocity[Y]             -40.025           45.39          1.3906         0.88518
v  Velocity[Z]             -61.184          35.012         -1.1253      -0.0055852
v  ǁVelocityǁ              0.01426          64.547          7.6782          7.6587
v  Pressure                 -86852      3.3546e+05      2.0982e+05      1.7652e+05
v  k                    2.0639e-06          14.537           0.123         0.13491
v  epsilon                0.021783       4.455e+06            4917          91.036
v  TurbVisc             4.1946e-12         0.51511       0.0051026        0.054055
v  CourantNb              0.041974           62532          52.194           8.728
v  FourierNb               0.02461      2.3655e+05           22.05         0.36372
v  total_pressure       4.1315e+05      8.3546e+05      7.0982e+05      6.7652e+05
v  Local Time Step           0.001        0.017712       0.0010008       0.0010058


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.56799       2.486e+05          74.244          9.0917


 TIME FOR THE TIME STEP              754:        0.78820E+02

===============================================================


 INSTANT    0.755000000E+01   TIME STEP NUMBER             755
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.263621475E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328075194E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11718E+03 0.92962E+01
   Friction velocity        uet   :  0.36651E-01 0.23974E+02
   Friction velocity        uk    :  0.46391E-01 0.23974E+02
   Dimensionless distance   yplus :  0.29487E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15621
   Nb of faces within the viscous sub-layer     :       9081
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16789E+02      55   0.11110E+00   0.79322E+02 0.34978E+02 
c  Velocity[X]                                      0.11007E+02 
c  Velocity[Y]                                      0.33349E+02 
c  Velocity[Z]                                      0.34966E+02 
c  Pressure     0.13925E+00     472   0.36680E-01   0.98607E-01 0.12567E+01 
c  k            0.90614E+00      27   0.26535E-03   0.15862E+00 0.51125E+02 
c  epsilon      0.89828E+04      15   0.14286E-03   0.36612E+07 0.41424E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001609                             2
a  epsilon                 -2.3251                             2
a  Local Time Step      1.5957e-08                        281479


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7689          18.966          2.2261         0.36935
v  Velocity[Y]             -39.136          33.345          1.3898         0.88507
v  Velocity[Z]             -69.026          44.473         -1.1173      -0.0066708
v  ǁVelocityǁ             0.016432          75.002          7.6766          7.6605
v  Pressure                 -86567      3.3539e+05      2.0979e+05      1.7655e+05
v  k                    1.1898e-06           13.92         0.12251         0.13464
v  epsilon                0.044488      4.4438e+06          4903.3          90.652
v  TurbVisc             4.4215e-12         0.51511       0.0051041        0.054052
v  CourantNb             0.0053735           62668          52.066          8.7284
v  FourierNb              0.024684      2.3655e+05          22.049         0.36348
v  total_pressure       4.1343e+05      8.3539e+05      7.0979e+05      6.7655e+05
v  Local Time Step           0.001        0.019483       0.0010008       0.0010059


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69249      2.4597e+05          74.115          9.0919


 TIME FOR THE TIME STEP              755:        0.89595E+02

===============================================================


 INSTANT    0.756000000E+01   TIME STEP NUMBER             756
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.185449141E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328174632E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13842E+03 0.10606E+02
   Friction velocity        uet   :  0.33565E-01 0.19025E+02
   Friction velocity        uk    :  0.61784E-01 0.19025E+02
   Dimensionless distance   yplus :  0.24276E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15619
   Nb of faces within the viscous sub-layer     :       9056
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16797E+02      55   0.11007E+00   0.76627E+02 0.34356E+02 
c  Velocity[X]                                      0.11227E+02 
c  Velocity[Y]                                      0.32249E+02 
c  Velocity[Z]                                      0.33151E+02 
c  Pressure     0.14112E+00     489   0.37765E-01   0.10005E+00 0.14535E+01 
c  k            0.90947E+00      27   0.37989E-03   0.19136E+00 0.55547E+02 
c  epsilon      0.89727E+04      16   0.19520E-03   0.52442E+07 0.49146E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.000232                             4
a  epsilon                 -24.502                             3
a  Local Time Step      1.5893e-08                        281499


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7741          18.228          2.2249         0.36903
v  Velocity[Y]             -34.633          34.646          1.3841         0.88517
v  Velocity[Z]             -58.841          35.511         -1.1008      -0.0084127
v  ǁVelocityǁ             0.015232          62.187          7.6685          7.6619
v  Pressure                 -86078      3.3531e+05      2.0972e+05      1.7661e+05
v  k                    1.8758e-06           13.04         0.12221         0.13436
v  epsilon                0.044814      4.4038e+06          4904.5          90.323
v  TurbVisc             1.2541e-12         0.51511       0.0051067        0.054042
v  CourantNb              0.013457           62923          52.025          8.7301
v  FourierNb               0.02476      2.3655e+05           22.05         0.36361
v  total_pressure       4.1392e+05      8.3531e+05      7.0972e+05      6.7661e+05
v  Local Time Step           0.001        0.013684       0.0010008       0.0010056


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5401      2.4916e+05          74.076          9.0937


 TIME FOR THE TIME STEP              756:        0.81190E+02

===============================================================


 INSTANT    0.757000000E+01   TIME STEP NUMBER             757
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.745813799E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328395595E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10992E+03 0.12132E+02
   Friction velocity        uet   :  0.28230E-01 0.17956E+02
   Friction velocity        uk    :  0.41777E-01 0.17956E+02
   Dimensionless distance   yplus :  0.18487E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15619
   Nb of faces within the viscous sub-layer     :       9070
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16800E+02      61   0.10806E+00   0.71173E+02 0.33140E+02 
c  Velocity[X]                                      0.11703E+02 
c  Velocity[Y]                                      0.29918E+02 
c  Velocity[Z]                                      0.29552E+02 
c  Pressure     0.14400E+00    1170   0.38760E-01   0.10217E+00 0.52577E+01 
c  k            0.91810E+00      29   0.51971E-03   0.19727E+00 0.55377E+02 
c  epsilon      0.89003E+04      14   0.27158E-03   0.10123E+08 0.68291E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016091                             7
a  epsilon                 -8.6783                            10
a  Local Time Step      1.5719e-08                        281473


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.8174          18.468          2.2231          0.3686
v  Velocity[Y]             -36.039          34.662          1.3722         0.88486
v  Velocity[Z]             -62.526          41.192         -1.0838      -0.0081011
v  ǁVelocityǁ             0.015201          68.012          7.6563          7.6608
v  Pressure                 -86787      3.3387e+05      2.0832e+05      1.7555e+05
v  k                    1.1308e-06          13.888         0.12186         0.13413
v  epsilon                0.015795      4.3052e+06          4871.2          90.042
v  TurbVisc             4.4878e-12         0.51511       0.0051175        0.054025
v  CourantNb             0.0014708           63617          51.908          8.7296
v  FourierNb              0.024835      2.3655e+05          22.052          0.3636
v  total_pressure       4.1321e+05      8.3387e+05      7.0832e+05      6.7555e+05
v  Local Time Step           0.001        0.015053       0.0010008       0.0010057


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70061      2.4688e+05           73.96          9.0932


 TIME FOR THE TIME STEP              757:        0.11640E+03

===============================================================


 INSTANT    0.758000000E+01   TIME STEP NUMBER             758
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.459326808E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328373206E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11700E+03 0.12404E+02
   Friction velocity        uet   :  0.10551E-01 0.12969E+02
   Friction velocity        uk    :  0.25194E-01 0.12969E+02
   Dimensionless distance   yplus :  0.13264E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15575
   Nb of faces within the viscous sub-layer     :       9081
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16793E+02      72   0.10685E+00   0.68881E+02 0.32591E+02 
c  Velocity[X]                                      0.10868E+02 
c  Velocity[Y]                                      0.27918E+02 
c  Velocity[Z]                                      0.30095E+02 
c  Pressure     0.14172E+00     503   0.37909E-01   0.10060E+00 0.16484E+01 
c  k            0.92522E+00      32   0.40574E-03   0.16665E+00 0.51230E+02 
c  epsilon      0.88745E+04      15   0.23056E-03   0.49290E+07 0.47044E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021988                             4
a  epsilon                 -4.3315                             2
a  Local Time Step      1.5581e-08                        281479


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.781          18.501          2.2236         0.36851
v  Velocity[Y]             -39.357          38.147          1.3582         0.88501
v  Velocity[Z]             -56.647          35.349         -1.0665      -0.0087727
v  ǁVelocityǁ             0.016623          60.028          7.6409          7.6613
v  Pressure                 -85921      3.3377e+05      2.0824e+05       1.756e+05
v  k                    2.4628e-06          15.539         0.12146         0.13392
v  epsilon                0.014543      4.2124e+06            4857          89.863
v  TurbVisc             4.4799e-12         0.51511       0.0051353        0.054005
v  CourantNb              0.050322           64179          51.815          8.7259
v  FourierNb              0.024908      2.3655e+05          22.056         0.36357
v  total_pressure       4.1408e+05      8.3377e+05      7.0824e+05       6.756e+05
v  Local Time Step           0.001        0.013615       0.0010008       0.0010056


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5805      2.4531e+05          73.871          9.0895


 TIME FOR THE TIME STEP              758:        0.84565E+02

===============================================================


 INSTANT    0.759000000E+01   TIME STEP NUMBER             759
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.104474146E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328493122E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10319E+03 0.11672E+02
   Friction velocity        uet   :  0.74800E-02 0.17863E+02
   Friction velocity        uk    :  0.39964E-01 0.17863E+02
   Dimensionless distance   yplus :  0.18105E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15602
   Nb of faces within the viscous sub-layer     :       9120
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16807E+02      57   0.10839E+00   0.70159E+02 0.32882E+02 
c  Velocity[X]                                      0.10496E+02 
c  Velocity[Y]                                      0.25990E+02 
c  Velocity[Z]                                      0.33672E+02 
c  Pressure     0.14188E+00     910   0.37971E-01   0.10055E+00 0.47483E+01 
c  k            0.92908E+00      31   0.22991E-03   0.13866E+00 0.47503E+02 
c  epsilon      0.87094E+04      14   0.29525E-03   0.47734E+08 0.15292E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014609                             4
a  epsilon                 -1.9183                             3
a  Local Time Step       1.571e-08                        281493


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7861           18.41          2.2199         0.36781
v  Velocity[Y]             -37.043          38.188          1.3407         0.88522
v  Velocity[Z]             -67.731          47.062         -1.0502       -0.008063
v  ǁVelocityǁ             0.014041          73.474          7.6199          7.6601
v  Pressure                 -86260       3.325e+05      2.0701e+05      1.7467e+05
v  k                     2.391e-06           15.91         0.12068         0.13368
v  epsilon                0.045837      4.1324e+06          4761.8           89.53
v  TurbVisc             4.7592e-12         0.51511       0.0051497         0.05398
v  CourantNb              0.032908           63655          51.684          8.7238
v  FourierNb              0.024979      2.3655e+05          22.059         0.36374
v  total_pressure       4.1374e+05       8.325e+05      7.0701e+05      6.7467e+05
v  Local Time Step           0.001        0.014976       0.0010008       0.0010058


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54551      2.4708e+05          73.743          9.0875


 TIME FOR THE TIME STEP              759:        0.94615E+02

===============================================================


 INSTANT    0.760000000E+01   TIME STEP NUMBER             760
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.720128501E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328401751E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13251E+03 0.11829E+02
   Friction velocity        uet   :  0.32234E-01 0.17852E+02
   Friction velocity        uk    :  0.47223E-01 0.17852E+02
   Dimensionless distance   yplus :  0.19539E-02 0.25084E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15582
   Nb of faces within the viscous sub-layer     :       9176
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16806E+02      60   0.10715E+00   0.67108E+02 0.32159E+02 
c  Velocity[X]                                      0.99438E+01 
c  Velocity[Y]                                      0.24216E+02 
c  Velocity[Z]                                      0.32948E+02 
c  Pressure     0.13220E+00     429   0.35501E-01   0.93730E-01 0.16667E+01 
c  k            0.92773E+00      26   0.36181E-03   0.14915E+00 0.49054E+02 
c  epsilon      0.85001E+04      15   0.29749E-03   0.29535E+08 0.12211E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00039493                             5
a  epsilon                  -259.3                             3
a  Local Time Step       1.582e-08                        281472


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6432          18.379          2.2202         0.36705
v  Velocity[Y]             -34.114          41.443           1.322         0.88611
v  Velocity[Z]             -57.149          35.183         -1.0359      -0.0085107
v  ǁVelocityǁ             0.014851          60.842          7.6042           7.659
v  Pressure                 -85350      3.3238e+05      2.0697e+05      1.7474e+05
v  k                    2.2138e-06          14.836         0.11987         0.13336
v  epsilon                0.045674       4.065e+06          4680.9          89.065
v  TurbVisc              4.238e-12         0.51511       0.0051551        0.053948
v  CourantNb              0.046589           63211          51.471          8.7202
v  FourierNb              0.025045      2.3655e+05          22.058          0.3636
v  total_pressure       4.1465e+05      8.3238e+05      7.0697e+05      6.7474e+05
v  Local Time Step           0.001        0.014012       0.0010008       0.0010058


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87742      2.4532e+05          73.529          9.0838


 TIME FOR THE TIME STEP              760:        0.74743E+02

===============================================================


 INSTANT    0.761000000E+01   TIME STEP NUMBER             761
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.385291319E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328493862E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10234E+03 0.11486E+02
   Friction velocity        uet   :  0.34289E-01 0.16770E+02
   Friction velocity        uk    :  0.48140E-01 0.16770E+02
   Dimensionless distance   yplus :  0.12063E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15557
   Nb of faces within the viscous sub-layer     :       9179
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16811E+02      62   0.10957E+00   0.64072E+02 0.31408E+02 
c  Velocity[X]                                      0.97192E+01 
c  Velocity[Y]                                      0.22925E+02 
c  Velocity[Z]                                      0.31428E+02 
c  Pressure     0.13024E+00     783   0.34644E-01   0.92321E-01 0.42046E+01 
c  k            0.92740E+00      24   0.23895E-03   0.14958E+00 0.49399E+02 
c  epsilon      0.84207E+04      14   0.21264E-03   0.12052E+08 0.78551E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0016117                             6
a  epsilon                 -9.8587                             7
a  Local Time Step      1.5561e-08                        281478


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6154          18.426          2.2216         0.36648
v  Velocity[Y]             -37.919          38.848          1.3045         0.88625
v  Velocity[Z]             -65.441          42.968         -1.0297      -0.0076773
v  ǁVelocityǁ             0.013245          70.976          7.5946          7.6569
v  Pressure                 -85520      3.3123e+05      2.0587e+05      1.7392e+05
v  k                    2.5319e-06          14.592         0.11928         0.13299
v  epsilon                0.045176      4.0042e+06          4636.8          88.691
v  TurbVisc             4.6444e-12         0.51511       0.0051556        0.053905
v  CourantNb                     0           64264          51.359          8.7178
v  FourierNb              0.025105      2.3655e+05          22.058         0.36347
v  total_pressure       4.1448e+05      8.3123e+05      7.0587e+05      6.7392e+05
v  Local Time Step           0.001        0.015413       0.0010008       0.0010058


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70988      2.4703e+05          73.417          9.0813


 TIME FOR THE TIME STEP              761:        0.98942E+02

===============================================================


 INSTANT    0.762000000E+01   TIME STEP NUMBER             762
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.166855079E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328419870E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12600E+03 0.11812E+02
   Friction velocity        uet   :  0.18986E-01 0.17646E+02
   Friction velocity        uk    :  0.64385E-01 0.17646E+02
   Dimensionless distance   yplus :  0.22517E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15545
   Nb of faces within the viscous sub-layer     :       9186
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16808E+02      72   0.11055E+00   0.65568E+02 0.31804E+02 
c  Velocity[X]                                      0.95285E+01 
c  Velocity[Y]                                      0.23903E+02 
c  Velocity[Z]                                      0.32136E+02 
c  Pressure     0.13097E+00     407   0.34216E-01   0.92859E-01 0.13934E+01 
c  k            0.92632E+00      25   0.46705E-03   0.19285E+00 0.55522E+02 
c  epsilon      0.83095E+04      18   0.23838E-03   0.21711E+08 0.10622E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020205                             4
a  epsilon                 -4.0798                             2
a  Local Time Step      1.5537e-08                        281481


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7091          18.382          2.2197         0.36657
v  Velocity[Y]             -40.626          45.873          1.2877         0.88654
v  Velocity[Z]             -54.027          35.555         -1.0285      -0.0079187
v  ǁVelocityǁ             0.011526          57.275          7.5869          7.6552
v  Pressure                 -86794      3.3124e+05      2.0584e+05      1.7395e+05
v  k                    1.9765e-06          14.793         0.11862         0.13258
v  epsilon                0.020763      3.1398e+06          4600.7          88.256
v  TurbVisc             4.6573e-12         0.51511       0.0051464        0.053851
v  CourantNb              0.066551           64362          51.306          8.7157
v  FourierNb              0.025159      2.3655e+05          22.055         0.36336
v  total_pressure       4.1321e+05      8.3124e+05      7.0584e+05      6.7395e+05
v  Local Time Step           0.001         0.01691       0.0010008       0.0010057


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76068      2.4696e+05          73.361          9.0791


 TIME FOR THE TIME STEP              762:        0.78757E+02

===============================================================


 INSTANT    0.763000000E+01   TIME STEP NUMBER             763
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.274437363E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328463299E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.94542E+02 0.11826E+02
   Friction velocity        uet   :  0.34599E-01 0.17681E+02
   Friction velocity        uk    :  0.45842E-01 0.17681E+02
   Dimensionless distance   yplus :  0.10278E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15535
   Nb of faces within the viscous sub-layer     :       9186
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16811E+02      60   0.10845E+00   0.66698E+02 0.32013E+02 
c  Velocity[X]                                      0.94431E+01 
c  Velocity[Y]                                      0.24640E+02 
c  Velocity[Z]                                      0.32615E+02 
c  Pressure     0.13437E+00     429   0.34545E-01   0.95352E-01 0.12946E+01 
c  k            0.92590E+00      23   0.49266E-03   0.24569E+00 0.63402E+02 
c  epsilon      0.82503E+04      19   0.24265E-03   0.79630E+07 0.64848E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012045                             3
a  epsilon                 -1.0832                             2
a  Local Time Step      1.5555e-08                        281470


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5464          18.433          2.2185         0.36691
v  Velocity[Y]             -41.333          42.921          1.2787         0.88638
v  Velocity[Z]             -66.897          41.462         -1.0378      -0.0088551
v  ǁVelocityǁ             0.017152           72.57          7.5903          7.6551
v  Pressure                 -91003      3.3123e+05       2.058e+05      1.7397e+05
v  k                    2.0843e-06          15.266         0.11798         0.13213
v  epsilon                 0.04434      3.1366e+06          4574.7          87.785
v  TurbVisc             4.1744e-12         0.51511       0.0051208        0.053791
v  CourantNb               0.02455           64288          51.243          8.7137
v  FourierNb              0.025207      2.3655e+05           22.05         0.36328
v  total_pressure         4.09e+05      8.3123e+05       7.058e+05      6.7397e+05
v  Local Time Step           0.001        0.018601       0.0010008       0.0010058


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47147       2.491e+05          73.293          9.0769


 TIME FOR THE TIME STEP              763:        0.78243E+02

===============================================================


 INSTANT    0.764000000E+01   TIME STEP NUMBER             764
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.705416584E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328570355E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13068E+03 0.11144E+02
   Friction velocity        uet   :  0.35574E-01 0.21535E+02
   Friction velocity        uk    :  0.39136E-01 0.21535E+02
   Dimensionless distance   yplus :  0.26342E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15535
   Nb of faces within the viscous sub-layer     :       9213
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16814E+02      57   0.10769E+00   0.65897E+02 0.31871E+02 
c  Velocity[X]                                      0.98580E+01 
c  Velocity[Y]                                      0.25268E+02 
c  Velocity[Z]                                      0.30771E+02 
c  Pressure     0.12982E+00     673   0.33592E-01   0.92074E-01 0.14106E+01 
c  k            0.92142E+00      22   0.68503E-03   0.20943E+00 0.58322E+02 
c  epsilon      0.82104E+04      18   0.19529E-03   0.53304E+07 0.53078E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018666                             3
a  epsilon                 -3.3868                             2
a  Local Time Step      1.5671e-08                        281457


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5164          18.233          2.2183         0.36706
v  Velocity[Y]             -37.885           47.22          1.2771         0.88704
v  Velocity[Z]             -56.415          35.785         -1.0485      -0.0095297
v  ǁVelocityǁ            0.0082854          60.078          7.5966          7.6551
v  Pressure                 -94648      3.3116e+05       2.057e+05      1.7389e+05
v  k                    2.9346e-06          15.459         0.11737         0.13177
v  epsilon                0.044156      3.1963e+06          4559.6          87.421
v  TurbVisc             4.4472e-12         0.51511       0.0050813        0.053726
v  CourantNb              0.031917           63814          51.282           8.715
v  FourierNb              0.025247      2.3655e+05          22.045         0.36305
v  total_pressure       4.0535e+05      8.3116e+05       7.057e+05      6.7389e+05
v  Local Time Step           0.001        0.020111       0.0010008       0.0010057


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68718      2.4638e+05          73.327           9.078


 TIME FOR THE TIME STEP              764:        0.80365E+02

===============================================================


 INSTANT    0.765000000E+01   TIME STEP NUMBER             765
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.375760795E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328617989E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93972E+02 0.11136E+02
   Friction velocity        uet   :  0.26959E-01 0.26478E+02
   Friction velocity        uk    :  0.32407E-01 0.26478E+02
   Dimensionless distance   yplus :  0.31458E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15556
   Nb of faces within the viscous sub-layer     :       9210
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16812E+02      62   0.11105E+00   0.65376E+02 0.31755E+02 
c  Velocity[X]                                      0.96291E+01 
c  Velocity[Y]                                      0.25903E+02 
c  Velocity[Z]                                      0.29845E+02 
c  Pressure     0.12942E+00    1068   0.34034E-01   0.91611E-01 0.33970E+01 
c  k            0.91613E+00      22   0.64289E-03   0.19673E+00 0.56712E+02 
c  epsilon      0.82348E+04      15   0.26663E-03   0.66342E+07 0.59273E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014118                             2
a  epsilon                 -1.8505                             2
a  Local Time Step      1.5899e-08                        281445


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5359          18.811          2.2176         0.36728
v  Velocity[Y]             -38.761          40.635          1.2819          0.8878
v  Velocity[Z]             -65.436          41.921         -1.0592      -0.0087458
v  ǁVelocityǁ            0.0089925           71.11          7.6047          7.6529
v  Pressure                 -97718       3.304e+05      2.0491e+05      1.7322e+05
v  k                    2.3699e-06          15.452         0.11692         0.13139
v  epsilon                0.043977      3.2107e+06          4573.8          87.085
v  TurbVisc             4.4513e-12         0.51511       0.0050353        0.053667
v  CourantNb                0.0916           62898          51.326          8.7163
v  FourierNb              0.025279      2.3655e+05          22.041         0.36279
v  total_pressure       4.0228e+05       8.304e+05      7.0491e+05      6.7322e+05
v  Local Time Step           0.001        0.018658       0.0010008       0.0010057


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72773      2.4584e+05          73.366          9.0791


 TIME FOR THE TIME STEP              765:        0.11456E+03

===============================================================


 INSTANT    0.766000000E+01   TIME STEP NUMBER             766
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.130462103E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328488396E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12622E+03 0.10678E+02
   Friction velocity        uet   :  0.33485E-01 0.23474E+02
   Friction velocity        uk    :  0.42488E-01 0.23474E+02
   Dimensionless distance   yplus :  0.26994E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15556
   Nb of faces within the viscous sub-layer     :       9205
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16799E+02      63   0.10790E+00   0.69713E+02 0.32797E+02 
c  Velocity[X]                                      0.10305E+02 
c  Velocity[Y]                                      0.26862E+02 
c  Velocity[Z]                                      0.32546E+02 
c  Pressure     0.13596E+00     569   0.35422E-01   0.96112E-01 0.14549E+01 
c  k            0.91032E+00      23   0.66578E-03   0.22888E+00 0.61331E+02 
c  epsilon      0.82299E+04      17   0.20446E-03   0.54827E+07 0.53949E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00013255                             5
a  epsilon                 -7.7103                             6
a  Local Time Step      1.6082e-08                        281459


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5683           18.32          2.2174         0.36717
v  Velocity[Y]             -36.789          41.557          1.2842         0.88894
v  Velocity[Z]             -58.851          35.678         -1.0701      -0.0083198
v  ǁVelocityǁ             0.018944          62.213          7.6082          7.6506
v  Pressure                 -97976      3.3045e+05      2.0489e+05      1.7314e+05
v  k                    9.5452e-07          14.652         0.11638         0.13102
v  epsilon                0.043693      3.2626e+06          4577.7          86.666
v  TurbVisc             4.4398e-12         0.51511       0.0049829        0.053609
v  CourantNb              0.028697           62181          51.416          8.7158
v  FourierNb              0.025302      2.3655e+05          22.035         0.36237
v  total_pressure       4.0202e+05      8.3045e+05      7.0489e+05      6.7314e+05
v  Local Time Step           0.001        0.020524       0.0010009       0.0010059


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60579      2.4611e+05          73.452          9.0782


 TIME FOR THE TIME STEP              766:        0.73324E+02

===============================================================


 INSTANT    0.767000000E+01   TIME STEP NUMBER             767
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.175070811E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328329152E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.95291E+02 0.10062E+02
   Friction velocity        uet   :  0.31894E-01 0.21710E+02
   Friction velocity        uk    :  0.63912E-01 0.21710E+02
   Dimensionless distance   yplus :  0.18141E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15558
   Nb of faces within the viscous sub-layer     :       9147
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16793E+02      62   0.10557E+00   0.69883E+02 0.32806E+02 
c  Velocity[X]                                      0.10617E+02 
c  Velocity[Y]                                      0.25831E+02 
c  Velocity[Z]                                      0.33435E+02 
c  Pressure     0.13402E+00     513   0.35462E-01   0.94878E-01 0.13284E+01 
c  k            0.90921E+00      24   0.42135E-03   0.15305E+00 0.49815E+02 
c  epsilon      0.82818E+04      15   0.23238E-03   0.11986E+08 0.79268E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018175                             1
a  epsilon                 -3.5519                             2
a  Local Time Step      1.5994e-08                        281444


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7207          18.905          2.2179         0.36645
v  Velocity[Y]             -38.761          37.049          1.2829         0.88909
v  Velocity[Z]             -69.482           39.39         -1.0803      -0.0071435
v  ǁVelocityǁ              0.01322          75.522          7.6128          7.6477
v  Pressure                 -95376      3.3054e+05      2.0492e+05       1.731e+05
v  k                    2.0226e-06          14.193         0.11631         0.13084
v  epsilon                0.024736      3.3199e+06            4608          86.566
v  TurbVisc             4.5707e-12         0.51511       0.0049327        0.053553
v  CourantNb              0.014382           62523           51.48          8.7146
v  FourierNb              0.025317      2.3655e+05          22.032         0.36202
v  total_pressure       4.0462e+05      8.3054e+05      7.0492e+05       6.731e+05
v  Local Time Step           0.001        0.022576       0.0010009       0.0010059


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.60907      2.4816e+05          73.512          9.0766


 TIME FOR THE TIME STEP              767:        0.85305E+02

===============================================================


 INSTANT    0.768000000E+01   TIME STEP NUMBER             768
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.767566974E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328130707E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14016E+03 0.10516E+02
   Friction velocity        uet   :  0.21653E-01 0.20912E+02
   Friction velocity        uk    :  0.28944E-01 0.20912E+02
   Dimensionless distance   yplus :  0.18974E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15567
   Nb of faces within the viscous sub-layer     :       9161
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16789E+02      65   0.10590E+00   0.68216E+02 0.32420E+02 
c  Velocity[X]                                      0.10445E+02 
c  Velocity[Y]                                      0.26376E+02 
c  Velocity[Z]                                      0.31396E+02 
c  Pressure     0.13199E+00     471   0.35403E-01   0.93285E-01 0.12687E+01 
c  k            0.90923E+00      25   0.35094E-03   0.11922E+00 0.43757E+02 
c  epsilon      0.83287E+04      15   0.23905E-03   0.13085E+08 0.82478E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001672                             4
a  epsilon                  -2.011                             3
a  Local Time Step      1.5955e-08                        281448


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]               -8.82          18.072          2.2228         0.36608
v  Velocity[Y]             -38.771          47.631          1.2823         0.88863
v  Velocity[Z]             -60.658          36.276         -1.0881      -0.0053059
v  ǁVelocityǁ             0.015836          63.687          7.6175          7.6454
v  Pressure                 -91835      3.3062e+05      2.0499e+05      1.7308e+05
v  k                    1.8333e-06          14.018         0.11612         0.13072
v  epsilon                0.043088      3.3537e+06          4633.7          86.398
v  TurbVisc             4.4985e-12         0.51511       0.0048923        0.053514
v  CourantNb              0.030941           62675          51.524          8.7126
v  FourierNb              0.025323      2.3655e+05          22.029          0.3618
v  total_pressure       4.0817e+05      8.3062e+05      7.0499e+05      6.7308e+05
v  Local Time Step           0.001        0.019858       0.0010008        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.41074      2.4513e+05          73.553          9.0744


 TIME FOR THE TIME STEP              768:        0.74427E+02

===============================================================


 INSTANT    0.769000000E+01   TIME STEP NUMBER             769
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.114420988E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327930941E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11489E+03 0.11100E+02
   Friction velocity        uet   :  0.28922E-01 0.19442E+02
   Friction velocity        uk    :  0.40568E-01 0.19442E+02
   Dimensionless distance   yplus :  0.19798E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15534
   Nb of faces within the viscous sub-layer     :       9138
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16787E+02      62   0.10996E+00   0.67834E+02 0.32398E+02 
c  Velocity[X]                                      0.10833E+02 
c  Velocity[Y]                                      0.25806E+02 
c  Velocity[Z]                                      0.31195E+02 
c  Pressure     0.13385E+00     459   0.36043E-01   0.94546E-01 0.12256E+01 
c  k            0.91404E+00      26   0.26502E-03   0.91911E-01 0.37880E+02 
c  epsilon      0.83801E+04      17   0.19334E-03   0.66119E+07 0.58277E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020126                             3
a  epsilon                 -3.3666                             2
a  Local Time Step      1.5847e-08                        281444


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9676          18.864          2.2244          0.3657
v  Velocity[Y]             -38.477          38.288          1.2837         0.88808
v  Velocity[Z]             -66.073          39.005          -1.091      -0.0029452
v  ǁVelocityǁ             0.014164          71.938          7.6204          7.6426
v  Pressure                 -86973      3.3069e+05      2.0508e+05      1.7305e+05
v  k                    2.0707e-06           13.88         0.11655         0.13075
v  epsilon                0.042673      3.4029e+06          4649.3          86.577
v  TurbVisc              4.036e-12         0.51511       0.0048642        0.053483
v  CourantNb               0.03198           63103          51.648          8.7112
v  FourierNb              0.025321      2.3655e+05           22.03         0.36168
v  total_pressure       4.1303e+05      8.3069e+05      7.0508e+05      6.7305e+05
v  Local Time Step           0.001        0.021844       0.0010008       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45649      2.5174e+05          73.678          9.0729


 TIME FOR THE TIME STEP              769:        0.82681E+02

===============================================================


 INSTANT    0.770000000E+01   TIME STEP NUMBER             770
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.893855677E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327650693E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12878E+03 0.12026E+02
   Friction velocity        uet   :  0.32695E-01 0.20731E+02
   Friction velocity        uk    :  0.49316E-01 0.20731E+02
   Dimensionless distance   yplus :  0.18030E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15525
   Nb of faces within the viscous sub-layer     :       9147
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16773E+02      60   0.10870E+00   0.68378E+02 0.32522E+02 
c  Velocity[X]                                      0.11408E+02 
c  Velocity[Y]                                      0.25193E+02 
c  Velocity[Z]                                      0.31777E+02 
c  Pressure     0.13741E+00     805   0.36643E-01   0.96974E-01 0.40207E+01 
c  k            0.92003E+00      24   0.32472E-03   0.90889E-01 0.36874E+02 
c  epsilon      0.85343E+04      16   0.11489E-02   0.55658E+08 0.16571E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021312                             4
a  epsilon                  -3.492                             2
a  Local Time Step      1.6533e-08                        281457


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9735          17.881          2.2297         0.36613
v  Velocity[Y]             -35.751          44.144          1.2791         0.88771
v  Velocity[Z]             -58.015           35.26          -1.094       -0.002242
v  ǁVelocityǁ             0.002512          61.503          7.6193          7.6419
v  Pressure                 -86095       3.318e+05       2.062e+05      1.7387e+05
v  k                    1.8159e-06          14.337         0.11702         0.13092
v  epsilon                0.042404      4.6766e+06          4736.1          86.842
v  TurbVisc             4.4296e-12         0.51511       0.0048515        0.053465
v  CourantNb              0.080866           60486          51.716          8.7085
v  FourierNb              0.025309      2.3655e+05          22.032         0.36149
v  total_pressure       4.1391e+05       8.318e+05       7.062e+05      6.7387e+05
v  Local Time Step           0.001        0.024028       0.0010009       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75701      2.5075e+05          73.748            9.07


 TIME FOR THE TIME STEP              770:        0.96121E+02

===============================================================


 INSTANT    0.771000000E+01   TIME STEP NUMBER             771
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.153574306E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327601711E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.93416E+02 0.11480E+02
   Friction velocity        uet   :  0.36073E-01 0.24282E+02
   Friction velocity        uk    :  0.38831E-01 0.24282E+02
   Dimensionless distance   yplus :  0.17599E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15504
   Nb of faces within the viscous sub-layer     :       9127
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16778E+02      74   0.10803E+00   0.68863E+02 0.32645E+02 
c  Velocity[X]                                      0.11405E+02 
c  Velocity[Y]                                      0.26355E+02 
c  Velocity[Z]                                      0.31102E+02 
c  Pressure     0.13683E+00     727   0.37002E-01   0.96532E-01 0.77147E+01 
c  k            0.92321E+00      27   0.25752E-03   0.96750E-01 0.38230E+02 
c  epsilon      0.86852E+04      17   0.45166E-03   0.30179E+08 0.12107E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023092                             3
a  epsilon                 -4.5379                             2
a  Local Time Step      1.6459e-08                        281461


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9978          18.716          2.2302         0.36664
v  Velocity[Y]             -35.405          36.632          1.2749         0.88753
v  Velocity[Z]             -67.438          40.527         -1.0927        -0.00481
v  ǁVelocityǁ            0.0019547          73.396          7.6141          7.6445
v  Pressure                 -84883      3.3389e+05      2.0828e+05      1.7549e+05
v  k                     2.099e-06           14.74         0.11774          0.1312
v  epsilon                0.042201      4.3662e+06          4766.2          87.201
v  TurbVisc             3.7916e-12         0.51511       0.0048568        0.053462
v  CourantNb              0.019439           60758           51.77          8.7073
v  FourierNb              0.025289      2.3655e+05          22.038          0.3615
v  total_pressure       4.1512e+05      8.3389e+05      7.0828e+05      6.7549e+05
v  Local Time Step           0.001        0.026431       0.0010008       0.0010063


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94619       2.513e+05          73.808          9.0688


 TIME FOR THE TIME STEP              771:        0.86910E+02

===============================================================


 INSTANT    0.772000000E+01   TIME STEP NUMBER             772
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.947803060E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327884592E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13301E+03 0.11466E+02
   Friction velocity        uet   :  0.34276E-01 0.23734E+02
   Friction velocity        uk    :  0.54833E-01 0.23734E+02
   Dimensionless distance   yplus :  0.19350E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15529
   Nb of faces within the viscous sub-layer     :       9144
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16793E+02      59   0.10781E+00   0.70454E+02 0.32935E+02 
c  Velocity[X]                                      0.11647E+02 
c  Velocity[Y]                                      0.27304E+02 
c  Velocity[Z]                                      0.31502E+02 
c  Pressure     0.13519E+00     359   0.36637E-01   0.95403E-01 0.11571E+01 
c  k            0.92806E+00      23   0.34536E-03   0.10065E+00 0.38621E+02 
c  epsilon      0.87370E+04      15   0.40738E-03   0.27064E+08 0.11442E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020945                             5
a  epsilon                 -3.1623                             3
a  Local Time Step      1.6328e-08                        281440


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.938           18.66           2.231         0.36692
v  Velocity[Y]             -40.091          46.647          1.2729         0.88754
v  Velocity[Z]             -62.151          35.147         -1.0919        -0.00637
v  ǁVelocityǁ             0.014642          65.354          7.6069           7.647
v  Pressure                 -85236      3.3385e+05       2.083e+05      1.7544e+05
v  k                     2.311e-06          15.337          0.1185         0.13155
v  epsilon                0.042523      4.4101e+06          4789.6          87.615
v  TurbVisc             4.3911e-12         0.51511       0.0048744        0.053479
v  CourantNb              0.065992           61244          51.741          8.7073
v  FourierNb              0.025259      2.3655e+05          22.043         0.36162
v  total_pressure       4.1476e+05      8.3385e+05       7.083e+05      6.7544e+05
v  Local Time Step           0.001        0.023485       0.0010009       0.0010063


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61015      2.4917e+05          73.784          9.0689


 TIME FOR THE TIME STEP              772:        0.68209E+02

===============================================================


 INSTANT    0.773000000E+01   TIME STEP NUMBER             773
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.114242554E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328119167E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12012E+03 0.11659E+02
   Friction velocity        uet   :  0.15666E-01 0.24500E+02
   Friction velocity        uk    :  0.24852E-01 0.24500E+02
   Dimensionless distance   yplus :  0.22794E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15517
   Nb of faces within the viscous sub-layer     :       9133
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16800E+02      66   0.10839E+00   0.71527E+02 0.33242E+02 
c  Velocity[X]                                      0.11479E+02 
c  Velocity[Y]                                      0.28833E+02 
c  Velocity[Z]                                      0.31215E+02 
c  Pressure     0.13673E+00     610   0.36677E-01   0.96543E-01 0.11359E+01 
c  k            0.93097E+00      26   0.30354E-03   0.12054E+00 0.42138E+02 
c  epsilon      0.88428E+04      15   0.64824E-03   0.42143E+08 0.14109E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023172                             4
a  epsilon                 -4.9901                             3
a  Local Time Step      1.6178e-08                        281460


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9342          18.759           2.233         0.36676
v  Velocity[Y]             -35.366          42.749          1.2713         0.88748
v  Velocity[Z]             -65.534          43.788         -1.0921      -0.0074952
v  ǁVelocityǁ             0.022264          71.361          7.6017          7.6482
v  Pressure                 -85687      3.3377e+05      2.0829e+05      1.7537e+05
v  k                    2.3306e-06          14.739         0.11916         0.13197
v  epsilon                0.043102      4.6035e+06          4841.8          88.015
v  TurbVisc             4.6108e-12         0.51511       0.0048921        0.053508
v  CourantNb              0.048955           61811          51.655          8.7079
v  FourierNb               0.02522      2.3655e+05           22.05         0.36169
v  total_pressure       4.1431e+05      8.3377e+05      7.0829e+05      6.7537e+05
v  Local Time Step           0.001        0.025833       0.0010008       0.0010063


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82018      2.4652e+05          73.705          9.0696


 TIME FOR THE TIME STEP              773:        0.82913E+02

===============================================================


 INSTANT    0.774000000E+01   TIME STEP NUMBER             774
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.818307571E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328238319E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12686E+03 0.10276E+02
   Friction velocity        uet   :  0.22997E-01 0.28659E+02
   Friction velocity        uk    :  0.29394E-01 0.28659E+02
   Dimensionless distance   yplus :  0.22199E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15499
   Nb of faces within the viscous sub-layer     :       9136
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16793E+02      62   0.11056E+00   0.71575E+02 0.33133E+02 
c  Velocity[X]                                      0.11084E+02 
c  Velocity[Y]                                      0.29750E+02 
c  Velocity[Z]                                      0.30741E+02 
c  Pressure     0.13968E+00     438   0.37309E-01   0.98720E-01 0.11268E+01 
c  k            0.92389E+00      26   0.56268E-03   0.13358E+00 0.44379E+02 
c  epsilon      0.88168E+04      19   0.32956E-03   0.79755E+07 0.61790E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019614                             4
a  epsilon                 -3.5108                             2
a  Local Time Step      1.6077e-08                        281459


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.8497          18.839          2.2312         0.36671
v  Velocity[Y]              -34.38          51.002          1.2728         0.88772
v  Velocity[Z]             -62.793          34.967         -1.0939      -0.0081677
v  ǁVelocityǁ             0.015934          66.164          7.5958            7.65
v  Pressure                 -85993      3.3371e+05      2.0828e+05      1.7533e+05
v  k                    2.0867e-06          14.543         0.11916         0.13236
v  epsilon                0.043941      4.4913e+06          4812.3          88.157
v  TurbVisc             4.4951e-12         0.51511       0.0048999        0.053552
v  CourantNb              0.015105           62202          51.623          8.7066
v  FourierNb              0.025171      2.3655e+05          22.052         0.36181
v  total_pressure       4.1401e+05      8.3371e+05      7.0828e+05      6.7533e+05
v  Local Time Step           0.001        0.028416       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83989      2.4711e+05          73.675          9.0684


 TIME FOR THE TIME STEP              774:        0.72974E+02

===============================================================


 INSTANT    0.775000000E+01   TIME STEP NUMBER             775
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.189729135E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328372402E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12270E+03 0.90799E+01
   Friction velocity        uet   :  0.34234E-01 0.27518E+02
   Friction velocity        uk    :  0.45441E-01 0.27518E+02
   Dimensionless distance   yplus :  0.26447E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15486
   Nb of faces within the viscous sub-layer     :       9155
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16799E+02      58   0.10736E+00   0.69322E+02 0.32730E+02 
c  Velocity[X]                                      0.10696E+02 
c  Velocity[Y]                                      0.28332E+02 
c  Velocity[Z]                                      0.30293E+02 
c  Pressure     0.14081E+00     448   0.37736E-01   0.99481E-01 0.11389E+01 
c  k            0.92085E+00      29   0.41535E-03   0.10772E+00 0.39413E+02 
c  epsilon      0.87558E+04      14   0.21362E-03   0.47863E+07 0.47647E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020523                             8
a  epsilon                 -9.7364                            10
a  Local Time Step      1.5809e-08                        281446


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.8584           18.81          2.2294         0.36624
v  Velocity[Y]             -37.913          38.068          1.2758         0.88808
v  Velocity[Z]             -66.355          41.347         -1.0925       -0.008284
v  ǁVelocityǁ              0.01246           72.02          7.5944          7.6514
v  Pressure                 -86014      3.3363e+05      2.0824e+05      1.7529e+05
v  k                    7.7291e-07          14.386         0.11908         0.13279
v  epsilon                0.025362      4.4328e+06          4816.4          88.419
v  TurbVisc             4.4706e-12         0.51511       0.0048962        0.053601
v  CourantNb             0.0032737           63254          51.545          8.7067
v  FourierNb              0.025115      2.3655e+05          22.048         0.36192
v  total_pressure       4.1399e+05      8.3363e+05      7.0824e+05      6.7529e+05
v  Local Time Step           0.001        0.031258       0.0010009       0.0010064


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66022      2.4594e+05          73.594          9.0687


 TIME FOR THE TIME STEP              775:        0.76565E+02

===============================================================


 INSTANT    0.776000000E+01   TIME STEP NUMBER             776
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.104116877E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328419595E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12830E+03 0.92292E+01
   Friction velocity        uet   :  0.25382E-01 0.33415E+02
   Friction velocity        uk    :  0.51311E-01 0.33415E+02
   Dimensionless distance   yplus :  0.26507E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15501
   Nb of faces within the viscous sub-layer     :       9150
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16798E+02      59   0.10752E+00   0.68096E+02 0.32383E+02 
c  Velocity[X]                                      0.10780E+02 
c  Velocity[Y]                                      0.27711E+02 
c  Velocity[Z]                                      0.29605E+02 
c  Pressure     0.13993E+00     495   0.37549E-01   0.98738E-01 0.11228E+01 
c  k            0.92048E+00      23   0.21879E-03   0.56939E-01 0.28899E+02 
c  epsilon      0.87050E+04      13   0.18720E-03   0.32569E+07 0.39687E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022188                             3
a  epsilon                 -4.2947                             2
a  Local Time Step      1.5876e-08                        281438


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.785          18.414          2.2332         0.36591
v  Velocity[Y]             -41.328          49.621           1.282           0.888
v  Velocity[Z]             -61.095          34.353         -1.0878      -0.0082875
v  ǁVelocityǁ             0.011541          64.289          7.5939          7.6526
v  Pressure                 -85839       3.335e+05      2.0818e+05      1.7527e+05
v  k                    2.1046e-06          14.969         0.11872         0.13315
v  epsilon                0.033397      4.4027e+06          4800.2          88.621
v  TurbVisc             2.9442e-13         0.51511       0.0048847        0.053661
v  CourantNb              0.062556           62987          51.581          8.7057
v  FourierNb              0.025053      2.3655e+05          22.042         0.36196
v  total_pressure       4.1416e+05       8.335e+05      7.0818e+05      6.7527e+05
v  Local Time Step           0.001        0.034384       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91392      2.4978e+05          73.623          9.0677


 TIME FOR THE TIME STEP              776:        0.86864E+02

===============================================================


 INSTANT    0.777000000E+01   TIME STEP NUMBER             777
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.126310593E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328444897E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11676E+03 0.97080E+01
   Friction velocity        uet   :  0.54923E-02 0.31440E+02
   Friction velocity        uk    :  0.58100E-01 0.31440E+02
   Dimensionless distance   yplus :  0.26499E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15508
   Nb of faces within the viscous sub-layer     :       9156
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16798E+02      63   0.10877E+00   0.71484E+02 0.33228E+02 
c  Velocity[X]                                      0.10704E+02 
c  Velocity[Y]                                      0.30351E+02 
c  Velocity[Z]                                      0.30428E+02 
c  Pressure     0.14171E+00     382   0.37893E-01   0.99917E-01 0.10879E+01 
c  k            0.92071E+00      23   0.28675E-03   0.72209E-01 0.32529E+02 
c  epsilon      0.86875E+04      13   0.23058E-03   0.10948E+08 0.72729E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015901                             3
a  epsilon                 -2.2298                             2
a  Local Time Step      1.5806e-08                        281444


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.8238          18.429          2.2338         0.36574
v  Velocity[Y]              -38.58          33.606          1.2921         0.88763
v  Velocity[Z]             -65.746          46.537         -1.0821      -0.0083464
v  ǁVelocityǁ              0.02168          71.278          7.5978          7.6535
v  Pressure                 -85648      3.3341e+05      2.0816e+05      1.7523e+05
v  k                     2.251e-06           14.63          0.1183         0.13344
v  epsilon                0.045919      4.3509e+06            4821          88.755
v  TurbVisc             4.2649e-12         0.51511       0.0048681        0.053722
v  CourantNb              0.033584           63266          51.567          8.7061
v  FourierNb              0.024988      2.3655e+05          22.035         0.36212
v  total_pressure       4.1435e+05      8.3341e+05      7.0816e+05      6.7523e+05
v  Local Time Step           0.001         0.02874       0.0010009       0.0010063


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.54549      2.4678e+05          73.602          9.0683


 TIME FOR THE TIME STEP              777:        0.78723E+02

===============================================================


 INSTANT    0.778000000E+01   TIME STEP NUMBER             778
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.446642495E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328430894E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12633E+03 0.10560E+02
   Friction velocity        uet   :  0.22526E-01 0.30827E+02
   Friction velocity        uk    :  0.50966E-01 0.30827E+02
   Dimensionless distance   yplus :  0.17088E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15511
   Nb of faces within the viscous sub-layer     :       9164
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16796E+02      71   0.10697E+00   0.72931E+02 0.33556E+02 
c  Velocity[X]                                      0.11014E+02 
c  Velocity[Y]                                      0.30924E+02 
c  Velocity[Z]                                      0.30993E+02 
c  Pressure     0.13997E+00     482   0.37023E-01   0.98700E-01 0.10862E+01 
c  k            0.92186E+00      26   0.37399E-03   0.11223E+00 0.39949E+02 
c  epsilon      0.87283E+04      14   0.20141E-03   0.57552E+07 0.52299E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022064                             3
a  epsilon                 -4.5234                             2
a  Local Time Step      1.6425e-08                        281450


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.797          18.346          2.2366         0.36581
v  Velocity[Y]             -33.916           46.27          1.2991         0.88709
v  Velocity[Z]             -58.234          34.758         -1.0778      -0.0086412
v  ǁVelocityǁ             0.018081          61.647          7.6015          7.6546
v  Pressure                 -85284      3.3342e+05      2.0811e+05      1.7523e+05
v  k                    2.0437e-06          14.079          0.1178         0.13356
v  epsilon                0.037182      4.3982e+06          4825.1           88.79
v  TurbVisc             4.2481e-12         0.51511       0.0048533         0.05378
v  CourantNb               0.12908           60884          51.553          8.7072
v  FourierNb              0.024924      2.3655e+05          22.028         0.36221
v  total_pressure       4.1472e+05      8.3342e+05      7.0811e+05      6.7523e+05
v  Local Time Step           0.001        0.028646       0.0010009       0.0010063


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85331      2.4572e+05          73.581          9.0694


 TIME FOR THE TIME STEP              778:        0.81593E+02

===============================================================


 INSTANT    0.779000000E+01   TIME STEP NUMBER             779
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.784739058E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328444350E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10784E+03 0.11802E+02
   Friction velocity        uet   :  0.84271E-02 0.28116E+02
   Friction velocity        uk    :  0.41303E-01 0.28116E+02
   Dimensionless distance   yplus :  0.23031E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15524
   Nb of faces within the viscous sub-layer     :       9153
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16797E+02      62   0.10799E+00   0.74324E+02 0.33824E+02 
c  Velocity[X]                                      0.11005E+02 
c  Velocity[Y]                                      0.31127E+02 
c  Velocity[Z]                                      0.32192E+02 
c  Pressure     0.14069E+00     643   0.36873E-01   0.99282E-01 0.12827E+01 
c  k            0.92883E+00      24   0.59756E-03   0.15920E+00 0.46097E+02 
c  epsilon      0.87683E+04      14   0.24758E-03   0.87056E+07 0.63179E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010901                             5
a  epsilon                 -26.747                             6
a  Local Time Step       1.613e-08                        281449


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7715          18.808          2.2357         0.36572
v  Velocity[Y]             -35.561          47.247          1.3087         0.88689
v  Velocity[Z]             -67.799          45.328         -1.0785      -0.0084626
v  ǁVelocityǁ             0.015338          73.509          7.6093          7.6573
v  Pressure                 -85322      3.3322e+05      2.0788e+05      1.7507e+05
v  k                    2.3393e-06           14.05         0.11745         0.13364
v  epsilon                0.046487      4.4359e+06          4818.8          88.897
v  TurbVisc             4.5839e-12         0.51511       0.0048379        0.053821
v  CourantNb              0.067883           61995          51.545          8.7075
v  FourierNb              0.024863      2.3655e+05          22.024         0.36217
v  total_pressure       4.1468e+05      8.3322e+05      7.0788e+05      6.7507e+05
v  Local Time Step           0.001        0.030056       0.0010009       0.0010063


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65328      2.4718e+05          73.569          9.0697


 TIME FOR THE TIME STEP              779:        0.91944E+02

===============================================================


 INSTANT    0.780000000E+01   TIME STEP NUMBER             780
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.694967364E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328396930E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13351E+03 0.13150E+02
   Friction velocity        uet   :  0.21814E-01 0.25954E+02
   Friction velocity        uk    :  0.38892E-01 0.25954E+02
   Dimensionless distance   yplus :  0.27877E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15557
   Nb of faces within the viscous sub-layer     :       9111
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16800E+02      61   0.10818E+00   0.74250E+02 0.33854E+02 
c  Velocity[X]                                      0.11168E+02 
c  Velocity[Y]                                      0.30426E+02 
c  Velocity[Z]                                      0.32656E+02 
c  Pressure     0.13884E+00     399   0.36920E-01   0.97934E-01 0.11108E+01 
c  k            0.94163E+00      25   0.78276E-03   0.18105E+00 0.48912E+02 
c  epsilon      0.89580E+04      19   0.57736E-03   0.61147E+08 0.16584E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.000227                             2
a  epsilon                 -4.8317                             2
a  Local Time Step       1.575e-08                        281458


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6736          18.435          2.2326         0.36571
v  Velocity[Y]             -40.193           32.97          1.3199         0.88629
v  Velocity[Z]             -57.745          35.013         -1.0875      -0.0083393
v  ǁVelocityǁ             0.021197          61.258          7.6215           7.659
v  Pressure                 -85151      3.3327e+05      2.0784e+05      1.7508e+05
v  k                    2.6518e-06          17.352         0.11775         0.13362
v  epsilon                0.046665      4.4886e+06          4893.3           89.16
v  TurbVisc              4.303e-12         0.51511       0.0048312        0.053855
v  CourantNb              0.020306           63491          51.586          8.7119
v  FourierNb              0.024808      2.3655e+05          22.022         0.36229
v  total_pressure       4.1485e+05      8.3327e+05      7.0784e+05      6.7508e+05
v  Local Time Step           0.001        0.033062       0.0010009       0.0010065


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.84619      2.4522e+05          73.608          9.0742


 TIME FOR THE TIME STEP              780:        0.80498E+02

===============================================================


 INSTANT    0.781000000E+01   TIME STEP NUMBER             781
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.454196811E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328389717E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98275E+02 0.12819E+02
   Friction velocity        uet   :  0.34239E-01 0.22155E+02
   Friction velocity        uk    :  0.46953E-01 0.22155E+02
   Dimensionless distance   yplus :  0.23050E-02 0.26216E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15588
   Nb of faces within the viscous sub-layer     :       9107
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16792E+02      61   0.10802E+00   0.75887E+02 0.34172E+02 
c  Velocity[X]                                      0.11185E+02 
c  Velocity[Y]                                      0.31744E+02 
c  Velocity[Z]                                      0.32958E+02 
c  Pressure     0.14286E+00     380   0.38443E-01   0.10094E+00 0.11627E+01 
c  k            0.94850E+00      25   0.37214E-03   0.13947E+00 0.45670E+02 
c  epsilon      0.90062E+04      14   0.34613E-03   0.58847E+08 0.16441E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013939                            20
a  epsilon                  -14.18                            15
a  Local Time Step      1.5878e-08                        281469


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.8017          18.596          2.2281         0.36547
v  Velocity[Y]             -38.379          36.867          1.3363         0.88586
v  Velocity[Z]             -67.477          40.907         -1.0987       -0.007885
v  ǁVelocityǁ             0.010763          73.189          7.6407          7.6593
v  Pressure                 -85177      3.3329e+05      2.0781e+05      1.7506e+05
v  k                    9.3488e-08          18.407         0.11772         0.13351
v  epsilon                0.019761      4.4901e+06          4867.7          89.247
v  TurbVisc             4.5003e-12         0.51511       0.0048301        0.053874
v  CourantNb            0.00052068           62980          51.712          8.7162
v  FourierNb              0.024763      2.3655e+05          22.021         0.36229
v  total_pressure       4.1482e+05      8.3329e+05      7.0781e+05      6.7506e+05
v  Local Time Step           0.001        0.021953       0.0010008        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71742      2.4585e+05          73.732          9.0785


 TIME FOR THE TIME STEP              781:        0.74751E+02

===============================================================


 INSTANT    0.782000000E+01   TIME STEP NUMBER             782
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.592375813E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328286471E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13263E+03 0.11508E+02
   Friction velocity        uet   :  0.32370E-01 0.19821E+02
   Friction velocity        uk    :  0.47617E-01 0.19821E+02
   Dimensionless distance   yplus :  0.17891E-02 0.27008E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15631
   Nb of faces within the viscous sub-layer     :       9080
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16793E+02      73   0.10537E+00   0.82994E+02 0.35761E+02 
c  Velocity[X]                                      0.11845E+02 
c  Velocity[Y]                                      0.36347E+02 
c  Velocity[Z]                                      0.34802E+02 
c  Pressure     0.15281E+00     352   0.40983E-01   0.10822E+00 0.12327E+01 
c  k            0.93843E+00      28   0.85012E-03   0.19733E+00 0.52463E+02 
c  epsilon      0.91258E+04      19   0.51206E-03   0.60520E+08 0.16445E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002273                             3
a  epsilon                 -4.9184                             2
a  Local Time Step      1.5849e-08                        281470


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6994          18.379          2.2253         0.36554
v  Velocity[Y]             -34.249          37.634          1.3516         0.88547
v  Velocity[Z]             -56.681          34.724         -1.1011      -0.0066185
v  ǁVelocityǁ             0.011204          59.998          7.6515          7.6593
v  Pressure                 -85160       3.333e+05       2.078e+05      1.7505e+05
v  k                     3.713e-07          15.163         0.11837         0.13321
v  epsilon               0.0011196      4.5663e+06          4938.3          89.123
v  TurbVisc              4.353e-12         0.51511       0.0048448         0.05388
v  CourantNb              0.012108           63096           51.97          8.7187
v  FourierNb              0.024727      2.3655e+05          22.024         0.36214
v  total_pressure       4.1484e+05       8.333e+05       7.078e+05      6.7505e+05
v  Local Time Step           0.001        0.024149       0.0010008        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66407      2.4814e+05          73.994          9.0809


 TIME FOR THE TIME STEP              782:        0.76003E+02

===============================================================


 INSTANT    0.783000000E+01   TIME STEP NUMBER             783
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.895615518E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328171969E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10116E+03 0.10636E+02
   Friction velocity        uet   :  0.25495E-01 0.19916E+02
   Friction velocity        uk    :  0.40576E-01 0.19916E+02
   Dimensionless distance   yplus :  0.21228E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15680
   Nb of faces within the viscous sub-layer     :       9082
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16793E+02      61   0.10884E+00   0.82811E+02 0.35704E+02 
c  Velocity[X]                                      0.12270E+02 
c  Velocity[Y]                                      0.35471E+02 
c  Velocity[Z]                                      0.35069E+02 
c  Pressure     0.15915E+00     318   0.43314E-01   0.11306E+00 0.13831E+01 
c  k            0.92148E+00      26   0.72732E-03   0.29752E+00 0.69519E+02 
c  epsilon      0.90127E+04      15   0.38718E-03   0.63841E+08 0.17268E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00013733                             3
a  epsilon                 -4.0811                             4
a  Local Time Step      1.5532e-08                        281456


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7593          18.665          2.2249         0.36592
v  Velocity[Y]             -35.708           34.49          1.3564         0.88511
v  Velocity[Z]             -68.496           45.37         -1.0977      -0.0050427
v  ǁVelocityǁ             0.018144          74.386          7.6555          7.6593
v  Pressure                 -85403      3.3331e+05      2.0779e+05      1.7503e+05
v  k                    2.3163e-06          14.827         0.11838         0.13284
v  epsilon                0.046898      4.5573e+06          4878.2          88.652
v  TurbVisc             4.4659e-12         0.51511        0.004871        0.053864
v  CourantNb              0.065127           64385          52.085          8.7225
v  FourierNb              0.024703      2.3655e+05          22.031         0.36204
v  total_pressure        4.146e+05      8.3331e+05      7.0779e+05      6.7503e+05
v  Local Time Step           0.001        0.026564       0.0010009       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66676      2.4734e+05          74.116          9.0845


 TIME FOR THE TIME STEP              783:        0.69739E+02

===============================================================


 INSTANT    0.784000000E+01   TIME STEP NUMBER             784
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.857485292E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327986881E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13616E+03 0.95404E+01
   Friction velocity        uet   :  0.20810E-01 0.20409E+02
   Friction velocity        uk    :  0.48864E-01 0.20409E+02
   Dimensionless distance   yplus :  0.26042E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15705
   Nb of faces within the viscous sub-layer     :       9088
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16797E+02      58   0.10813E+00   0.82552E+02 0.35675E+02 
c  Velocity[X]                                      0.13180E+02 
c  Velocity[Y]                                      0.34450E+02 
c  Velocity[Z]                                      0.34921E+02 
c  Pressure     0.15728E+00     452   0.43657E-01   0.11180E+00 0.13902E+01 
c  k            0.90789E+00      28   0.43627E-03   0.17335E+00 0.54017E+02 
c  epsilon      0.89883E+04      18   0.55714E-03   0.65377E+08 0.17300E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021586                             3
a  epsilon                 -3.7658                             2
a  Local Time Step      1.5805e-08                        281463


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7674          18.205          2.2215         0.36591
v  Velocity[Y]              -39.32          35.986          1.3593         0.88531
v  Velocity[Z]             -58.759          35.395         -1.0898       -0.003667
v  ǁVelocityǁ            0.0067773          62.059          7.6522          7.6598
v  Pressure                 -85402      3.3333e+05      2.0785e+05      1.7511e+05
v  k                    1.6472e-06          14.822         0.11901         0.13237
v  epsilon                0.046922       4.545e+06          4936.1          88.259
v  TurbVisc             5.1565e-12         0.51511       0.0049098        0.053838
v  CourantNb              0.012654           63273          52.089          8.7252
v  FourierNb              0.024692      2.3655e+05          22.038         0.36203
v  total_pressure        4.146e+05      8.3333e+05      7.0785e+05      6.7511e+05
v  Local Time Step           0.001        0.022915       0.0010008       0.0010059


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76513      2.4845e+05          74.127          9.0872


 TIME FOR THE TIME STEP              784:        0.87715E+02

===============================================================


 INSTANT    0.785000000E+01   TIME STEP NUMBER             785
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.343866614E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327852460E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10948E+03 0.87198E+01
   Friction velocity        uet   :  0.22490E-01 0.17278E+02
   Friction velocity        uk    :  0.29067E-01 0.17278E+02
   Dimensionless distance   yplus :  0.19569E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15707
   Nb of faces within the viscous sub-layer     :       9085
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16793E+02      57   0.10697E+00   0.85173E+02 0.36196E+02 
c  Velocity[X]                                      0.13886E+02 
c  Velocity[Y]                                      0.36898E+02 
c  Velocity[Z]                                      0.34390E+02 
c  Pressure     0.15755E+00     470   0.44387E-01   0.11200E+00 0.13951E+01 
c  k            0.90187E+00      28   0.26462E-03   0.11703E+00 0.44551E+02 
c  epsilon      0.88435E+04      18   0.27986E-03   0.59306E+08 0.16842E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010885                             4
a  epsilon                 -83.307                             4
a  Local Time Step      1.5565e-08                        281462


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.791          18.575          2.2178         0.36597
v  Velocity[Y]             -39.433          35.072          1.3538         0.88514
v  Velocity[Z]             -69.564          42.123          -1.081      -0.0028931
v  ǁVelocityǁ             0.010034          75.536          7.6462          7.6599
v  Pressure                 -85299      3.3339e+05       2.079e+05      1.7516e+05
v  k                    1.7813e-06          13.873          0.1189         0.13185
v  epsilon                0.046482      4.4691e+06          4847.7          87.648
v  TurbVisc             3.6596e-12         0.51511       0.0049485        0.053793
v  CourantNb              0.023717           64249          51.999          8.7265
v  FourierNb              0.024693      2.3655e+05          22.045         0.36201
v  total_pressure        4.147e+05      8.3339e+05       7.079e+05      6.7516e+05
v  Local Time Step           0.001        0.020778       0.0010008       0.0010059


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.62191      2.4734e+05          74.044          9.0885


 TIME FOR THE TIME STEP              785:        0.77545E+02

===============================================================


 INSTANT    0.786000000E+01   TIME STEP NUMBER             786
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.756588872E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327731440E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+03 0.95899E+01
   Friction velocity        uet   :  0.36665E-01 0.21325E+02
   Friction velocity        uk    :  0.39523E-01 0.21325E+02
   Dimensionless distance   yplus :  0.27210E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15705
   Nb of faces within the viscous sub-layer     :       9085
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16795E+02      59   0.11033E+00   0.85524E+02 0.36318E+02 
c  Velocity[X]                                      0.14177E+02 
c  Velocity[Y]                                      0.37170E+02 
c  Velocity[Z]                                      0.34177E+02 
c  Pressure     0.15577E+00     559   0.43767E-01   0.11082E+00 0.15834E+01 
c  k            0.90173E+00      30   0.24330E-03   0.10162E+00 0.41227E+02 
c  epsilon      0.87631E+04      16   0.22210E-03   0.78546E+07 0.61491E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014319                             5
a  epsilon                 -39.961                             5
a  Local Time Step      1.5949e-08                        281470


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.8396          18.044          2.2141         0.36598
v  Velocity[Y]             -35.732          36.198          1.3482         0.88517
v  Velocity[Z]             -57.366          35.764         -1.0684      -0.0026339
v  ǁVelocityǁ            0.0098581          60.701          7.6326          7.6603
v  Pressure                 -84761      3.3347e+05      2.0797e+05       1.753e+05
v  k                    2.3871e-06          13.396         0.11915         0.13134
v  epsilon                0.045931      4.3716e+06          4839.1          87.214
v  TurbVisc             3.5825e-12         0.51511       0.0049893        0.053738
v  CourantNb              0.015827           62700          51.869          8.7271
v  FourierNb              0.024705      2.3655e+05          22.055           0.362
v  total_pressure       4.1524e+05      8.3347e+05      7.0797e+05       6.753e+05
v  Local Time Step           0.001        0.022856       0.0010008        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.46095      2.4759e+05          73.924          9.0891


 TIME FOR THE TIME STEP              786:        0.82492E+02

===============================================================


 INSTANT    0.787000000E+01   TIME STEP NUMBER             787
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.844653518E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327749138E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10528E+03 0.10927E+02
   Friction velocity        uet   :  0.39633E-01 0.15295E+02
   Friction velocity        uk    :  0.41610E-01 0.15295E+02
   Dimensionless distance   yplus :  0.19516E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15680
   Nb of faces within the viscous sub-layer     :       9119
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16799E+02      56   0.10963E+00   0.86752E+02 0.36597E+02 
c  Velocity[X]                                      0.14733E+02 
c  Velocity[Y]                                      0.38444E+02 
c  Velocity[Z]                                      0.33575E+02 
c  Pressure     0.15943E+00     627   0.44473E-01   0.11348E+00 0.17597E+01 
c  k            0.90532E+00      32   0.28484E-03   0.97364E-01 0.39982E+02 
c  epsilon      0.86853E+04      14   0.20090E-03   0.77547E+07 0.61242E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023033                             4
a  epsilon                 -5.3726                             3
a  Local Time Step      1.5638e-08                        281454


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.8459          18.553          2.2134         0.36591
v  Velocity[Y]             -36.095          34.852          1.3389         0.88501
v  Velocity[Z]             -66.881          41.658         -1.0535      -0.0035648
v  ǁVelocityǁ            0.0094644          72.625          7.6206          7.6602
v  Pressure                 -84139      3.3353e+05      2.0804e+05      1.7545e+05
v  k                    2.0387e-06           13.68         0.11874         0.13088
v  epsilon                0.045327      4.2973e+06          4797.2          86.814
v  TurbVisc             4.2458e-12         0.51511       0.0050147        0.053673
v  CourantNb             0.0069359           63948          51.679          8.7256
v  FourierNb               0.02473      2.3655e+05          22.064          0.3618
v  total_pressure       4.1586e+05      8.3353e+05      7.0804e+05      6.7545e+05
v  Local Time Step           0.001        0.024801       0.0010008       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91372      2.4804e+05          73.743          9.0874


 TIME FOR THE TIME STEP              787:        0.93225E+02

===============================================================


 INSTANT    0.788000000E+01   TIME STEP NUMBER             788
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.174829220E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327857024E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13059E+03 0.12189E+02
   Friction velocity        uet   :  0.33454E-01 0.17958E+02
   Friction velocity        uk    :  0.63364E-01 0.17958E+02
   Dimensionless distance   yplus :  0.13665E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15686
   Nb of faces within the viscous sub-layer     :       9147
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16795E+02      61   0.10548E+00   0.84076E+02 0.36035E+02 
c  Velocity[X]                                      0.14703E+02 
c  Velocity[Y]                                      0.36745E+02 
c  Velocity[Z]                                      0.32628E+02 
c  Pressure     0.15812E+00     420   0.44068E-01   0.11261E+00 0.16119E+01 
c  k            0.91288E+00      28   0.55625E-03   0.13188E+00 0.44123E+02 
c  epsilon      0.85967E+04      16   0.28194E-03   0.18465E+08 0.94703E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00032531                             7
a  epsilon                  -2.581                             2
a  Local Time Step      1.5513e-08                        281468


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7803          18.056          2.2165          0.3663
v  Velocity[Y]             -38.989          36.733          1.3306         0.88625
v  Velocity[Z]             -58.197          35.466         -1.0415      -0.0048655
v  ǁVelocityǁ             0.014293          61.818          7.6079          7.6597
v  Pressure                 -83385      3.3348e+05      2.0802e+05      1.7553e+05
v  k                    1.7633e-06          13.851         0.11813         0.13048
v  epsilon                0.044826      4.1727e+06          4725.5          86.588
v  TurbVisc             4.4227e-12         0.51511       0.0050164        0.053605
v  CourantNb              0.050782           64462           51.54          8.7228
v  FourierNb              0.024764      2.3655e+05          22.068         0.36154
v  total_pressure       4.1661e+05      8.3348e+05      7.0802e+05      6.7553e+05
v  Local Time Step           0.001        0.021535       0.0010008        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6917      2.4928e+05          73.608          9.0843


 TIME FOR THE TIME STEP              788:        0.84292E+02

===============================================================


 INSTANT    0.789000000E+01   TIME STEP NUMBER             789
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.955493252E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328040150E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10033E+03 0.12283E+02
   Friction velocity        uet   :  0.24308E-01 0.22204E+02
   Friction velocity        uk    :  0.32884E-01 0.22204E+02
   Dimensionless distance   yplus :  0.28333E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15663
   Nb of faces within the viscous sub-layer     :       9181
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16810E+02      56   0.10707E+00   0.81165E+02 0.35319E+02 
c  Velocity[X]                                      0.14060E+02 
c  Velocity[Y]                                      0.35159E+02 
c  Velocity[Z]                                      0.31946E+02 
c  Pressure     0.15542E+00     425   0.43327E-01   0.11095E+00 0.16672E+01 
c  k            0.92299E+00      29   0.49498E-03   0.11033E+00 0.41798E+02 
c  epsilon      0.84546E+04      14   0.39205E-03   0.44687E+08 0.15033E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0001826                             3
a  epsilon                 -3.1781                             2
a  Local Time Step       1.502e-08                        281462


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.754          18.265          2.2201         0.36586
v  Velocity[Y]             -39.087          35.624          1.3222         0.88681
v  Velocity[Z]             -67.533          46.279         -1.0291       -0.006911
v  ǁVelocityǁ             0.017867          73.248          7.5977            7.66
v  Pressure                 -82756      3.3343e+05      2.0796e+05      1.7559e+05
v  k                    2.4646e-06          15.623         0.11737          0.1301
v  epsilon                0.044512      4.0904e+06          4636.4          86.376
v  TurbVisc             3.4816e-12         0.51511       0.0049957        0.053537
v  CourantNb              0.083328           66577          51.461          8.7213
v  FourierNb              0.024806      2.3654e+05          22.071         0.36133
v  total_pressure       4.1724e+05      8.3343e+05      7.0796e+05      6.7559e+05
v  Local Time Step           0.001        0.020422       0.0010008        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.65781      2.4942e+05          73.532          9.0826


 TIME FOR THE TIME STEP              789:        0.76565E+02

===============================================================


 INSTANT    0.790000000E+01   TIME STEP NUMBER             790
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.122483794E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328306014E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13264E+03 0.12530E+02
   Friction velocity        uet   :  0.17291E-01 0.15761E+02
   Friction velocity        uk    :  0.36824E-01 0.15761E+02
   Dimensionless distance   yplus :  0.14426E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15635
   Nb of faces within the viscous sub-layer     :       9200
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16821E+02      56   0.10739E+00   0.76786E+02 0.34406E+02 
c  Velocity[X]                                      0.12932E+02 
c  Velocity[Y]                                      0.30725E+02 
c  Velocity[Z]                                      0.33129E+02 
c  Pressure     0.15291E+00     521   0.41954E-01   0.10912E+00 0.14178E+01 
c  k            0.93075E+00      25   0.22754E-03   0.13741E+00 0.47269E+02 
c  epsilon      0.83735E+04      20   0.74113E-03   0.31722E+08 0.12758E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019731                             3
a  epsilon                 -3.5711                             2
a  Local Time Step       1.512e-08                        281447


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7877           18.23          2.2217         0.36566
v  Velocity[Y]             -36.215           39.67          1.3151         0.88729
v  Velocity[Z]             -53.682          35.821         -1.0192      -0.0097411
v  ǁVelocityǁ              0.01478          57.011          7.5924          7.6614
v  Pressure                 -82141       3.334e+05       2.079e+05       1.756e+05
v  k                    2.4152e-06          15.957         0.11688         0.12978
v  epsilon                0.044243       3.195e+06          4614.2          86.237
v  TurbVisc             4.1826e-12         0.51511       0.0049631        0.053468
v  CourantNb               0.15952           66137          51.328          8.7195
v  FourierNb              0.024852      2.3655e+05          22.067         0.36095
v  total_pressure       4.1786e+05       8.334e+05       7.079e+05       6.756e+05
v  Local Time Step           0.001        0.017442       0.0010008        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82689      2.4228e+05          73.395          9.0804


 TIME FOR THE TIME STEP              790:        0.80311E+02

===============================================================


 INSTANT    0.791000000E+01   TIME STEP NUMBER             791
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.682056534E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328628470E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.94062E+02 0.11670E+02
   Friction velocity        uet   :  0.26194E-01 0.18733E+02
   Friction velocity        uk    :  0.39707E-01 0.18733E+02
   Dimensionless distance   yplus :  0.20982E-02 0.25121E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15639
   Nb of faces within the viscous sub-layer     :       9198
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16828E+02      61   0.10554E+00   0.72666E+02 0.33418E+02 
c  Velocity[X]                                      0.11521E+02 
c  Velocity[Y]                                      0.27165E+02 
c  Velocity[Z]                                      0.33981E+02 
c  Pressure     0.14913E+00    1081   0.40714E-01   0.10652E+00 0.89392E+01 
c  k            0.93302E+00      24   0.51703E-03   0.32819E+00 0.73933E+02 
c  epsilon      0.83570E+04      13   0.22967E-03   0.66518E+07 0.58695E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00036977                             9
a  epsilon                 -7.5808                             9
a  Local Time Step      1.4952e-08                        281444


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7126          18.512           2.225         0.36527
v  Velocity[Y]             -37.874          38.901          1.3018         0.88709
v  Velocity[Z]             -69.088          42.904         -1.0096      -0.0078251
v  ǁVelocityǁ             0.016135          74.918          7.5879          7.6588
v  Pressure                 -83681      3.3103e+05      2.0554e+05      1.7372e+05
v  k                    2.8557e-06          15.391         0.11642          0.1295
v  epsilon               0.0031791      3.0955e+06            4608          86.117
v  TurbVisc              5.059e-12         0.51511       0.0049295        0.053404
v  CourantNb              0.040377           66881          51.335          8.7193
v  FourierNb                0.0249      2.3655e+05          22.063         0.36064
v  total_pressure       4.1632e+05      8.3103e+05      7.0554e+05      6.7372e+05
v  Local Time Step           0.001        0.019186       0.0010009       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87472      2.4801e+05          73.398          9.0799


 TIME FOR THE TIME STEP              791:        0.95311E+02

===============================================================


 INSTANT    0.792000000E+01   TIME STEP NUMBER             792
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.891577488E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328211398E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13833E+03 0.11137E+02
   Friction velocity        uet   :  0.32260E-02 0.23910E+02
   Friction velocity        uk    :  0.49385E-01 0.23910E+02
   Dimensionless distance   yplus :  0.30509E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15625
   Nb of faces within the viscous sub-layer     :       9194
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16821E+02      57   0.10963E+00   0.69896E+02 0.32858E+02 
c  Velocity[X]                                      0.11016E+02 
c  Velocity[Y]                                      0.25475E+02 
c  Velocity[Z]                                      0.33406E+02 
c  Pressure     0.14089E+00     954   0.37297E-01   0.10037E+00 0.19480E+01 
c  k            0.93125E+00      26   0.10845E-02   0.43256E+00 0.82951E+02 
c  epsilon      0.83223E+04      18   0.37196E-03   0.92621E+07 0.67962E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00048139                             6
a  epsilon                 -6.5916                             3
a  Local Time Step      1.4971e-08                        281442


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6781            18.2          2.2235         0.36515
v  Velocity[Y]             -37.889          43.457          1.2896         0.88726
v  Velocity[Z]             -61.741          35.749          -1.006       -0.006241
v  ǁVelocityǁ             0.016185          65.444          7.5836          7.6559
v  Pressure                 -83431      3.3073e+05      2.0519e+05      1.7346e+05
v  k                      1.85e-06           14.26         0.11576         0.12929
v  epsilon                0.035129      4.1683e+06          4605.4          85.961
v  TurbVisc             4.9264e-12         0.51511       0.0049007        0.053343
v  CourantNb             0.0077914           66797          51.283          8.7158
v  FourierNb              0.024948      2.3655e+05           22.06         0.36051
v  total_pressure       4.1657e+05      8.3073e+05      7.0519e+05      6.7346e+05
v  Local Time Step           0.001        0.019979       0.0010008       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88967      2.4571e+05          73.343          9.0763


 TIME FOR THE TIME STEP              792:        0.83066E+02

===============================================================


 INSTANT    0.793000000E+01   TIME STEP NUMBER             793
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.113139048E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328173700E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10884E+03 0.11002E+02
   Friction velocity        uet   :  0.32071E-01 0.23832E+02
   Friction velocity        uk    :  0.58605E-01 0.23832E+02
   Dimensionless distance   yplus :  0.30409E-02 0.25113E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15592
   Nb of faces within the viscous sub-layer     :       9197
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16807E+02      57   0.10923E+00   0.68009E+02 0.32328E+02 
c  Velocity[X]                                      0.10411E+02 
c  Velocity[Y]                                      0.25482E+02 
c  Velocity[Z]                                      0.32116E+02 
c  Pressure     0.13405E+00     444   0.35265E-01   0.95485E-01 0.12916E+01 
c  k            0.92923E+00      24   0.59182E-03   0.26128E+00 0.65536E+02 
c  epsilon      0.82767E+04      14   0.35978E-03   0.81825E+07 0.65306E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028501                             4
a  epsilon                 -2.9431                             3
a  Local Time Step      1.5153e-08                        281433


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.6691          18.441          2.2224          0.3648
v  Velocity[Y]             -40.088          37.363           1.283         0.88758
v  Velocity[Z]             -68.879          40.593         -1.0093      -0.0053641
v  ǁVelocityǁ            0.0062444          74.772           7.589          7.6537
v  Pressure                 -90086       3.308e+05      2.0521e+05      1.7346e+05
v  k                    2.3311e-06          14.262         0.11527         0.12909
v  epsilon                0.036829      3.7974e+06            4606          85.814
v  TurbVisc             3.9627e-12         0.51511       0.0048597        0.053287
v  CourantNb              0.080608           65992          51.248          8.7153
v  FourierNb               0.02499      2.3655e+05          22.054         0.36019
v  total_pressure       4.0991e+05       8.308e+05      7.0521e+05      6.7346e+05
v  Local Time Step           0.001        0.015231       0.0010008       0.0010059


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64896      2.4403e+05          73.302          9.0755


 TIME FOR THE TIME STEP              793:        0.48091E+02

===============================================================


 INSTANT    0.794000000E+01   TIME STEP NUMBER             794
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.773761539E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328162452E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13849E+03 0.11075E+02
   Friction velocity        uet   :  0.31829E-01 0.23770E+02
   Friction velocity        uk    :  0.43602E-01 0.23770E+02
   Dimensionless distance   yplus :  0.17206E-02 0.25216E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15579
   Nb of faces within the viscous sub-layer     :       9187
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16804E+02      61   0.11029E+00   0.66517E+02 0.32046E+02 
c  Velocity[X]                                      0.10377E+02 
c  Velocity[Y]                                      0.24994E+02 
c  Velocity[Z]                                      0.31146E+02 
c  Pressure     0.12724E+00     434   0.33701E-01   0.90568E-01 0.12249E+01 
c  k            0.92243E+00      22   0.78792E-03   0.26322E+00 0.65858E+02 
c  epsilon      0.82650E+04      16   0.27027E-03   0.54326E+07 0.53189E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014296                             3
a  epsilon                 -3.2223                             3
a  Local Time Step      1.5158e-08                        281421


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.5628          18.435          2.2208         0.36471
v  Velocity[Y]             -38.857          45.149          1.2795         0.88778
v  Velocity[Z]             -57.935          35.652         -1.0193      -0.0046208
v  ǁVelocityǁ             0.012536          61.512          7.5932          7.6523
v  Pressure                 -95527       3.309e+05      2.0524e+05      1.7347e+05
v  k                     2.337e-06          13.939         0.11481         0.12885
v  epsilon                0.042687      3.9588e+06          4608.6          85.507
v  TurbVisc             4.4335e-12         0.51511       0.0048147        0.053237
v  CourantNb                     0           65971          51.333          8.7157
v  FourierNb              0.025026      2.3655e+05          22.048         0.35996
v  total_pressure       4.0447e+05       8.309e+05      7.0524e+05      6.7347e+05
v  Local Time Step           0.001        0.016754       0.0010009        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43529      2.4891e+05           73.38          9.0756


 TIME FOR THE TIME STEP              794:        0.62844E+02

===============================================================


 INSTANT    0.795000000E+01   TIME STEP NUMBER             795
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.144707828E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328127979E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99213E+02 0.11854E+02
   Friction velocity        uet   :  0.24151E-01 0.22985E+02
   Friction velocity        uk    :  0.45134E-01 0.22985E+02
   Dimensionless distance   yplus :  0.20292E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15569
   Nb of faces within the viscous sub-layer     :       9179
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16802E+02      58   0.10782E+00   0.67826E+02 0.32305E+02 
c  Velocity[X]                                      0.10459E+02 
c  Velocity[Y]                                      0.26900E+02 
c  Velocity[Z]                                      0.30467E+02 
c  Pressure     0.13083E+00     458   0.34296E-01   0.93039E-01 0.11300E+01 
c  k            0.91718E+00      21   0.66789E-03   0.24902E+00 0.64178E+02 
c  epsilon      0.82525E+04      15   0.29277E-03   0.13514E+08 0.84146E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020493                             3
a  epsilon                 -4.3663                             2
a  Local Time Step      1.4979e-08                        281423


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -10.935          18.712          2.2197         0.36461
v  Velocity[Y]              -39.12          37.506          1.2772         0.88772
v  Velocity[Z]             -69.724           43.29         -1.0292      -0.0040706
v  ǁVelocityǁ             0.017708          75.758             7.6          7.6504
v  Pressure                 -99814      3.3102e+05      2.0529e+05      1.7346e+05
v  k                    2.3541e-06           14.23         0.11439         0.12859
v  epsilon                0.042586      3.0832e+06            4613          85.176
v  TurbVisc             3.9517e-12         0.51511       0.0047738        0.053189
v  CourantNb             0.0050899           66760          51.404          8.7152
v  FourierNb              0.025053      2.3655e+05          22.039         0.35975
v  total_pressure       4.0019e+05      8.3102e+05      7.0529e+05      6.7346e+05
v  Local Time Step           0.001        0.018429       0.0010009       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42572      2.4814e+05          73.444           9.075


 TIME FOR THE TIME STEP              795:        0.38711E+02

===============================================================


 INSTANT    0.796000000E+01   TIME STEP NUMBER             796
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.158009434E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327994330E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14134E+03 0.11181E+02
   Friction velocity        uet   :  0.16745E-01 0.20212E+02
   Friction velocity        uk    :  0.16749E-01 0.20212E+02
   Dimensionless distance   yplus :  0.22197E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15563
   Nb of faces within the viscous sub-layer     :       9176
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16797E+02      56   0.10719E+00   0.64997E+02 0.31687E+02 
c  Velocity[X]                                      0.10544E+02 
c  Velocity[Y]                                      0.24523E+02 
c  Velocity[Z]                                      0.29930E+02 
c  Pressure     0.12808E+00     459   0.33371E-01   0.90939E-01 0.10722E+01 
c  k            0.91444E+00      22   0.57613E-03   0.24527E+00 0.63619E+02 
c  epsilon      0.82659E+04      14   0.36155E-03   0.10504E+08 0.73970E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00014859                             3
a  epsilon                 -1.6524                             2
a  Local Time Step      1.4862e-08                        281424


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -8.915          18.108          2.2194         0.36502
v  Velocity[Y]             -34.108          47.971          1.2775         0.88757
v  Velocity[Z]             -52.777           36.14         -1.0391      -0.0034874
v  ǁVelocityǁ             0.012657          56.037          7.6035          7.6501
v  Pressure            -1.0284e+05       3.311e+05      2.0533e+05       1.735e+05
v  k                     2.323e-06          14.333         0.11406         0.12833
v  epsilon                0.042622      3.1014e+06          4628.4          84.845
v  TurbVisc             4.2749e-12         0.51511       0.0047376        0.053144
v  CourantNb              0.054662           67284           51.44          8.7138
v  FourierNb              0.025071      2.3655e+05          22.033         0.35973
v  total_pressure       3.9716e+05       8.311e+05      7.0533e+05       6.735e+05
v  Local Time Step           0.001        0.017985       0.0010009       0.0010062


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5343      2.4779e+05          73.472          9.0736


 TIME FOR THE TIME STEP              796:        0.38295E+02

===============================================================


 INSTANT    0.797000000E+01   TIME STEP NUMBER             797
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.839274787E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327950738E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88800E+02 0.10922E+02
   Friction velocity        uet   :  0.31949E-01 0.17276E+02
   Friction velocity        uk    :  0.55617E-01 0.17276E+02
   Dimensionless distance   yplus :  0.13861E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15549
   Nb of faces within the viscous sub-layer     :       9169
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16801E+02      58   0.11010E+00   0.63652E+02 0.31289E+02 
c  Velocity[X]                                      0.10407E+02 
c  Velocity[Y]                                      0.23647E+02 
c  Velocity[Z]                                      0.29599E+02 
c  Pressure     0.12687E+00     524   0.32839E-01   0.90024E-01 0.10347E+01 
c  k            0.91509E+00      22   0.36068E-03   0.14527E+00 0.48753E+02 
c  epsilon      0.82067E+04      13   0.23637E-03   0.20287E+08 0.10331E+03 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017764                             3
a  epsilon                 -2.6047                             2
a  Local Time Step      1.4905e-08                        281421


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7353          18.764          2.2207         0.36557
v  Velocity[Y]             -39.227          41.248          1.2806         0.88702
v  Velocity[Z]             -68.604          42.182         -1.0498      -0.0029193
v  ǁVelocityǁ             0.015295          74.625          7.6097           7.649
v  Pressure            -1.0452e+05      3.3121e+05       2.054e+05      1.7352e+05
v  k                    2.3858e-06           14.98         0.11382         0.12829
v  epsilon                0.042756      3.1321e+06          4600.5          84.874
v  TurbVisc             4.2953e-12         0.51511       0.0047051        0.053101
v  CourantNb              0.066787           67091          51.453          8.7138
v  FourierNb              0.025079      2.3655e+05          22.026         0.35952
v  total_pressure       3.9548e+05      8.3121e+05       7.054e+05      6.7352e+05
v  Local Time Step           0.001        0.019553       0.0010009       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.68407      2.4438e+05          73.479          9.0734


 TIME FOR THE TIME STEP              797:        0.22302E+02

===============================================================


 INSTANT    0.798000000E+01   TIME STEP NUMBER             798
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.270447943E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327829687E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13756E+03 0.11713E+02
   Friction velocity        uet   :  0.32796E-01 0.24723E+02
   Friction velocity        uk    :  0.34202E-01 0.24723E+02
   Dimensionless distance   yplus :  0.12705E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15555
   Nb of faces within the viscous sub-layer     :       9151
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16801E+02      55   0.11010E+00   0.67629E+02 0.32327E+02 
c  Velocity[X]                                      0.10211E+02 
c  Velocity[Y]                                      0.24615E+02 
c  Velocity[Z]                                      0.32803E+02 
c  Pressure     0.13654E+00     428   0.34416E-01   0.96755E-01 0.99874E+00 
c  k            0.91726E+00      21   0.25762E-03   0.11341E+00 0.42869E+02 
c  epsilon      0.82278E+04      13   0.31886E-03   0.95981E+07 0.70927E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020429                             2
a  epsilon                 -3.3847                             2
a  Local Time Step      1.5016e-08                        281444


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.7737          18.069          2.2242         0.36608
v  Velocity[Y]             -37.186          46.622          1.2792         0.88698
v  Velocity[Z]             -59.155          35.876         -1.0587      -0.0023099
v  ǁVelocityǁ             0.017722          62.501          7.6108          7.6473
v  Pressure            -1.0403e+05      3.3123e+05      2.0544e+05      1.7356e+05
v  k                    2.9291e-06          15.029         0.11379         0.12834
v  epsilon                0.042982      3.1411e+06          4605.1          84.957
v  TurbVisc             4.5823e-12         0.51511       0.0046774        0.053076
v  CourantNb              0.011649           66597          51.512          8.7135
v  FourierNb              0.025076      2.3655e+05          22.024         0.35948
v  total_pressure       3.9597e+05      8.3123e+05      7.0544e+05      6.7356e+05
v  Local Time Step           0.001        0.017604       0.0010009        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.66527      2.4712e+05          73.536           9.073


 TIME FOR THE TIME STEP              798:        0.20629E+02

===============================================================


 INSTANT    0.799000000E+01   TIME STEP NUMBER             799
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.112463168E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327748083E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96140E+02 0.11429E+02
   Friction velocity        uet   :  0.12184E-01 0.24542E+02
   Friction velocity        uk    :  0.25097E-01 0.24542E+02
   Dimensionless distance   yplus :  0.17200E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15551
   Nb of faces within the viscous sub-layer     :       9144
   Total number of wall faces                   :      41000
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step        799
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16794E+02      57   0.10483E+00   0.67157E+02 0.32214E+02 
c  Velocity[X]                                      0.10468E+02 
c  Velocity[Y]                                      0.24527E+02 
c  Velocity[Z]                                      0.32162E+02 
c  Pressure     0.12826E+00     790   0.33047E-01   0.90896E-01 0.34253E+01 
c  k            0.91782E+00      22   0.23610E-03   0.85125E-01 0.36816E+02 
c  epsilon      0.82338E+04      16   0.37790E-03   0.13239E+08 0.83465E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020181                             5
a  epsilon                 -8.2902                             7
a  Local Time Step      1.4951e-08                        281426


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.8762          18.603          2.2271         0.36621
v  Velocity[Y]             -39.319          45.407          1.2738         0.88769
v  Velocity[Z]             -65.764          41.651         -1.0704      -0.0037548
v  ǁVelocityǁ             0.021374          71.557          7.6127           7.648
v  Pressure            -1.0009e+05      3.3208e+05      2.0634e+05      1.7426e+05
v  k                    1.7792e-06          15.294         0.11367         0.12851
v  epsilon                0.043128       3.243e+06          4595.5          85.085
v  TurbVisc             4.2396e-12         0.51511       0.0046627        0.053062
v  CourantNb              0.016427           66885          51.541          8.7125
v  FourierNb               0.02506      2.3655e+05          22.022         0.35941
v  total_pressure       3.9991e+05      8.3208e+05      7.0634e+05      6.7426e+05
v  Local Time Step           0.001        0.019364       0.0010009       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.86088      2.4948e+05          73.563          9.0719


 TIME FOR THE TIME STEP              799:        0.24918E+02

===============================================================


 INSTANT    0.800000000E+01   TIME STEP NUMBER             800
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.711410016E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327860960E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12762E+03 0.11112E+02
   Friction velocity        uet   :  0.33467E-01 0.24996E+02
   Friction velocity        uk    :  0.40357E-01 0.24996E+02
   Dimensionless distance   yplus :  0.31678E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15556
   Nb of faces within the viscous sub-layer     :       9155
   Total number of wall faces                   :      41000
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step        800
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            



 Write final restart files
   checkpoint at iteration        800, Physical time    0.80000E+01


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint/main
 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                            
  Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary
 End writing


 Time for restart files:    0.39337E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16806E+02      56   0.10607E+00   0.66285E+02 0.31984E+02 
c  Velocity[X]                                      0.10299E+02 
c  Velocity[Y]                                      0.25874E+02 
c  Velocity[Z]                                      0.30111E+02 
c  Pressure     0.12784E+00     451   0.33761E-01   0.90544E-01 0.10918E+01 
c  k            0.91473E+00      20   0.39838E-03   0.79847E-01 0.34694E+02 
c  epsilon      0.82495E+04      13   0.23431E-03   0.58086E+07 0.54835E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017907                             4
a  epsilon                 -2.3248                             2
a  Local Time Step      1.5141e-08                        281420


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9142          17.942           2.229         0.36615
v  Velocity[Y]             -36.305          44.722          1.2698         0.88812
v  Velocity[Z]             -58.009          35.228         -1.0785      -0.0046539
v  ǁVelocityǁ            0.0085572          61.292          7.6145          7.6495
v  Pressure                 -95272      3.3204e+05      2.0638e+05      1.7427e+05
v  k                    1.9493e-06          14.551         0.11368         0.12877
v  epsilon                0.043239      3.2884e+06          4589.5           85.27
v  TurbVisc             4.0416e-12         0.51511       0.0046563        0.053066
v  CourantNb              0.078629           66047          51.603          8.7126
v  FourierNb              0.025035      2.3655e+05          22.023         0.35952
v  total_pressure       4.0473e+05      8.3204e+05      7.0638e+05      6.7427e+05
v  Local Time Step           0.001        0.017918       0.0010009        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88404      2.5214e+05          73.625          9.0721


 TIME FOR THE TIME STEP              800:        0.21163E+02

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.15970E-03
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation

t necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            



 Write final restart files
   checkpoint at iteration        800, Physical time    0.80000E+01


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint/main
 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                            
  Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary
 End writing


 Time for restart files:    0.46832E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16806E+02      56   0.10607E+00   0.66285E+02 0.31984E+02 
c  Velocity[X]                                      0.10299E+02 
c  Velocity[Y]                                      0.25874E+02 
c  Velocity[Z]                                      0.30111E+02 
c  Pressure     0.12784E+00     451   0.33761E-01   0.90544E-01 0.10918E+01 
c  k            0.91473E+00      20   0.39838E-03   0.79847E-01 0.34694E+02 
c  epsilon      0.82495E+04      13   0.23431E-03   0.58086E+07 0.54835E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017907                             4
a  epsilon                 -2.3248                             2
a  Local Time Step      1.5141e-08                        281420


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9142          17.942           2.229         0.36615
v  Velocity[Y]             -36.305          44.722          1.2698         0.88812
v  Velocity[Z]             -58.009          35.228         -1.0785      -0.0046539
v  ǁVelocityǁ            0.0085572          61.292          7.6145          7.6495
v  Pressure                 -95272      3.3204e+05      2.0638e+05      1.7427e+05
v  k                    1.9493e-06          14.551         0.11368         0.12877
v  epsilon                0.043239      3.2884e+06          4589.5           85.27
v  TurbVisc             4.0416e-12         0.51511       0.0046563        0.053066
v  CourantNb              0.078629           66047          51.603          8.7126
v  FourierNb              0.025035      2.3655e+05          22.023         0.35952
v  total_pressure       4.0473e+05      8.3204e+05      7.0638e+05      6.7427e+05
v  Local Time Step           0.001        0.017918       0.0010009        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88404      2.5214e+05          73.625          9.0721


 TIME FOR THE TIME STEP              800:        0.42678E+02

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.13780E-03
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation

-----------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.112463168E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327748083E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96140E+02 0.11429E+02
   Friction velocity        uet   :  0.12184E-01 0.24542E+02
   Friction velocity        uk    :  0.25097E-01 0.24542E+02
   Dimensionless distance   yplus :  0.17200E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15551
   Nb of faces within the viscous sub-layer     :       9144
   Total number of wall faces                   :      41000
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step        799
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16794E+02      57   0.10483E+00   0.67157E+02 0.32214E+02 
c  Velocity[X]                                      0.10468E+02 
c  Velocity[Y]                                      0.24527E+02 
c  Velocity[Z]                                      0.32162E+02 
c  Pressure     0.12826E+00     790   0.33047E-01   0.90896E-01 0.34253E+01 
c  k            0.91782E+00      22   0.23610E-03   0.85125E-01 0.36816E+02 
c  epsilon      0.82338E+04      16   0.37790E-03   0.13239E+08 0.83465E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020181                             5
a  epsilon                 -8.2902                             7
a  Local Time Step      1.4951e-08                        281426


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.8762          18.603          2.2271         0.36621
v  Velocity[Y]             -39.319          45.407          1.2738         0.88769
v  Velocity[Z]             -65.764          41.651         -1.0704      -0.0037548
v  ǁVelocityǁ             0.021374          71.557          7.6127           7.648
v  Pressure            -1.0009e+05      3.3208e+05      2.0634e+05      1.7426e+05
v  k                    1.7792e-06          15.294         0.11367         0.12851
v  epsilon                0.043128       3.243e+06          4595.5          85.085
v  TurbVisc             4.2396e-12         0.51511       0.0046627        0.053062
v  CourantNb              0.016427           66885          51.541          8.7125
v  FourierNb               0.02506      2.3655e+05          22.022         0.35941
v  total_pressure       3.9991e+05      8.3208e+05      7.0634e+05      6.7426e+05
v  Local Time Step           0.001        0.019364       0.0010009       0.0010061


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.86088      2.4948e+05          73.563          9.0719


 TIME FOR THE TIME STEP              799:        0.45747E+02

===============================================================


 INSTANT    0.800000000E+01   TIME STEP NUMBER             800
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.711410016E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.327860960E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12762E+03 0.11112E+02
   Friction velocity        uet   :  0.33467E-01 0.24996E+02
   Friction velocity        uk    :  0.40357E-01 0.24996E+02
   Dimensionless distance   yplus :  0.31678E-02 0.24887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15556
   Nb of faces within the viscous sub-layer     :       9155
   Total number of wall faces                   :      41000
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step        800
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            



 Write final restart files
   checkpoint at iteration        800, Physical time    0.80000E+01


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint/main
 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                            
  Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary
 End writing


 Time for restart files:    0.51792E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16806E+02      56   0.10607E+00   0.66285E+02 0.31984E+02 
c  Velocity[X]                                      0.10299E+02 
c  Velocity[Y]                                      0.25874E+02 
c  Velocity[Z]                                      0.30111E+02 
c  Pressure     0.12784E+00     451   0.33761E-01   0.90544E-01 0.10918E+01 
c  k            0.91473E+00      20   0.39838E-03   0.79847E-01 0.34694E+02 
c  epsilon      0.82495E+04      13   0.23431E-03   0.58086E+07 0.54835E+02 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017907                             4
a  epsilon                 -2.3248                             2
a  Local Time Step      1.5141e-08                        281420


  ** Computed fields on cells
     ------------------------

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -8.9142          17.942           2.229         0.36615
v  Velocity[Y]             -36.305          44.722          1.2698         0.88812
v  Velocity[Z]             -58.009          35.228         -1.0785      -0.0046539
v  ǁVelocityǁ            0.0085572          61.292          7.6145          7.6495
v  Pressure                 -95272      3.3204e+05      2.0638e+05      1.7427e+05
v  k                    1.9493e-06          14.551         0.11368         0.12877
v  epsilon                0.043239      3.2884e+06          4589.5           85.27
v  TurbVisc             4.0416e-12         0.51511       0.0046563        0.053066
v  CourantNb              0.078629           66047          51.603          8.7126
v  FourierNb              0.025035      2.3655e+05          22.023         0.35952
v  total_pressure       4.0473e+05      8.3204e+05      7.0638e+05      6.7427e+05
v  Local Time Step           0.001        0.017918       0.0010009        0.001006


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88404      2.5214e+05          73.625          9.0721


 TIME FOR THE TIME STEP              800:        0.32111E+02

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.15221E-03
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation

e+05          73.625          9.0721


 TIME FOR THE TIME STEP              800:        0.62695E+02

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.18877E-03
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:          68906.594 s
  System CPU time:          210.348 s

  Elapsed time:           69308.275 s
  CPU / elapsed time          0.997

Memory use summary:

  Total memory used:                             676.949 MiB
  Theoretical instrumented dynamic memory:       318.238 MiB

Calculation time summary:

  User CPU time:          68986.305 s
  System CPU time:          208.480 s

  Elapsed time:           69378.436 s
  CPU / elapsed time          0.997

Memory use summary:

  Total memory used:                             676.949 MiB
  Theoretical instrumented dynamic memory:       318.238 MiB

Calculation time summary:

  User CPU time:          68979.734 s
  System CPU time:          209.992 s

  Elapsed time:           69383.243 s
  CPU / elapsed time          0.997

Memory use summary:

  Total memory used:                             676.949 MiB
  Theoretical instrumented dynamic memory:       318.238 MiB

Calculation time summary:

  User CPU time:          69077.461 s
  System CPU time:          209.900 s

  Elapsed time:           69480.258 s
  CPU / elapsed time          0.997

Memory use summary:

  Total memory used:                             676.953 MiB
  Theoretical instrumented dynamic memory:       318.238 MiB
